NASA TN D-934
TECHNICAL NOTE
D-934
TABLES OF INTERFERENCE FACTORS FOR USE IN WIND-TUNNEL AND
GROUND-EFFECT CALCULATIONS FOR VTOL-STOL AIRCRAFT
PART II - WIND TUNNELS HAVING WIDTH-HEIGHT RATIO OF 1.5
By Harry H. Heyson
Langley Research Center
Langley Air Force Base, Va.
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
WASHINGTON January 1962
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
TECHNICAL NOTE D-93 1 *-
TABLES OF INTERFERENCE FACTORS FOR USE IN WIND-TUNNEL AND
GROUND-EFFECT CALCULATIONS FOR VTOL-STOL AIRCRAFT
PART II - WIND TUNNELS HAVING WIDTH -HEIGHT RATIO OF 1-5
By Harry H. Hey son
SUMMARY
Tables of interference factors for use in wind - t ^ e ^ n J 1 ^ 0 ^; els
effect calculations for ^L-STOL aircraft
^rare a intendid e for use with the procedures of NASA Technical Report R-12A.
These tables are presented without comment.
INTRODUCTION
Reference 1 presents a linearized theory of wind-tunnel jet -boundary
correction^and ground effect for VTOL-STOL aircraft. (See aiso refer-
ence 2 .) In the course of that investigation, interference factors w
calculated for many combinations of wind-tunnel. i“°_ 6
location These calculations were obtained on IBM 704 and 7090 exec
Tronic data processing systems and the tables are reproduced from the
original tabulations as received from the machines. The ^erf
factors presented herein are for wind tunnels having a width-heig^
... -1 c qimilar results for tunnels having other width-helgni
5 5- Details of the derivation
and use of these factors are covered m reference 1.
NOTATION
The tabular data presented herein were recorded by machines an*
the limitations of the machines as to available type faces necessitated
some differences between the notation in these tables and the sy^ols
used in the analysis of reference 1. The following symbols are those
reference 1 and in the captions of the present tables, the dif
ferent notation recorded in the machine tabulation is included m paren-
theses after the symbol definitions.
2
b lateral distance from center of model to right-hand side of
vind tunnel (viewed from behind), ft (see fig. l)
B semiwidth of wind tunnel, ft
h. height of model center above wind-tunnel floor, ft
H semiheight of wind tunnel, ft
u longitudinal velocity component, positive rearward, ft /sec
v vertical velocity component, positive upward, ft /sec
x,y,z location of a point with respect to X-, Y-, Z-axes, respectively,
x measured positive rearward, y measured positive to right
when viewed from behind, and z measured positive upward, ft
(listed as X, Y, and Z in machine tabulations)
X,Y,Z Cartesian axes with origin at center of model (see fig. l)
7 ratio of wind-tunnel width to wind-tunnel height, B/H (listed
as GAMMA in machine tabulations)
8 interference factor
&u,D interference factor for longitudinal interference velocity
due to drag (listed under the heading 5 as (U,D) in machine
tabulations)
&u>L interference factor for longitudinal interference velocity due
to lift (listed under the heading 6 as (U,L) in machine
tabulations)
^w,D interference factor for vertical interference velocity due
to drag (listed under the heading 8 as (W,D) in machine
tabulations)
®w,L interference factor for vertical interference velocity due to
lift (listed under the heading 8 as (W,L) in machine
tabulations)
£ ratio of wind-tunnel semiheight to height of model above wind-
tunnel floor, H/h (listed as zjstA in machine tabulations)
^ H i ON
3
ratio of lateral distance between model center and right-hand
wall to semiwidth of wind tunnel, b/B (listed as ETA in
machine tabulations)
wake skew angle, angle between Z-axis (negative direction) and
wake center line, positive rearward, deg (listed as CHI in
machine tabulations)
PRESENTATION OF TABIiES
The corrections to wind-tunnel data for VTOL-STOL aircraft as given
in reference 1 require the determination of interference factors ^u,D*
&u l> &w D> 811(1 ^,1/ T* 1686 interference factors for a tunnel of
width-height ratio - = 1.5 are tabulated herein.
H
Longitudinal Distribution
The longitudinal distributions of interference factors for a
vanishingly small model for T) = 1.00, 7 = 4 • 5 > and C in the range
between 0.60 and 10.00 are presented in tables 1 to 8. For convenience
in locating specific tables, the following information is provided.
Table
5
Page
1
o.6o
1.00
7
2
• 70
1.00
16
3
.80
1.00
25
4
1.00
1.00
34
5
1.50
1.00
43
6
2.00
1.00
52
7
4.00
1.00
6l
8
10.00
1.00
70
Lateral Distribution
The lateral distributions of interference factors for 7 = 1*5 and
for a range of tj from 0.25 to 1.00 and £ from 0.60 to 10.00 are pre-
sented in tables 9 to 28. The lateral interference factors at y/H = 0
are excluded from tables 9 to l6, inasmuch as they are already included
in part (c) of tables 1 to 8. In certain cases, the factors were computed
for positions which require more decimal places than the two which were
4
allowed in the machine tabulation. In such cases, the additional decimal
places are stated in the subtitle of the table only. For convenience in
locating specific tables, the following information is given:
Table
4
Page
9
0.60
1.00
79
10
.70
1.00
82
11
.80
1.00
85
12
1.00
1.00
88
13
1.50
1.00
91
l 4
2.00
1.00
94
15
4.00
1.00
97
16
10.00
1.00
100
17
.70
.75
103
18
1.00
.75
no
19
2.00
.75
117
20
4.00
• 75
124
21
.70
.50
131
22
1.00
.50
158
23
2.00
.50
145
24
4.00
.50
152
25
■ 10
.25
159
26
1.00
•25
166
27
2.00
•25
175
28
4.00
.25
180
Vertical Distributions
The vertical distributions of interference factors for a vanishingly
small model for y = 1.5 , tj = 1.00, and for a range of {; from 0.60 to
10.00 are presented in tables 29 to 36. The vertical interference fac-
tors at z/H = 0 are excluded from tables 29 to 36, inasmuch as they
are already included in part (c) of tables 1 to 8. For convenience in
locating specific tables the following infonnation is given:
Table
5
T|
Page
29
0.60
1.00
I87
30
■10
1.00
I89
31
.80
1.00
191
32
1.00
1.00
193
33
1.50
1.00
195
34
2.00
1.00
197
35
4 .oo
1.00
199
36
10.00
1.00
201
H On
-F=-\J1 H IT*
5
CONCLUDING REMARKS
Longitudinal, lateral, and vertical distributions of interference
factors for a vanishingly small model have been presented. m tabular
form. These tabulations are intended for use in determining j -
boundary corrections and ground effect for VTOL-STOL aircraft for
tunnels having a width-height ratio of 1.5 *y the procedures given in
NASA Technical Report R-124.
Langley Research Center,
National Aeronautics and Space Administration,
Langley Air Force Base, Va. , June 3> 1961-
9
references
1 .
Hey son, Harry H. :
Corrections and
TR R-12^, 1962.
Linearized Theory of Wind-Tunnel Jet -Boundary
Ground Effect for VTOL-STOL Aircraft. NASA
2. Hey son, Harry H. : Wind-Tunnel Wall Interference and Ground Effect
for VTOL-STOL Aircraft. Jour. Am. Helicopter Soc._, vo . ,
no. 1, Jan. 1961 , PP* 1-9 •
3-
Hevson Harry H. : Tables of Interference Factors for Use m Wind-
Tunnel and Ground-Effect Calculations . for VTOL-STOL Aircraft.
Part I - Wind Tunnels Having Width -Height Ratio of 2.0. NAS
TN D-933, 1962.
k Hevson, Harry H. : Tables of Interference Factors for Use in Wind
' Tunnel anf Ground -Effect Calculations for VTOL-STOL Aircraft _
Part III - Wind Tunnels Having Width-Height Ratio of 1.0. NAS
TN D-935 , 1962.
Heyson, Harry H. : Tables of Interference Factors for Use m Wind-
Tunnel and Ground-Effect Calculations for VTOL-STOL Aircraft.
Part IV - Wind Tunnels Having Width-Height Ratio of 0.5- NAS
TN D-936, 1962.
7
TABLE 1
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 1 = 15. < * Q ' 60 ' AND n ' 1 '°°
(a) x/H = -2.00
r
Correction factors for correcting from a wind tunnel
which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
'
CHI ■ 0*
GAMMA* 1.5
ZETA* 0.60 X /Ha-2.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-O.OB95
0.0663
0.1155
0.7266
-0.0998 0.1317
0.2661 0.1798
-0.2065 0.0861
-0.0352 -0*1307
-0.1262
0.1840
-0.1479
0.2366
-0.1113
-0. 1 479
0.1840
—0.0116
0.0367
-0.1176
0.7634
0.4900
0.0264
0.0821
-0*0586
-0.2719
CHI-15.00
GAMMA* 1.5
ZETA* 0.60 X/H=-2.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
fU.D)
-0.0225
0.0520
0.1054
0.7358
-0.0460 0.1209
0*2173 0*1643
-0.1282 0.0698
-0.0880 -0.1561
-0.0649
0.1523
-0*1002
0*1781
-0.0761
-0.1002
0.1523
-0.0417
0.0424
-0.1003
0.2056
0.5577
0.0189
0*0651
-0.0280
-0.2661
CHI-30.00
gamma= 1.5
ZETA* 0.60 X/Hs-2.00 Y/H* 0.
Z/H= 0.
ETA* 1.00
(W.L)
(U.L)
rw.D)
(U.DI
0.0197
0.0316
0.0070
0.7353
-0.0132 0.1191
0.1760 0.1414
-0.0865 0.0481
-0.1251 -0.1721
-0.0284
0.1222
-0.0765
0.1327
-0*0477
-0.0765
0. 1222
-0.0571
0.0481
-0.0907
0.1635
0.6026
0.015?
0.0538
-0.0100
-0*2578
CHl -45.00
GAMMA* 1.5
ZETA* 0.60 X/H*-2.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L I
(U.L)
(W.D)
(U.D)
0.0476
0.0098
0.0663
0.7322
0.0054 0.1188
0.1408 0.1164
-0.06^7 0*0252
-0,1522 -0.1833
-0.0083
0.0958
-0.0647
0.0974
-0*0263
-0.0647
0.0958
-0.0620
0.0558
-0.0860
0.1310
0.6346
0.0137
0*0450
0.0000
-0.2496
CHI-60.00
GAMMA* 1*5
ZETA* 0.60 X/H*-2. 00 Y/H= 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.DI
0,0671
-0,0104
0.0450
0.7291
0.0130 0.1175
0.1101 0.0911
-0.0549 0.0030
-0.1730 -0.1923
-0.0003
0.0743
-0.0592
0.0700
-0.0107
-0.0592
0.0743
-0.0583
0.0674
-0.0847
0.1041
0.6591
0.0141
0.0358
0.004?
—0 . ?4?9
CHI-75. 00
GAMMA* 1.5
ZETA* 0.60 X/H--2.00 Y/H* 0.
Z/H= 0*
ETA" 1.00
(W.L)
(U.L 1
(W.D)
(U.D)
0.0827
-0.0247
0.0233
0.7263
0.0152 0.1141
0.0821 0.0658
-0.0528 -0.0177
-0.1897 -0.2009
-0.0019
0.0597
-0.0564
0.0487
0.0006
-0.0564
C . 0597
-0.0473
0.0846
-O.0B44
0.0797
0.6776
0.0170
0.0224
0.0036
-0.2384
CHI-90.00
GAMMA* 1.5
ZETA* 0.60 X/H*-2.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
0.0943
-0.0001
0.0001
0.7242
0.0115 0.1082
0.0549 0.0401
-0*0549 -0.0401
-0.2044 -0*2103
-0.0092
0.0542
-0.0542
0.0325
0.0092
-0.054?
0.054?
-0.0325
0.1035
—0 .0543
0.0543
0.6917
0.0207
0.0007
-0.0007
-0.2369
8
TABLE 1.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, < = 0.60, AND „ = 1.00
(b) x/H = -1.00
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 — — , —
to grour
id effect
C H j = : *
r-uMMA- 1*5
/ft a* n,6f> x / r- - -
l,oo y/h= n.
7/h= r.
fta= 1,00
»L )
n.i»u i
< > t ■’ >
>
-> .521?
-
, 3 1
C. * 3 75 f >
-ti, in ao
n ,6746
-0,6906
0 , 0 O I 3
0,6693
O, -(94?
-n,;- : 06 9
-n.n
-0, 36*0
0, 2374
-0,4109
0 , >956
-0. On i 8
-0,4103
0, ? 3 7 6
0 . 1 ?61
-0,1633
-0,4600
0 , p8l
0 , 0 1 4 1 1
0,3*1 1
r , 4 3 7 1
-0.4 707
-n . 7 041
CHI = 1
r-A^viA- i®5
7 r T A = 0,60 X/H = -
1,00 y/H= 0,
7 t h = n ,
r T A = 1 ,O0
{ w t LI
( i J * L
< w*r>)
< i . « n >
-U.-410?
-0 * 19* '6
<J . 3 794
0,476 1
-0,0407
0,6367
-0,6/07
-0,039 I
0,4699
0 , 4 6 ] n
— 0 , ■ 63 B
-0 ,719 7
0,3409
-0 , ;>a 3 v
-0 , 033P
-0 . 6 3 7
0 , - 4 0 g
0,0334
-0.09! .0
-0.4316
n, 64 -- 1
0,3774
0* 1 790
0 • 3 q 5 9
-0.40 /O
— 0. 7.8 06
CHI =3 .
GAMMA* 1,5
/FT A* 0,60 >' / H = —
.00 v/h= 0,
?/H= n.
PTA* 1 , on
( W t L )
( tt, L )
1 w * D )
< U *0 1
— J* 15 /9
-0.20 lb
i., *3 94 S'
i;,fcl4si
0 , 00 73
0 , 5 / ri J
- 0 , 4?K 1
“-••1642
0 , *16 4 6
0,4600
-0, 1 724
-O, ■■' -,w",
-0,1777
0,7 03 5
-0*1 76?
0,1*74
-0, 07.7 7
-0. 1 7ft?
0.7088
-0,0374
-0 . 0 3 6 9
-0.41 0?
0.571 1
0.4774
0,1 70*
0*7 6« 7
-0.741 C
-0.3416
CHI =4 5. O'"
oft MMA= 1,5
7PT.A= 0,60 */*< = -
,00 Y/H= o.
;/h= 0 ,
P T A = 1 , n o
IW*L)
<l'*L )
( W » D )
( U * D J
*C'ii!47A
“i : • 2 3 7 7
r; *3(144
0 * fe 7 B 5
O,0?*4
n , 4 1 a 5
-0,4405
-0,7 746
0,?964
0,441 6
- 0 ,,'fih 7
-0,3390
-0,063/}
O, 1 643
-0,1776
0.1756
-0,0010
- 0 . 1 3 76
0, 1443
-0,0470
0.01 54
-0.4030
0.41 17
0.4603
0.091 3
0,3337
-0,3137
-0*4031
chi = f>n , Du
GAMMA* 1,5
/PIA= 0,60
,00 y/H= n.
Z/h'4 0 ,
FTA* 1,00
( to f L }
(U*L)
(w»n )
( U .0 ]
'•<*i.;3 66
, 7 Hi' 4
,! «W 'A
n ,7390
0.SV/-7
0,4697
-0,3905
-0,3719
0,243^
0 , 4 0 A 4
-'1.7475
6 Or' 6
-o,0366
0,1714
- A .1 A 1 7
o.Ofl 1 ]
0 , m 4c
-0,101?
0,1714
-0,0603
0,0771
-0 ,4013
0.461 1
0,64 G fj
0 • 0 c s ?
0,3377
-0 , 7 pen
-0*4*- 30
CHI ~ V b • U w
GAMMA* 1,5
/£?A= 0 ,60 X / N = - 1
.00 Y/H= 0 .
?/H= 0.
FT A= 1,00
< W,L )
(U*L)
1
( u ♦ n j
0.1103
--*4115
: .. , '4 2' 9 r :
0 , 6 0 5 9
-0,0043
0 , 405 . 6 .
-0, 3fc4S
-0,4616
0. 1 937
0. 766 A
-0.7*60
-0.47H «
-0,0316
0.0Q04
-0,0864
0.0466
0.0707
-0, 0344
0, 0006
- 0 , 0446
0.1419
-0.407.0
0.4164
0, 74Q3
0*0777
.0*? 151
—0*7 74 R
—0*5090
C H I = ‘/V i . i u
GAMMA= 1,5
/FIA= 0,60 >/h=-]
,00 Y/H* 0,
;/h= 0 .
FTA = 1,00
C irf • L )
< '• 1 » L )
i * 0 )
f U *0 )
-•1606
-0.7661
0.7*61
9 76 K
-0 ■ 0469
0,3614
-0 ,3614
-0.6607
0.1403
0.31H5
-0,3166
- 0, 4 66 S
-0,0356
0.0755
-0.07 5 6
0.077 7
0,0336
-0,0755
0,0754
- 0 . n??7
0,7194
-0*3697
0.3637
0.6441
-0*00fl?
0*7 759
-0*7756
-0*4733
6-t^i- 1 n
l-15^9
9
TABLE 1.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 15, C = 0.60, AND » = 1.00
(c) x/H = y/H = z/H - 0
Correction factors for correcting from a wind tunnel which is
8
closed
close d
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground
effect
CHI
fi A M W A - 1.6
7 FT A =
0,60 V/m=
0, Y/H = 0,
z/h= n.
?TA = 1,00
t )
t U * L )
rv«ni
MJthi
“2.4767
C # 0 0 4 5
-0.4753
-1,5775
1.3773
-0,0793
-0.7768
1.0072
7,4253
-0.7060
0.00? 1
1,2308
-0.69RP
-0.0381
-0,7004
0,0051
0.6754
-n, 7004
-0. 0381
0, 2990
-1 « 8780
0,0476
(1,7751
-1 ,6877
1 ,9766
-0*0413
-0,07*4
1 ,0971
CHI= 3.'' , 0
GA^A* 1.5
7 FT A =
0,60 X/H=
n, Y/M= 0.
7 /m= 0 »
fTA* 1,00
<W*U
{ V * L )
rw*o>
IUiOI
-2.4767
-0 ,0 A 45
-0.3475
-1 .4?91
1 , 3 77 R
0.0793
«.r. , 7*^33
1,1337
3,2270
-0,267«
-0,0031
1.2308
-0.5988
0.0381
-0.6691
0,0769
0.5316
-0.6691
0.0381
0. ?99p
-1.8780
-0.0426
0.3713
-1.6060
1 .9766
0.041 2
-0.114?
1 .061 7
OH I 3 1 5 , 9 9
RAWA= 1.5
7 F r A =
0,60 X ,/ u =
0, Y f H ~ 0 ,
Z/H = ",
f T A = 1.00
(W,L )
(U*L )
f W » D )
(u.ni
-7.4305
-0,0430
-0,05? 3
-1.1816
1,4626
C , 3 8 5 ^
-0 .8364
1 . ' 736
5 , 9 08 ?
0.0297
-0,0361
1 ,1751
-0. 5748
0.17*6
-0.5536
0.1760
0.3014
-0,3436
0, 1 746
0 , 2467
-1 .8967
-0.2] 76
0.5017
1 ,9-374
0.3107
-0. 2 R2P
0*9976
oht
r, ' , 5
?vr a -
0,46 y/Ms
0, Y/ Us
7/ui- 0,
C T A = 1.00
* • L )
(U*L 1
(w*ni
(U,D1
-0.19Q4
0.34 7 9
-0.9767
1 ,683*
0,7138
-0 ,5748
1,1117
7,6767
0.4277
-0,184?
1 ,0344
-0,776 0
0 . 7649
-0. ’ 766
0. 701 0
0, 1 397
-0 , 7 766
0. 2649
0,1317
-1 . 9473
-0.4644
0, 7?44
—1.1778
7 , 0^96
0.4480
-0.49O •)
0,91 07
CHIs4S.n0
f,AMMA= 1.5
7 FT As
0,50 X/H=
0, v/hs 0,
Z/H* 0,
FT A= 1.00
(Will
f U • L >
( w * o i
tu »r> j
-7, 7331
-0.5194
0,7370
-0 ,B4 A 2
1,937’
0*9314
— 0 , 98 3 e
0,3566
7,5983
0,8110
-0,4930
0.8679
-0.3149
0.2506
-0,2757
0.1 49P
0,087?
-0, 3757
0,2505
0.0074
-2*01 P?
-0.7690
0,9728
-0.9900
7.167?
0.7410
-0*7470
0.8067
CHI =6% *
GA MM A= 1.5
7FT A =
Oi,60 X/H =
: 0, v /H= 0,
7/H- 0.
r T A = 1.00
( W * L )
(U*L )
|V,0)
111*01
-2.1988
-0.9765
1.1235
-0.6831
2,137'-
1,284/
-1 * 7?Oj-
0 , 737 11
2.603?
1 , 1 845
-0,9764
0 , 6- 8 5 9
-0.118?
0.1 799
-0.1 842
0. 03 00
0 , 0 8 ? 9
-0 , 164?
0. 1 7 99
-0,0794
-7 ,0806
-1.1563
1.2777
-0.7639
7.7566
1 . 1 043
-1 ,0667
0*6671
OHl s7K.no
GA MV A= , .5
7 FT A :
r 0,60 X/H-
= 0 , V /H= 0.
7/H= 0,
cta= 1.00
M> r * L )
t>'«U
(W*0)
(U *0 >
-2.1915
-1,5086
1.5520
-0.4245
2,26’ 5
1 , 6 5 ’ •+
-1 .601 *
0.4430
7,633 8
1 ,597k
-1 .4651
0,4261
-n,opp7
0.1176
-0.112?
0.0?99
0. 0RK6
-0.112?
0,1176
-0.0269
-2.1032
-! .6261
3 *664?
—0 .4646
? , 3499
1*6360
-1 .4894
0.4130
HA^HAs -.5
?CT A
r ",6 0 V/K
= o, y/M=0,
?/«= 0,
FTA= 1,00
fW,L t
M.<*1 )
( W * D )
(IJtOI
-7.1768
-7.0651
2.9651
-9, ''■non
2, ’ 704
7.1374
-2,1374
n , non.-,
2 • 6 6 c 0
7,0897
-7,0597
n.ooor
-0.O8KQ
0,0859
-0,0859
—0 ,
0,085®
-0,0859
0.0859
0 .
-2.0908
-2,1611
2.1611
-0,0000
2.4156
2.0466
-2*0466
0,0000
10
TABLE 1,- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 0.80, AND rj = 1.00
(d) x/H = 1.00
s
Correction factors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
— -t “ » 1 — r- -|
-r 1
CHI- 0.
GAMMA = 1,5
2ETA- 0.60
X/H*
1.00 Y/H- 0.
Z/H* 0.
ETA* 1,00
<w,u _ "
(u.u
(W.D)
(U.D }
-0.5212
0.2320
-0.7845
-0,9143
-0,1069
-0,6746
-0.0259
-0,1565
2.4360
-0.7179
0.2069
“0,0253
“0.3580
-0,2374
-0*4562
“0.2249
1.2259
“0.4562
“0.2374
0.1261
-0.1633
0.4695
-0.3283
-0.6094
0*251!
-0*4371
0.4303
0*0683
CHI-15.00
GAMMA* 1.3
ZETA- 0.60
X/H =
1.00 Y/H* 0*
Z/H- 0.
ETA* 1.00
(W»L)
(U*L )
(W.D)
(UiD)
-0,7989
0*3507
-0,8958
-0.8556
-0,1479
“0,6382
-0,0720
0.0530
2.2284
-0*8226
0.3274
0.0595
“0.5201
“0,1586
-0,5498
“0.1204
0.9787
-0.5498
-0.1586
0.2286
-0.2788
0,5094
“0,3460
“0,7352
0*372?
-0*4795
0.4779
0.1734
CHI-30. 00
GAMMA* 1,5
ZETA* 0,60
X/H*
1.00 Y/H- 0.
Z/H- 0.
ETA* 1.00
(W.L )
(UiL)
1 W »D J
(U.DJ
-1 .0881
0.6275
“0,8951
-0.6345
-0,0513
-0.5494
-0.0338
0.1587
1 .995 5 ~
-0*8155
0,6073
0.2791
“0.6230
0.0256
-0.5431
0.0147
0. 6463
-0.5431
0.0256
0.2946
“0*4651
0.6019
“0.3520
-0.6497
0.5717
-0.5751
0*509?
0.1441
CHI-45.00
GAMMA* 1,5
ZETA* 0.60
X/H =
1,00 Y/H* 0.
Z/H* 0.
ETA* 1*00
fW.L)
fU»L)
(W.D1
(U.DI ■
-1 ,3257
0.8944
“0,7885
“0.5507
0.4301
-0.4082
0.1806
0.3222
1.8974
-0.7042
0,8827
0*3203
“0.5143
0.2332
“0.3932
0.1100
0.3385
-0. 3932
0.2332
0.1892
-0.8114
0.6617
“0.3954
—0 .6606
0,9444
-0.6415
0.5737
0.2123
CHI-60.00
GAMMA- U5~
ZETA* 0.60
X/H=
1.00 y/H= 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U*L)
rw.D)
fU.D)
-1,6771
0,8385
-0,6204
“0.6501
1.3246
-0.3747
0*3865
0.4089
2.2114
“0.53eR
0.8489
0.3535
-0.7702
0.2326
“0.7123
0.0732
0. 1983
-0,2123
0.7326
0.0188
“1.4069
0.6058
-0.4080
-0.7233
1*5947
“0.6073
0.5988
0,3357
CHI-73.00
GAMMA- 1,5
ZETA* 0.60
X/M =
1.00 Y/H- 0.
Z/H- 0.
ETA* 1.00
(W.L)
fUiL)
IW.D)
IU.D)
“2,5300
0,4534
“0,3783
-0,8085
2.5101
-0,2531
0.3089
0.5022
3.0996
-0.3191
0,4925
0,4897
“0.1611
0.1277
-0.1207
0.0086
0.1569
-0. 1207
0.1277
-0.0037
-2.3689
0.3257
-0.2576
-0.8172
2.671?
-0*3808
0. 4? 96
0.4936
CHI-90,00
GAMMA- 1,5
ZET A= 0.60
X/H*
1.00 Y/H- 0,
Z/H* 0.
ETA* 1.00
(W.L )
(U.L )
(W.D1
(U.D)
-4,5343
-0,2881
0.2881
-0,8768
4.7061
0.3514
-0.3514
0.5507
5.1778
0*3185
“0.3185
0.5565
“0.1333
0.0755
-0.0755
“0.0227
0*1333
-0.0755
0. 0755
0.0227
-4.4010
-0*3637
0*3637
-0.8541
4.8394
0.2758
-0.2758
0.5733
6+^i-n
l-15^9
11
TABLE 1.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.60, AND f] = 1.00
(e) x/H = 2.00
s
Correction foctors for correcting from a wind tunnel which is
—
closed
closed
on bottom
only
open
closed floor
only
{ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
, — '
CHI* 0*
GAMMA- 1.5
ZETA*
0.60
X/H* 2.00 Y/H* 0*
Z/H- 0.
ETA= 1.00
(W.L)
( U * L )
( W*D)
(U»D)
-0.0695
-0.0663
—0*2943
-0.8544
-0.0998
-0.2661
-0.1030
-0.1585
2.4169
-0.2408
-0.0861
-0.1307
-0.1262
-0.1840
-0.2129
-0.1963
1.3780
-0.2129
-0. 1840
-0.0116
0.0367
0.1176
-0.0814
-0.6581
0.0264
-0.0821
0.1099
0.0378
CHI *15.00
G A MM A = 1.5
ZETA-
0.60
X/H* 2.00 Y/H* 0.
Z/H = 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U*D)
-0.2285
-0.2106
-0.2913
-0.1931
1.2947
-0.2913
-0.2106
0.0428
CHI-30.00
GAMMA- 1.5
ZETA-
0.60
X/H* 2.00 Y/H* 0.
Z/H* 0.
ETA- 1.00
(W.L)
(U.L)
IW.D)
(U.D)
-0.3853
-0.0176
-0.4431
-0.8204
-0.3069
-0.3881
-0.1993
-0.1393
2.1562
-0.3793
-0.0452
0.0283
-0.3871
-0.2241
-0.3589
-0*1902
1.1206
-0.3589
-0.2241
0. 1708
0.0018
0*2064
-0.0842
-0.6303
0.0802
-0.1640
0.1596
0.0509
CHI *45 * 00
GAMMA- 1.5
ZETA-
0.60
X/H* 2.00 Y/H- 0.
Z/H- 0.
ETA* 1.00
(W.L)
(U.L)
(W.O)
(U.D)
-0 .7128
0.2546
-0.5535
-0.6562
-0.4269
-0.3306
-0.2095
-0.0111
1.8790
-0.4809
0.221 1
0.1225
-0.6236
-0*0625
-0.4317
-0*0548
0.8129
-0.4317
-0.0625
0.2626
-0.0893
0.3171
-0.1219
-0.6014
0.1967
-0.2680
0.2222
0.0437
CHI-60.00
GAMMA- 1.5
ZETA*
0.60
X/H- 2.00 Y/H- 0.
Z/H- 0.
ETA- 1.00
(W.L)
(U.L)
(W.O )
(U.D)
-0*9511
0.6675
-0.50S9
-0.5324
0.0846
-0.1904
0.0636
0.1068
1*6330
-0.4251
0.6578
0.1050
-0*5153
0.2238
-0.2869
0.0527
0.3922
-0.2869
0.2238
0.1450
-0.4358
0.4637
-0.2220
-0.5851
0.5998
-0.4142
0.3505
0.0541
CHI-75.00
GAMMA* 1.5
ZETA-
0.60
X/H* 2.00 Y/H- 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-1.5561
0.5260
-0.4154
-0.6333
1.4014
-0.2723
0.3189
0.1385
2.2128
-0.3395
0.5422
0.1259
-0.2337
0.1270
“0.1175
-0*0027
0.2265
-0.1175
0.1270
0.0113
-1.3224
0*3989
-0*2979
-0*6306
1.6350
-00993
0.4364
0.1411
CHI-90.00
GAMMA- 1.5
ZETA-
0.60
X/H= 2.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-4,4478
-0.0001
0.0001
-0.7242
4.6478
0.0549
-0.0549
0*2044
5.2099
0.0401
-0.0401
0.2103
-0.1627
0.0542
-0.0542
-0.0325
0.1627
-0.0542
0.0542
0.0325
-4.2851
-0.0543
0*0543
-0.6917
4.8105
0.0007
-0*0007
0*2369
12
TABLE 1.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0,60, AND tj = 1 .00
(f) x/H - 3.00
a
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
» 1 1- -- --
to grour
id effect
CHI a U*
oAMMA= 1.5
ZET A*
0*60 X/H- 3*00 Y/H- 0*
2/H= 0*
ETA = 1.00
( W * L )
tU.L )
( W # 0 1
( U * D )
- * y 1 6 6
-0*0761
-0*1503
-- . 73 12
-0*0319 <; • 43 j 1
— G*119i -C*lC*3
*3 i u I JO -0*0635
--•vfiU -0*09*4
— 0 • 04 3 3
-0. i ICO
— C* i 105
-0*1337
1*3950
“C * i 1 0 3
-0*1100
— C • J 3 9t>
-0* 00 J i
0*0349
0 • 0 h 0 'j
CHI =15*00
0 A MM A - l*y
ilcl A =
itoL. A / ri = 3*00 t / j •
to /i;= ^ ,
E7A = iivi
(W*L)
( U »L )
>
(U*D >
“ J * - 9 y 1
- J * 1 3 / 3
-V*i>li
-0 • 1 4 32
1*9019
-0*1311
-*• 13 t y
— 0 * -22 0
Crt I - 3 - • y -
i*y
=
G.cy ,/t; *.
<- / h - 5 •
LTift- 1 * 0 0
< ft * L )
1 U »L i
( « *D }
(U ti> )
“0 • 1449
- • 1 u d 2
“J *236 j
- y.7759
-*•15/5
--*1994 -w*i£)-+j
—y * 1499 -0*12* 1
— - * i ( i 4
-y • l / 05
— y*2y*2
“0 • a * y 0
a * 4 . 9 j y
— y* j. f y y
0 • 0 b 2 J
~0 * y j 1 1
— k.tju;
0 * 0 1. 0 6
— y t O2o 9
y • 0 - 4 j
CHI = 4 y * CO
5AMKA =» 1 « =
ZET*
-• -y a/H- ,«^ V/H- J •
*- / H = y *
ETA- 1 < uG
< ft ♦ L )
<C*L)
U 1 » D )
( U f 0 )
- c « 3 J 2 9
“v 1 * OW 3
-y *3l4l
-0 • 753 j
9 t *iu4l
-t-lt-SL -J*236y
“-*20j1 — y*i030
— **G72u -y*0135
— - • 3044
-G • jl 9 1 2
“0*4470
1 • 1 3 l 9
-0*2 7o /
— 0* ivL
0*093o
0 • 0 j 1 y
0* 1 1 y t
—0*0-34
“0*412.3*
0*0*15
—0 • y ub 2
0*0 7 3 o
0* uyy*
Cm = 60* vC
is A MM A = 1*3
2 L f <* =
u * o C a / — — jtuii V/n= v •
*/h = - •
c.TA= 1 *00
t ft' • L I
UJtLI
IW*D)
t u * O >
-v*739d
o*2645
-- • 62 5*
“0 • *90 / it / 14 1
-0*15^0 -0*3367
— v*l6*9 0*2 2oo
-•^woti 0 • i 1 3 2
-0 *3 Zoo
0*0030
-0* 32 34
— o * 026o
0 » i i. C' b
-U« 3234
C • Ou y 0
0 • 243 u
—0 • 0t> 3c
0*2390
-0*07 y 3
-u*o023
C* ls,j
-0*1950
0*1443
0* 0 3 3 2
CH I - i y • 0 0
yAMMA= i*y
ZETA =
y*o* A / H — 3*1/0 i /H= 0*
4 / H = u *
E i A = 1*00
( U » L 1
(U »L )
( Ml •& )
(UtD)
-1*0983
0*4757
-o*3293
-o#6133
0*7627 1 • e 1 3 V
—0*169/' — o*2 49o
0*1929 U*4b37
y*y5o3 0*0395
— u* 3ud3
0 • i 2 9o
-0*1169
— — * u * 2 7
0*2932
-o* iioy
u # i 2 9 o
0. 0193
“0* 7 6.9 7
0*34oi
-o *li4J
“2 • Oi 00
i • y 7i2
— 0 * 2 9 a j
0*3*9 O
0 • 0 3 3 i
CHI =90 iOu
GAMMA= 1*5
ZE7A =
0 • 6 y a / h - 3 • O' 0 ') / H - y t
2/H = 0*
t 1 A= IiwO
I w * L )
< O • L )
Ift *U)
(U»DJ
-4*4032
y *035 5
-0 * * 3 5 5
-0*6898
4*0331 5*2304
-#-122 y*yy9*
—J**i22 —(-*0090
0 • 0969 0*1026
-y*i 752
4*0353
— u • u 353
-0*03ib
4*1732
-0*033 J
- * 03 3 3
0*0316
—4 • 2 2 o 0
u • 00u 2
-0*0002
-0*O3b0
4* CiUoy
“0*0231
0*0231
0* 130o
6+£ i-i
L-15^9
13
TABLE 1.- Continued
longitudinal distribution of interference factors for V = 1 . 5 , c = 0.60, AND H = 1.00
(g) x/H = 4.00
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
'
CHI = 0,
6AMMA= 1,5
Ztl A=
0,60 a/H=
4.00 Y/H= 0,
l/H= u •
i T A= 1.00
(WtU
(U«L>
(WtD)
1 U »D )
-u ,0027
-0,0553
-0,0981
-C ,65 79
-0,0089
-0,0636
-0,0516
-0,0579
2,4379
—0,0 564
-0*0562
-0.0573
-0.0166
—0 • 0668
—0 , 0662
-0.0928
1.3935
-0. 06fc2
-0 • 0668
-0.0354
0*0138
0,0115
-0.0319
-0,5651
0.0076
0.0033
0.0146
C, 0349
CHI =15.00
GAMMA= 1,5
ZE7A =
0,60 X/H 8
4,00 Y/H = 0,
Z/H = 0.
ETA= 1.00
(WtL)
(UtL)
(WtD)
( U »D 1
-0,040b
-0,0851
-0,0888
-0.1005
1.3761
-0,0688
-0.0351
-0,0302
CHI =30,00
GAMMA= 1,5
ZET A -
0,60 X/H =
4,00 V /H = 0*
Z/H= 0.
E. T A= 1,00
(WtL 1
(UtL)
(WtD)
(UtD)
-0,0675
-0,0896
-0.1457
-0,6969
-0 , U 7 5 5
-0,1108
-0,0945
-0,058B
2,3762
-0,1013
-0,0931
-0.0545
-C .0868
-0.1106
-0.1189
-0,1062
1.3399
-0. 1189
-0.1106
-0.0192
0.0193
0.0210
-0*0268
-0.5906
0.0112
-0. 0002
0*0244
0.0473
CHI =45*00
GAMMA= 1,5
Zt T A =
0,60 A / ri =
4.0C Y/H= 0,
Z/rt = 0*
ETA= 1.00
(WtL)
( 0 * L )
(WtD)
IU*0)
-0, 1886
-0,1477
-0,1645
-0*1 07b
1.2565
-0.1645
-0.1477
0,0087
CHI =60.00
GAMM A= 1,5
ZEi A =
0,60 X / H 8
i 4.UCJ Y/H* 0,
Z/H = 0.
ETA= 1.00
(WtL)
(UtLI
(WtD)
( U * D )
-0,4509
-0,0596
-0,2744
-0,6830
-0,4326
-0,2143
-0,1892
-0,0396
2,0392
— G, 2 219
-0,0814
0.0202
-0.4813
—0 • 1 fa25
-0.2427
-0.0842
1.0069
-0.2427
-0.1625
0.1194
0.0303
0.1029
-0.0317
-0.5988
0.0486
-0,0520
0,0535
0.0446
CHI =75,00
GAMMA= 1,5
ZET A =
: 0,60 X / M :
- 4 . 00 Y / H= 0 •
L /H = u .
ET A= 1,00
(WtL)
( 0 t L )
(WtD)
(UtDI
-0,8626
j , 4446
-0*2700
-0.5847
0,2629
-0,0892
0,0771
0,0332
1.6369
-0,1960
0.4142
0.0142
-0,4035
0.1403
-0.1262
0.0026
0.3760
-0. 1262
0.1403
0.0341
-0.4592
0*3043
-0.1438
-0.5873
0.6864
-0.2295
0.2033
0.0306
CHI =90,00
(WtL)
(UtL)
(WtO)
(UtDI
GAMMA= 1,5
-4,3827
0,0401
—0 , 040 1
-0,6529
ZETA
= 0,60 X/h
4,6363
0,0028
-0,0028
0,0569
= 4.00 Y / H = 0.
5.2558
0.0046
-0.0046
0,0 594
Z/H = 0.
-0*1790
0.0225
-0.0225
-0.0271
eta= 1.0C
0.1790
-0.0225
0.0225
0.0271
-4.2037
0.0176
-0.0176
-0.6258
4,6153
-0.0197
0,0197
0.0839
TABLE 1.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.60, AND 1 }= 1.00
(h) x/H = 5 .00
8
Correction foctors for correcting from a wind tunnel which is
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
‘ 1 1 » — !
to grour
— f
>d effect
■ o*
GAMMA* 1.5
ZETA = 0.60 X/H*
5.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L 1
(U.L)
(WtOI
(U.D)
“0.0001
-0.0390
-0,0732
-0.5828
-0.0024
-0.0392
-0.0358
-0.0392
2.4404
-0.0349
-0.0375
-0.0378
-0.0071
-0.0432
-0.0437
-0.0676
1.3904
-0.0437
-0.0432
-0.0282
0.0070
0.0042
-0.0295
-0.5152
0.0047
0.0040
0.0079
0.0283
CHI *15.00
GAMMA* 1.5
2ET A*
0.60
X/H*
5.00
Y/H*
0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.0 1
“0,0137
-0.0501
-0.0858
-0,6050
-0.0164
-0.0511
-0.0475
-0.0391
2.4262
-0.0464
-0.0489
-0.0376
-0.0217
-0.0553
-0.0577
-0.0729
1.3795
-0.0577
-0.0553
-0.0263
0.0080
0.0052
-0.0281
-0.5321
0.0053
0.0042
0.0103
0.0337
CHI *30,00
GAMMA* 1.5
ZETA*
0,60
X/H*
5.00
y/h*
0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
IU.DJ
-0,0391
-0.0655
-0.1033
-0.6231
-0,0428
-0.0682
-0.0638
-0.0391
2.4005
-0*0628
-0.0646
-0.0372
-0.0493
-0.0726
-0.0765
-0.0773
1.3567
-0.0765
-0.0726
-0.0223
0.0101
0.0072
“0.0266
“0.5458
0.0065
0.0045
0.0126
0.0382
CHI *45.00
GAMMA* 1.5
ZETA- 0.60 X/H*
5.00 Y/H* 0.
Z/H* 0,
ETA* 1.00
(W.LI
(U.L)
(W.D)
( U »D )
-0,0951
-0.0881
-0.1306
-0.6377
-0.1006
-0.0957
-0.0894
-0.0388
2.3457
-0.0090
-0,0883
-0.0356
-0.1099
-0.1003
-0.1052
-0.0805
1.3044
-0.1052
-0.1003
-0.0126
0.0149
0.0123
-0.0254
-0.5572
0.0094
0.0046
0.0158
0.0417
CHI *60 • 00
GAMMA* 1.5
ZETA*
0.60
X/H*
o
o
in
Y/H*
0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
( W » D )
(U.D)
-0.2630
-0.1128
-0,1843
-0.6444
-0.2711
-0.1504
-0,1362
-0.0365
2.1867
-0.1404
-0.1169
-0,0227
-0.2902
-0,1475
-0.1592
-0.0785
1.1497
“0.1592
“0.1475
0.0277
0.0272
0.0347
-0*0251
-0.5659
0.0191
-0.0029
0.0230
0.0420
CHI-75.00
GAMMA* 1.5
ZETA*
0.60
X/H*
5.00
Y/H*
0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-0,7598
0,3967
-0.2374
-0.5479
-0.1586
-0.0334
-0.0299
0.0245
1.6085
-0.1754
0.3589
0.0244
-0.5428
0.1411
-0.1479
0.0057
0.4870
“0*1479
0.1411
0.0799
-0.2170
0.2556
-0.0896
-0.5536
0.3842
-0.1745
0.1180
0.0188
CHI-90.00
GAMMA* 1.5
ZETA-
0.60
X/H*
5.00
Y/H*
0.
Z/H* 0.
ETA* 1.00
(W.L)
(U i L )
(W.D)
(U.D)
-4.3718
0,0391
-0.0391
-0.6078
4.6418
0.0005
-0,0005
0.0362
5.2678
0,0038
-0.0038
0,0384
-0.1795
0.0147
“0.0147
“0.0220
0.1795
-0.0147
0.0147
0.0220
-4.1924
0.0244
-0.0244
-0.5858
4.8213
-0.0142
0.0142
0.0582
6 ^ 1-1
l-i^9
15
TABLE 1.- Concluded
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR Y = 15. C = ° «°. “ ’= 100
(i) Miscellaneous additional values of x/H
CHI-15. 00
GAMMA* 1*5
ZETA* 0.60
X/H* 0.45
Y/H- 0*
Z/H* 0*
ETA* 1.00
tW.L)
( U »L )
IW.D)
(U«D )
-1*7880
0.7*62
-1.0798
-1.0087
0.6750
-0*6933
0*0257
0.6071
2*6433
-1.0000
0.7371
0*7208
-0*6068
0*0206
-0*6190
0*0372
0*6093
-0.6190
0,0206
0.2995
-1.1812
0.7256
-0.4608
-1.0459
1.2819
-0.7138
0.6446
0*5699
CHl-30,00
GAMMA® 1.5
ZETA* 0.60
X/H- 0.97
Y/H- 0.
Z/H* 0,
ETA* 1*00
fW.L)
(U.L)
rw»D>
f U *D 1
-1*1224
0.6535
-0.9072
-0.6348
-0.0159
-0.5540
-0,0192
0.1796
2.0036
-0.8273
0.6342
0.2953
-0.6227
0.0368
-0*5431
0*0227
0.6274
-0.5431
0.0368
0.2944
-0.4997
0.6167
-0.3640
-0,6575
0.6068
-0.6909
0.5239
0.1569
CHI-45.00
GAMMA- 1.3
ZETA* 0.60
X /H» 1,67
Y/H* 0*
Z/H* 0*
ETA* 1.00
tW.L )
IU.U
t U »D I
-0.8664
0.4705
-0.6415
-0.5848
-0.3124
-0.3339
-0.1335
0.0533
1,7839
-0.5633
0.4397
0.1690
-0*6482
0*0464
—0 i 4503
0*0035
0*6499
-0*4503
0*0464
0*2807
-0.2181
0.4240
-0.1911
-0.5883
0.3358
-0.3803
0.3168
0.0518
CHI *60*00
GAMMA- 1.5
ZETA* 0*60
X/H- 2*89
Y/H- 0,
Z/H* 0*
ETA- 1*00
fW.L)
IU.U
(W*0)
IU*D1
-0.7657
0.3179
-0,4174
-0,6166
-0.4637
-0*1804
-0.1669
0.0184
1,7409
-0.3474
0*2786
0.1195
-0*6779
0*0364
-0*3278
-0*0159
0.6791
-0.3278
0,0364
0.2448
-0.0877
0.2815
-0.0896
-0.6006
0.2143
-0.2167
0*1610
0.0343
CHr-75.00
GAMMA* 1.5
ZETA- 0*60
X/H* 4,56
Y/H* 0.
Z/H* 0.
ETA* 1.00
f W ♦ L 1
IU.U
fW.Dl
»U*D 1
-0,7906
0.4232
-0.2488
-0,5638
0*0343
-0*0536
0.0162
0.0279
1.6040
-0.181 1
0.3887
0.0145
-0*4749
0*1453
-0*1369
0*0053
0.4329
-0.1369
0.1453
0.0539
-0.3157
0.2799
-0.1119
-0.5691
0*5091
-0.1990
0.1531
0.0226
16
TABLE 2
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR ? - 1.5, C = 0.70, AND V= 1.00
(a) x/H = -2,00
CHI- 0.
GAMMA- 1.5
ZET A = 0,70
X /H--2 • 00
Y/H=
0.
If H* 0.
ETA* 1.00
(W.L)
(U.L )
(W.D)
(U.D)
-0.1188
0.1283
0.0552
0,7134
-0,0802
0.2647
-0.1580
0,0735
0.1196
0.1226
0.1406
-0.0961
-0.1194
0.2122
-0.1387
0.2784
-0.1473
-0.1387
0.212?
-0.0373
0.0006
-0.OB4O
0.1939
0.4360
0.039?
0.0526
-0.019?
-0.2049
CHI-15.00
GAMMA* 1.5
ZET A- 0.70
X/H— 2.00
Y/H=
0.
Z/H= 0.
ETA= 1.00
( W »L }
(U.L)
(W.D)
(U.D)
-0.0508
0.0960
0.0632
0,7072
-0.0243
0.2173
-0.1038
0.0019
0*1276
0.1236
0.1074
-0.1235
-0.0572
0.1725
-0.0978
0.2099
-0.0994
-0.0970
0.1725
-0.0640
0.0064
-0.0765
0.1610
0*4973
0*0330
0.0448
-0.0060
-0.2080
CHI -30.00
GAMMA- 1.5
ZETA* 0.70
X/H— 2.00
Y/H=
0.
Z/H= 0.
ETA= 1.00
(W.L)
f U.L )
(W.D)
(U.D)
-0.0089
0 ,0640
0.0579
0.6996
0*0091
0.1779
-0.0770
-0.0487
0.1346
0.1122
0.0750
-0.1400
-0.0207
0.1378
-0.0784
0.1586
-0.0641
-0.0784
0.1378
-0.0769
0.0118
-0.0738
0.1364
0.5409
0.0298
0.0401
0.0014
-0.2073
CHI *45,00
GAMMA* 1*5
ZETA =
0.70
X/Hs-2.00
Y/H*
0.
Z/H* 0,
ETA* 1.00
(W.L )
(U.L 1
(W.DI
(U.Ol
0*0174
0.0333
0.0475
0.6929
0.0280
0.145?
-0.0650
-0.0862
0.1388
0.0962
0.0442
-0* 1506
-0.0008
0.1085
-0.0697
0.1192
-0.0383
-0.0697
0.1085
-0.0801
0*0182
-0.0751
0.1172
0.5737
0.0287
0,0367
0.0046
-0.2054
CH I *60.00
GAMMA = 1.5
ZETA =
0.70
X/H=— 2.00
Y/H*
0*
Z/H= 0.
ETA= 1.00
(W.L)
(U.L1
(W.DI
(U.D)
0.0345
0*0047
0,0354
0,688?
0.0364
0.1179
-0.0621
-0.1150
0.1398
0.0702
0.0153
-0*1583
0.0068
0.0850
-0.0663
0.0883
-0.0195
-0.0663
0.0850
-0,0750
0.0277
-0.0803
0.1016
0.5999
0.0296
0.0329
0.0042
-0.2033
CHI *75.00
GAMM A = 1.5
ZETA*
0.70
X/Hs-2.00
Y/H-
0.
Z/H = 0.
ETA* 1.00
(W.L 1
(U.L)
(W.D)
(U.D)
0.0475
-0,0194
0.0226
0,6854
0.0371
0.0946
-0.0653
-0.1380
0.1377
0*0595
-0,0118
-0.1659
0.0043
0.0694
-0.0652
0.0640
-0*0058
-0.0652
0*0694
-0.0623
0.0432
-0.0080
0.0070
0.6213
0.0329
0.0252
-0.0001
-0.2020
CHI-90,00
GAMMA* 1.5
ZET A*
0.70
X/H=-2, 00
Y/H-
0.
Z/H* 0.
ETA= 1.00
(W.L)
(U.L)
(W.D)
(U.D)
0,0587
-0.0086
0,0086
0.6847
0.0326
0.0727
-0.0727
-0.1577
0.1323
0.0401
-0.0401
-0.1749
-0.0049
0.0643
-0.0643
0.0450
0*0049
-0.0643
0.0643
-0.0450
0.0636
-0.0729
0.0729
0*6397
0*0375
0 a 0084
-0.0084
-0.2027
6-t T £l-'I
17
TABLE 2.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR r - 1-5, ? = 0.70, AND 1J = 1.00
(b) x/H = -1.00
\
h
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
i ' T
GAMMA* 1.5
7FTA =
0.70
X/w=-l.nO Y/H* 0.
Z/H~ 0.
FT A = 1.00
< WtL)
(1/tL )
<WtD)
(UtOi
—0 * 5696
—0,7109
0 ,5087
0,5501
0,0056
-0.416?
0.3?5R
-0,0894
-0.4801
-0.1 874
—0,7.10°
0,7974
-0.071 5
0,7057
0,1830
-0,1 8 7°
-0.0400
-0*0876
0.3R34
-0,66*0
0, 3 5 5°
0,1707
0.1710
-0,4801
0 ,6049
n, *?68
0, 1 7 4f
GAMMA * 1 *J5
l ETA =
0.70
X / n = — 1 *00 Y/H = 0.
Z/H = 0. .
FT A: .1*00,
.. . _.
( WtL )
MJtL )
(W*0)
(U.Dl
-0.3712
0*1018
0,0608
0.4535
-0,069 8
0.4879
-0,4717
0,770*
0.441 *
0.142?
0,1185
-0,0086
-0.2469
0.310?
-0.3074
0,7783
—0 * 069 R
-0.3074
0.710?
0.0153
-0,1 ? 4 3
-0*2054
0,7681
0.1 ? 8 1
0,1770
0*17 7.7
-0,1 64*
- 0 . 1 n°o
Z FT A =
0.70
X /H = — 1
.00 Y/H= 0.
7/H= 0.
FT A* 1.00
CHI =30. OU
{WtL)
(U,L )
( to' t D )
(U ,D )
GAMMA = 1.5
-0 . 2 36*5
0.0474
0.0263
0.4413
0.3955
0.2085
-0,1337
0.7671
-0.0433
-0.7091
0.7671
-0.0614
-0*10?7
-0.?1 48
0.1 600
0*179?
-0.1 51 9
-0*1 5?*
0.1353
0.4818
-0,3610
0.0905
0 .0658
" -TOT971
-0.7091
0.7479
0*?^89
CHI =45,00
G A MM A = 1.5
Z FT A =
0,70
X/H=-l
,00 Y/H= 0.
7/H=_ 0*__.
FT A = 1.00
_ . . . - - - -
(WtL >
{U*L )
( W « 0 1
(UtD)
-0.1498
-0*0755
0,1716'
0,5011
0,0830
0.3919
-0.3030
-0,071?
0.3706
0.7751
-0,0047
-0.1557
-0,0669
0.7 0 6 *?
-0,1854
0.1 680
-0.0170
-0. 1 564
0 . 205?
-0.08??
-0.08?9
-0,?3OP
0 * 3 ? 70
0.3731
0, 1 409
0.1 "67
-0*1 476
-0. 1 8°?
CHI =60.00
GAMMA = 1.5
ZET A =
0.70
X/H=-l
lt 00 Y/H= 0,
Z/H= 0.
FT A = 1.00
(WtL 1
(U,L )
( W»0)
(UtD)
-0.0946
-D'. 1045
0.1894
0.5255
0.1069
0.3811
-n,7
-0.1151
0.3498
0,? 40 5
-0,0808
-0,1981
— C ,0367
0.1631
-0,1763
0,10mA
C .01 7°
-C.1768
0,1631
-0.0837
-0*0679
-0*’575
0,31 4?
0 • A 1 67
0, 1 436
0*1081
-0.1630
—0 • ? ? 3 P
CHI =75 , 00
GAMMA= 1,5
ZET A =
0. /o
X/H = -
l.CO Y/H® 0,
Z/H= 0.
FT A= 1.00
—
- -
(WtL 1
-0.0515
0.1049
0,3259
-0.0337
0.11*9
-0.1 105
0.0681
0.0314
-0.1105
0 . 1 1 6 9
-0.06?6
-0*01 7 R
-0*?936
0*1386
Q*2GLQ
1 U »L 1
( w * D )
( UtD )
-0.1776
0,7001
0.5604
0.3219
-0,281?
-0.1961
0,2369
-0,1845
-0.2399
0*3106
0.4953
-0*1 707
-0.7613
CH I *90,00
GAMMA = 1.5
Z F T A =
0,70
X /Ms —
1,00 Y/H® n.
Z/H= 0.
FT A= 1 .on
... _
(WtL)
( U t L )
( w,D)
( UtD )
-0.0046
-0.7056
0.2056
0.6067
0.0850
0.2988
-0,2988
-0,2727
0.294B
0,276?
-0.276?
-0*?920
-0.0439
0.0984
-0.0984
0.0344
7.0439
-7.0984
3,0984
-3.0744
0.0397
-0.3040
0*7040
0*8773
0.1289
0.20 04
-0.2004
-0.3071
18
TABLE 2.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.70, AND i j = 1.00
(c) x/H = y/H = z/H = 0
8
Correction factors for correcting from a wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
_
open
floor
only
closed
closed
on bottom
only
to free air
■j —■ 1 T ■ i
to grour
id effect
CHI *-3,00
GAMMA- 1,5
ZFT A»
0.70
X/H*
0. Y/H*
0.
Z/H* 0.
FTA* 1.00
IW.U
tu*u
tw*D)
(U.01
-1.3458
-0.0421
-0.768?
-0.7869
-0.2260
-0.0606
-0.9624
0,4046
—
2*1666
-0.6602
-0.0428
0,6625
-0.0150
-0.0618
-0,9533
0.0070
0, 9192
-0*9533 .
-0,0518
0,4070
-0.5309
0*009?
0*1851
-0*7939
0.5870
-0*0088
-0*0090
0*3976
CHI * 3.00
GAMMA* 1,5
2 FT A *
0.70
X/H=
0. Y/H-
0,
Z/H* 0.
FTA* 1.00
lw*L )
IU.U
-1.3458
0.0421
-0.2280
0.0606
1.9537
-0.6107
-0.8150
0,0518
0.7236
-0.9107
-0*5308
-0*0097
0.5870
0.0088
(W.D1
lUiOl
-0,7007
-0.6287
-0.9392
0,4795
0.0428
0.6625
-0.9107
0,1047
0.0510
0.4070
0.2099
-0,7334
-0*0285
0*3740
CHI *15 #00
GAMMA* 1.5
“ZETA*
0.70
X/H*
0, Y/H*
0.
Z/H* 0.
FTA* 1,00
fW.Ll
(U it J
-1.2663
0.1673
-0.1296
0.2832
1.5785
-0.4076
-0*7280
0.2376
0.4102
-0.7536
-0*5403
-0.0503
0*5983
0*0456
fW.Dl
fU,D)
-0.4997
-0.3840
-0.8182
0.5717
0*1 908
0.5930
-0.7536
0.2396
0.2376
0.3352
0.2538
-0.6236
-0*0646
0.3321
CHI-30.00
GAMMA- 1.5
?ET A*=
0 *70
X/H*
0, Y/H*
0.
Z/H* 0,
FTA* 1.00
IW*LI
IU.U
-1.0619
0,2487
0.1228
0.4614
1.3040
-0,1159
-0.5118
0.3606
0.1901
-0,5126
-0.5701
-0.1119
0.6346
0*1009
IUiOI
-0.2074
-0.2287
-0 .6237T
0.5574
0,2566
0.4283
-0.5126
0.2736
0.3606
0.1650
0.3052
-0.5023
-0*1105
0*2838
CHt«45.00
GAMMA* 1.5
ZFT A*
0.70
X/H-
0, Y/H*
0.
Z/H* 0.
FTA- 1,00
IW.L 1
Ol.L)
fW.D)
IU*01
-0.9107
0,1414
0,0427
-0.1888
0.4040
0.5190
-0.4885
0.4426
1.2035
0.1289
0.1559
0.2750
-0.2924
0,3409
-0,3208
0.2039
0,1187
-0.3208
0.3409
0.0100
-0,6103
-0*1995
0.3636
-0,3927
0*6964
0*1781
-0*1677
0*2387
CHI -60.00
GAMMA* 1.5
ZET A =
0.70
X/H*
0. Y/H*
0.
Z/H- 0.
ETA- 1.00
IW*L)
1 U*L )
-0,8353
-0,0880
0,6199
0.5356
1.1937
0.3071
-0.1608
0,2448
0.1129
-0^?Q28
-0.6745
-0.3328
0.7807
0*2908
" fW.DI
01*0)
0,2345
-0.1742
-CT,46T5 _
0.2995
-0.0635
0 * 1M 9
-0*2098
0.1100
0,2448
“0,0536
0.4444
-0.2843
-0.2536
0*1895
CHI -75 . 00
GAMMA* 1,5
ZFT A*
0.70
X/H-
0, Y/H-
o*
Z/H- 0.
FTA* 1.00
rw*u
lU it 1
(W.D>
IU.D)
-0.8284
-0,3632
0.4120
-0,1195
0.7536
0.5979
-0.5460
0.1601
1.2136
0.4580
-0.3301
0.1219
-0.1201
0,1600
-0.1527"
0.0407
0.1165
-0.1527
0.1600
-0,0366
-0.7087
“0,5232
0.5647
-0.1602
0,0737
0.437 B
-0.3932
0.1193
CHI -90.00
GAMMA* 1,5
Z FT A*
0,70
X/H*
0* Y/H*
0.
Z/H- 0.
FTA- 1.00
fWtll
(U.L1
-0,8169
-0,6113
0*0350
0.7225
1*2360
0.6249
-0.1170
0.1170
0.1170
-0.1170
-0.6999
.-0,720?
0.9520
0*6055
(U.O)
0.6113
-o.onfto
-0.7225
0,0000
-0.6249
0.0000
-0,1170
-0.
0.1170
0.
0,7287
-0.0000
“0. 605*’
0.0000
6 ^ 1-1
L-15^9
19
TABLE 2.- Continued
longitudinal distribution of interference factors for V = 1.5, c = 0.70, AND t> = 1.00
(d) x/H = 1.00
s
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CHI- 0 •
GAMMA- 1.5
ZETA* 0.70 X/H-
1.00 Y/H= 0.
Z/H* 0.
ETA = 1.00
( W »L )
(U.L)
( W » D )
(U.D)
-0*5696
-0*1149
-0.6453
-1.0600
-0*2109
-0.5037
-0.3553
-0.116?
2.7865
-0.5784
-0.1307
0.1210
-0.4162
-0.3258
-0.5490
-0.3154
1.7343
-0. 5490
-0.3258
0.1245
-0.1534
0.2108
-0.0963
-0.7445
0.2057
-0.1830
0*1936
0.1992
CHI -15*00
GAMMA- 1.5
ZETA* 0.70 X/H*
1.00 Y/H- 0.
2/H* 0.
ETA” 1.00
( W.L )
t U »L )
(W.D)
IU.D)
—0 *8366
-0*0500
-0.7714
-0.9560
-0.3825
-0.4473
-0.4844
0*0330
2.4892
-0.6960
-0.0659
0*2531
-0.6378
-0.2622
-0.6870
-0.21 57
1.4477
-0.6870
—0.26??
0. ?707
-0.2008
0.2114
-0.0843
-0.7403
0.2553
-0*1851
0.2026
0*7406
CHI -30*00
GAMMA- 1.5
ZETA- 0.70 X/H*
1.00 Y/H* 0.
Z/H= 0.
ETA= 1.00
< W »L )
(U.L)
(w*0)
(U.D)
-1.1091
0.1902
-0.7908
-0.7011
-0.5003
-0.2613
-0.5310
0.1784
2.0746
-0.7071
0.1761
0.451 1
-0.8355
-0.0480
-0.7287
-0.0398
1.0207
-0. 7?87
-0.0480
0.3917
-0.2736
0.238?
-0.0671
-0.6614
0*335?
-0.2133
0.1977
0.218?
CHI-45.00
GAMMA- 1*5
ZETA* 0.70 X/H*
1.00 y/h= 0.
Z/H= 0*
ETA= 1.00
(W.L)
(U.L)
(W.0I
(U.D)
-1.1778
0.5222
-0.6242
-0*5083
-0.2831
0.0444
-0.3594
0.3539
1.6532
-0.5331
0.5110
0.4277
— 0.76R6
0.2724
-0.5671
0.1215
0.5535
-0.5671
0*2724
C.3039
-0.4092
0.2498
-0*0571
-0.6299
0.485*
-0.7280
0*2077
0.2323
CHI-60.00
GAMMA- 1*5
ZETA- 0.70 X/H*
1*00 Y/H- 0.
Z/H* 0.
ETA* 1.00
( W.L )
(U.L)
(WtO)
I U ♦ D )
-1*0641
0.5330
-0*3455
-0.5168
0.3446
0.1254
-0.1004
0.3598
1.5277
-0.2530
0.5324
0.269?
-0.414?
0.3748
-0.3039
0.0974
0.3041
-0.3039
0.3240
0.0463
-0.6499
0.2007
-0.0416
-0.6143
0.7588
-0.1994
0.2035
0.2623
CHI -75.00
GAMMA- 1*5
ZETA- 0.70 X/H*
1.00 Y/H* 0.
Z/H- 0.
ETA- 1.00
(W.L)
(UtL)
IW.D)
(U.D)
-1.2291
0.1958
-0.1152
-0.6000
0.9490
0.1111
-0.0548
0.3118
1.7229
-0*0457
0.2185
0 . ? 09 4
-0*2360
0.1742
-0.1641
0.0080
0.2299
-0. 1641
0.1742
-0.0006
-0.9930
0.0216
0.0489
-0.6079
1.1850
-0.0631
0.1093
0.3038
CHI -90.00
GAMMA- 1.5
ZETA- 0.70 X/H*
■ l.<Vb Y/H- 0.
Z/H- O.
ET 4= 1.00
(W.LI
(U.L )
(W.D)
(U.D)
-1.6292
-0.2056
0.2056
-0.6067
1.5850
0.2988
-0.2988
0.2727
2.1772
0.2262
-0.226?
0.2920
-0.1900
0.0984
-0.0984
-0.03*4
0.1900
-0.0984
0.0984
0.0344
-1.4392
-0.3040
0.3040
-0.5723
1.7750
0.2004
-0.2004
0.3071
20
TABLE 2.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > - 1.5, C = 0.70, AND 1J = 1.00
(e) x/H = 2.00
s
Correc
Non factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
{ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
T 1 1
1
CH I - 0*
GAMMA = 1,5
ZETA* 0.70
X/H* 2.00
Y/H* 0.
Z/H* 0*
ETA- 1.00
(W.L)
<U«L)
(W,D>
(U.D)
-0.1188
-0.1283
-0.2756
-0.9125
-0.0802
-0.2647
-0.1480
-0*1406
2.8449
-0.2272
-0*1406
-0.0961
-0.1194
-0.2122
-0.2288
“0.2361
1.8903
-0.2288
-0,2122
-0,0373
0.0006
0.0840
-0.0469
-0.6764
0.0392
-0.0525
0.0808
0.0955
CHI *15*00
GAMMA- 1.5
ZETA* 0.70
X/H* 2.00
y/h- o.
Z/H* 0.
ETA- 1.00
(W*l)
(U#L)
(W.D)
(U.D)
-0.2350
-0,1566
-0.3557
-0.9132
-0.1753
-0.3225
-0.2259
-0.1453
2.7547
-0.3020
-0.1708
-0.0577
-0,2261
-0.2544
-0.3147
-0.2431
1.8099
-0.3147
-0.2544
0.0128
-0,0089
0.0976
-0.0410
-0.6700
0.0508
-0.0681
0.0888
0.0978
CHI *30.00
GAMMA- 1,5
ZETA- 0.70
X/H- 2.00
Y/H- 0.
Z/H- 0.
ETA- 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-0.4431
-0,1556
-0.4557
-0.8757
-0.3411
-0.3702
-0.3163
-0.1070
2.5881
-0.3952
-0.1725
0.0472
-0.4170
-0.2815
-0,4199
-0.2231
1.6481
-0,4199
-0*2815
0. 1093
•0,0260
0.1259
-0.0358
-0.6526
0*0759
-0*0887
0.1036
0*1161
CHI *45 * 00
GAMMA- 1.5
ZETA* 0.70
X/H- 2.00
y/h* o.
Z/H- 0.
ETA- 1.00
( W »L )
IU.L I
(W.D)
(U.D)
-0.8199
-0.0169
-0.5722
-0.7690
-0.6083
-0.3269
-0.3968
-0.0135
2.2444
-0.5019
-0.0362
0,2292
-0,7460
-0.1939
-0.5267
-0.1335
1.2981
-0.5267
•0.1939
0.2860
-0.0739
0.1770
-0.0455
-0.6355
0,1378
-0.1330
0.1299
0.1200
CHI-60,00
GAMMA- 1.5
ZETA= 0.70
X/H- 2.00
Y/h* 0*
Z/H- 0.
ETA= 1.00
tw.u
(U.U
(W.D)
(U.D)
-1.0561
0,4966
-0.5047
-0.5739
-0.4884
0,0355
-0,2403
0.1721
1*6654
-0.4196
0.4724
0.2647
-0.8199
0.2406
-0.4239
0.0458
0.6634
“0*4239
0.2406
0.2691
-0.2362
0,2560
-0.0009
-0.6197
0.3315
-0.2052
0.1836
0. 1263
CHI-75.00
GAMMA- 1.5
ZETA= 0.70
X/H* 2.00
Y/H- 0.
Z/H- 0,
ETA* 1.00
(W.L)
(U.L )
(W.D)
(U.D)
-1.0271
0.3799
-0.2647
-0.6335
0.5162
-0,0156
0.0640
0.1583
1.612 2
-0*1786
0.3801
0.1336
-0.3507
0.1729
-0.1585
-0.0050
0.3390
-0. 1585
0.1729
0.0195
-0.6764
0.2070
-0.1062
-0.6285
0*8670
-0.1885
0*2225
0*1633
CHI -90,00
GAMMA- 1.5
ZETA= 0.70
X/H* 2.00
y/h- 0.
Z/H- 0.
ETA* 1.00
(W.L >
(U.L)
(W.D)
(U.D)
-1 .6925
-0,0086
0.0006
-0*6847
1.6373
0.0727
-0.0727
0.1577
2.3397
0.0401
-0.0401
0*1749
-0.2291
0.0643
-0.0643
-0.0450
0.2291
-0.0643
0.0643
0.0450
-1,4634
-0.0729
0.0729
-0.6397
1.8664
0*0084
-0,0084
0,2027
6 ^ 1-1
L-15^9
21
TABLE 2.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, 5 = 0-70, AND 1 = 1.00
(f) x/H = 3 .00
Correction foctors for
correcting from
a wind tunnel
which is
close d
closed floor
open
closed
s
closed
on bottom
open
only
floor
closed
on bottom
only
{ground effect)
only
only
to free air
to ground effect
CH I 3 0.
h“ t
GAMMA= 1*5 ZcTA = 0*70 a/H= 3*00 f/ri=
0.
a/h = 0.
E T A = 1*00
<WiL 1
1 U * L )
1 In »D )
1 U*D 1
-U,u231
-0.0873
-0.1431
-0.7759
-O . i*2 34
-0*122i
—0*0637
-0* jaou
2.6511
-0.1030
-0.0913
-0.0349
—0 . o 3 6 0
-0.1159
-0. i 147
-0.130/
1.3936
-0*1147
-0.115V
- • j • 0 3 2 l
0*0129
0 • C2 06
-0*0235
-0*o2 32
0 • 0 I20
—0* 0 Co 2
0*0310
0*0626
CH 1 -15*00
li«MMA= 1.5
*-£T A = u*70 a
' n j • 0 O' Y / n =
V.
L/r 1 = s. *
ETA- 1.00
( Wf L 1
( U i L )
(UtO)
-0.08 08
— U . 1 466
-0.1552
-0.1629
1.8 668
-0.1552
-0 • 1466
-0*0396
CHI =30*00
GAMMA= 1.5
ZETA = 0*70 a
/h= 3.00 Y/H*
0.
Z/H® 0.
E‘A= 1.00
( W *L )
( U » L )
( W » D )
( U »D )
-0.1530
-0.1422
-0.2268
-0.8042
-0*1450
-0*2042
-O *1657
-0*0683
2 . 7 40 7
-0.1635
-0.1501
-U * 0 56 b
-0.1658
-0.1878
-0*2092
-u • 1 7 u2
1.6010
-0*2092
-0.1878
■*0 .0136
0*0x26
0 » 0*00
-0*0196
— 0 a 6340
0* 0209
-0*0164
0*0435
0*0619
CHl=45.0G
GAMMA'-' -.3
j.'.j
/h - 3. CO Y/h-
C 4
4/h^ 0.
E I A= 1*00
1 W t L )
1 U *L )
(W»0>
(U»0 J
-u. 3489
-0.1615
-0.3141
-0.7937
-0*3213
-0*2665
-0*2369
-0*0735
2.5895
—0 . 2 6 3 8
-0.1739
-0.0116
-0.3576
-0.2333
-0.2940
-0.1604
1.6540
-0.2940
-0.2333
0. 0477
O.OC37
0.0717
-0.0200
-0.6334
0*0364
-0*0336
0*0b51
0*0863
CH 1=60*00
GAMMA= 1.5
ZcT A- 0*70 a
/h= 3.00 Y/h* 0.
Z/H- ^
, E T A= 1.00
( W *L )
( U * L )
( W»D)
<U.D)
-0.8550
-0.0059
-0.4347
-0.7168
-0.7134
-0*2424
-0.3118
-0*0054
2.1446
-0.3726
-0.0287
0.1891
-0*8202
-0.1527
-0.3982
-0.0907
1.2023
-0. 3982
-0.1527
0.2632
-0*0348
0.1469
-0.0365
-0*6261
0*1069
-0*0896
0*0864
0*0o53
CH I = 75 • 00
GAMMA- 1.3
2ETA= 0*70 A/H= 3.00 Y/H
■ 0.
2/H = 0. ETA= 1.00
(W»U
MJ.L)
(W.D)
I U f D t
-0.8969
0.4121
-0.2666
-U.6255
0*1042
0*0161
0*0124
0*0933
1.5612
-C.1816
0.3931
0.C595
-0.4791
0.1826
-0.1634
-0.0005
0.4534
-0. 1634
0* 1826
0.0337
-0*4178
0*2295
-0.1032
-0*6251
0*5633
-0*1665
0*1756
0*0936
CHI *90 • 00
6AMMA= 1.5
ZETA= 0.70 X/H = 3*00 Y/H
= 0.
Z/H= 0
. fcTA* 1*00
(M*L)
1 U * L I
1 W »D »
(U.D)
-1.6764
0.0281
-3*0281
-0.6835
1.6398
0.0184
-0.0184
0*0865
2.3868
O.O090
—0 • 0090
0.0975
-0*2420
0*0384
-0*0384
-0*0403
0.2420
-0.0384
0.0364
0.0403
-1 • 4344
-0*0i03
0*0103
-0 • 0432
1*3617
-0*0200
0*0200
0*1263
22
TABLE 2.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C * 0.70, AND 7] = 1.00
(g) x/H = 4.00
Correction foctors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI* 0*
GAMMA * 1*5
ZETA-
0.70
X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA* 1*00
(WtL)
<U»l>
(W,D)
(U»D)
-0*0043
-0.0571
-0*0928
-0.6756
-0.0064
-0*0646
-0*0535
-0.0566
2.8537
-0.0566
-0.0575
-0.0565
-0.0126
-0.0675
-0*0678
-0.1017
1*8939
-0*0678
-0.0675
-0.0416
0.0083
0.0105
-0.0250
-0.5739
0.0062
0.0029
0*0143
0.0452
CHI -15*00
GAMMA* 1.5
ZETA-
0.70
X/H* 4.00 Y/H* 0*
Z/H* 0.
ETA* 1.00
1 W *L 1
IU»L)
(W.D)
<U»D)
-0.0359
-0.0663
“0*0899
-0.1099
1*8768
“0*0099
“0.0863
“0*0380
CHI -30*00
GAMMA- 1*5
zeta-
0.70
X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA* 1*00
(w*U
(U*l )
(WtD)
(U.D)
-0*0798
-0.1131
-0.1195
“0*1166
1*8411
-0*1195
“0*1131
“0*0306
CHI *45.00
GAMMA- 1.5
ZETA-
0.70
X/H* 4.00 Y/H* 0.
Z/H* 0*
ETA- 1*00
IW.L)
(U.LI
1 W »D 1
IU.DI
-0.1766
-0*1553
-0*1646
-0.1209
1.-7590
“0. 1646
“0*1553
“0*0120
CM I >60*00
GAMMA- 1*5
ZETA*
0*70
X/H* 4.00 Y/H* 0*
Z/H- 0*
ETA* 1.00
<W»L)
(U.D
(W.D)
(U.D)
-0*4508
-0*1572
-0*2697
-0*7197
-0.4319
-0*2357
-0*2116
-0*0471
2.4603
-0.2242
-0.1674
0.0097
“0*4650
“0*2176
“0*2488
-0.1134
1*5152
“0*2488
“0*2176
0*0660
0.0143
0*0604
“0.0209
-0.6063
0.0331
-0.0181
0.0369
0.0663
CHI *75*00
GAMMA- 1.5
ZETA-
0*70
X/H* 4*00 Y/H* 0*
Z/H- 0*
ETA- 1.00
( W.L)
(U.D
(M.D)
(U.D)
-0.8849
0.4062
-0*2634
-0*5944
-0.3211
0.0703
-0*0785
0*0680
1*6190
-0*1925
0.3787
0.0551
-0*6675
0*1979
-0 * 1897
0*0077
0*6060
“0. 1897
0*1979
0*0806
-0.2174
0.2083
-0.0737
“0.6021
0*3464
-0.1276
0.1113
0.0603
CHI -90*00
GAMMA- 1.5
ZETA-
0*70
X/H* 4.00 Y/H* 0«
Z/H* 0*
ETA* 1*00
IW.D
(U.L)
(M.D)
(U.D)
-1.6615
0.0337
-0.0337
-0,6524
1.6461
0*0046
-0*0046
0.0542
2.4091
0.0041
-0.0041
0.0586
-0*2443
0*0230
-0*0230
-0*0322
0*2443
-0.0230
0*0230
0*0322
“1*4172
0.0107
“0*0107
-0.6203
1*8904
“0*0183
0*0183
0*0864
6t£ 1-1
L-15^9
25
TABLE 2.- Continued
LONGIT UDINAL DISTRIBUTION or INTERFERENCE FACTORS FOR V - !•».
(h) x/H = 5.00
= 0.70, AND tj = 1.00
Correction factors for correcting from o wind tunnel
which is
s
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
—
i —
CH I ■* 0,
GAMMA * 1*5
ZETA- 0.70 X/H* 5.00 Y/H* 0.
iu.i | -Q .0006
(U.L I -0.0389
( W » D ) -0.0686
( U * D ) -0.5983
-0.0017 2.8558
-0*0396 -0.0353
-0.0363 -0.0378
-0.0388 -0.0377
Z/H = 0.
-0.0051
-0.0429
-0.0444
-0.0729
iiTA* 1.00
1.8893
-Q.Q444
-0.0429
-0.0310
0.0045
0*0040
-0.0242
-0.5254
0.0034
0.0034
0.0081
0.0340
ChI-15.00 GAMMA* 1.5 ZET A
(W.L) -0.0142
(U.L) -0.0502
(W.D) -0.0810
(U.D) -0.6175
0,70 X/H= 5.00 Y/H- 0.
-0.0155 2.8416
-0.0515 -0.C468
-0.0481 -0.0492
-0.0389 -0,0375
Z/H* 0.
-0.0193
-0*0550
-0.0580
-0.0782
ETA= 1.00
1.8784
-0.0580
-0.0550
-0.0298
0.0051
0.0048
-0.0230
-0.5393
0.0038
0.0035
0.0099
0*0393
CHI-30.00 GAMMA* 1.5
ZETA= 0.70 X/H* 5.00 Y/H* 0.
IW.LI
(U.L)
(W.D)
(U.D)
-0.039B
-0.0664
-0.0984
-0.6336
-0.0413
-0.0687
-0.0646
-0.0393
2.8162
-0.0634
-0.0655
-0.0373
Z/H* 0.
-0.0459
-0.0725
-0.0764
-0.0827
ETA* 1.00
1.8557
-0.0764
-0.0725
-0.0273
0.0061
0.0061
- 0.0220
-0*5609
0.0046
0.0038
0.0116
0.0434
CHI-45.0U GAMMA- 1.5
ZETA* 0.70 x/H- 5.00 Y/H- 0.
(W.L)
(U.L)
(W.D I
(U.D)
-0.0956
-0.0909
-0.1253
-0.6465
-0.0974
-0.0962
-0.0907
-0.0389
2.7616
-0*0894
-0,0904
-0.0357
Z/H= 0.
-0*1042
-0.1007
-0.1046
-0.0B64
eta* 1.00
1,8037
-0.1046
-0. 1007
-0.0213
0.0086
0.0098
-0.0208
-0.5601
0.0066
0*0045
0*0139
0.0475
CHI -60.00
I Vi » L )
(U.L)
(W.D)
(U.D)
GAMMA- 1.5
ZETA- 0.70 X/H* 5.00 Y/H* 0.
2.0409
-1.4581
1*1471
-1.4193
2.0402
-1.4773
1.1854
-0. 8006
0.3044
1.1848
-1.4597
0.7364
Z/H- 0.
2.0266
-1.4806
1.1674
-0.8510
ETA- 1.00
-0.6512
1.1674
-1.4806
0.7652
0.0142
0*0225
-0.0203
-0.5683
0.0136
0*0033
0.0179
0.0504
CHI -75.00 GAMMA- 1.5
ZETA- 0.70 X/H* 5.00
(W.L)
(U.L)
< W *0 )
(U.D)
-0.9825 -0.7518
0,2518 0*0232
-0.2739 -0.1714
-0.5743 0.0377
1.8152
- 0.2201
0.2289
0.1373
Z/H- 0.
-0.9131
0.1005
-0.2289
-0.0060
ETA- 1.00
0.8432
-0.2289
0.1005
0. 1963
-0.0693
0.1513
-0.0449
-0.5683
0.1613
-0.0772
0.0575
0.0437
CHI-90. 00 GAMMA- 1*5 ZETA-
(W.L) -1.6520
(U.L) 0.0332
(W.D) -0.0332
(U.D) -0.6086
0,70 X/H* 5.00 Y/H- 0,
1,6524 2.4216
0,0010 0*0033
-0.0010 -0,0033
0.0355 0.0382
Z/H* 0.
-0.2435
0*0143
-0*0143
-0*0250
ETA* 1*00
0*2435
-0*0143
0*0143
0 . 0?*>0
-1.4084
0.0189
- 0. n ' °9
-0.5836
1*8959
-0*0133
0*0133
0*0605
2k
TABLE 2.- Concluded
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 0.70, AND rj = 1.00
(i) Miscellaneous additional values of x/H
$
Correc
tion factors for correcting from a wind tunnel which is 1
closed
close d
on bottom
f only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
1
1
CHI-15. 00
GAMMA- 1,5
ZETA-
0*70
X/H- 0,38
Y/H= 0,
Z/H= 0.
ETA- 1.00
(W.L)
fU.L )
fWfD)
itl»D 1
-1,3046
0,1785
-0,7960
-0,6773
-0*2894
-0*1060
-0*7230
0*3992
2,0246
-0.7076
0.1734
0*6190
-0.8258
0,0315
-0,8423
0.0537
0. 8227
-0.8423
0*0315
0*4075
-0*4787
0.1470
0,0464
-0.731 1
0,5364
-0.1384
0.1193
0*4455
CHI-30,00
GAMMA- 1,3
ZETA-
0.70
X/H- 0.83
Y/H= 0.
Z/H- 0.
ETA- 1.00
( W * L 1
(U.L)
fW*D)
tU.Dl
-1,2000
0.2841
-0,7857
-0,6350
-0.4322
-0,1622
-0*5448
0*2839
1 .9496
-0.6987
0.2728
0.5112
-0.0475
0*0510
-0*739?
0*0315
0*8525
-0.7392
0. 0510
0,4007
-0*3525
0* ?331
-0*0465
-0.6673
0*4153
-0,213?
0*1944
0*2524
CHI-45.00
GAMMA- 1.5
ZETA-
0.70
X/H- 1.43
Y/H- 0.
Z/H= 0.
ETA- 1,00
<W*L)
<u*n
(WiD)
(U»0)
-1 • 1054
0.3092
-0,6826
“0,6226
-0*5870
-0.1457
-0.4217
0.1702
1.8881
-0.5988
0,2903
0.3947
-0*8823
0*0640
-0*6130
0*0052
0.8834
-0.6130
0 , 0640
0.3821
-0.2231
0.2453
-0*0697
-0.6277
0*2953
“0*2097
0*1913
0*1650
CHI "60*00
GAMMA* 1.5
ZETA-
0.70
X/H- 2.48
Y/H- 0*
Z/H- 0*
ETA- 1.00
fW.L)
(U.L)
IWtD)
tU.D)
-1*0363
0,2557
-0.5033
-0.6474
-0.7244
-0,1013
-0.3138
0.0784
1.8849
-0*4290
0.2293
0*2785
-0*9228
0*0482
-0*4462
-0*0221
0.9259
-0.4462
0*0482
0.3332
-0.1135
0.2076
-0.0571
-0,6253
0*1984
-0*1494
0.1324
0*1005
CHI-75,00
GAMMA- 1,5
ZETA-
0.70
X/H- 3*90
Y/H- 0,
Z/H- 0*
ETA- 1.00
IW.LI
1U*L1
(W.D)
(u* 0 )
-0,0797
0.4098
-0,2629
-0,5978
-0.2762
0,0659
-0,0686
0.0699
l*607fe
-0*1903
0,3826
0,0515
-0*6444
0*1978
-0.1860
0,0072
0*5878
-0.1860
0* 1978
0*0727
-0,2353
0.2120
-0.0769
-0.6050
0*3682
-0*1319
0*1175
0*0627
6+£T- r l
L-15^9
25
TABLE 3
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 0.80, AND 0= 1-00
(a) x/H = -2.00
s
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
1
to free air
1 — p
to ground effect
■ 1 i ■
CHI* 0.
GAMMA- 1.5
ZETA*
0,80
K/H—2.00
Y/H* 0,
Z/H* 0.
ETA- 1.00
(WtL)
(UtL)
( WtD )
(UtD)
-0.1198
0.1749
0.0214
0.7301
-0,0727
0.2647
-0.1190
0.1344
0.0944
0.0895
0*1812
-0.0952
-0,1092
0.2330
-0.1238
0.3116
-0.1781
-0.1238
O. 2330
-0.0629
-0.0106
-0.0581
0.1452
0.4185
0.0365
0.0317
0*0048
-0.177?
CHI-15.00
GAMMA" 1.5
ZETA*
0.80
X/H*— 2 . 00
Y/H- 0.
Z/H- 0.
ETA- 1.00
( WtL )
(UtL)
(WtD)
(UtO)
-0.0541
0.1323
0,0334
0,7093
-0.0154
0.2155
-0.0008
0.0550
0.1179
0.0943
0.1385
-0*1193
-0,0477
0 • 1874
-0.0912
0.2367
-0.1205
-0.0912
0.1874
-0.0855
-0.0064
-0.0548
0*1246
0.4726
0*0323
0.0281
0.0104
-0*1 81 7
CHI-30.00
GAMMA" 1*5
ZET A"
0.80
X/H--?. 00
Y/H- 0.
Z/H- 0.
ETA* 1.00
(WtL)
(UtL)
(WtD)
(UtO)
-0.0146
0.0945
0.0321
0.6931
0.0188
0.1755
-0.0640
-0.0013
0.1336
0*0867
0.1003
-0.1329
-0.0118
0.1494
-0.0770
0 • 1 817
-0*0797
-0*0770
0. 1494
-0.0959
-0.0028
-0.0549
0.1091
0*5114
0.0306
0.0261
0.0131
-0*1829
CHI *45.00
GAMMA- 1.5
ZET A"
C.80
X/H--2.00
Y/H* 0*
Z/H* 0,
ETA- 1.00
(WtL)
(UtL)
(WtD)
(UtD)
0*0089
0.0597
0.0254
0.6807
0*0384
0,1429
-0.0584
-0.0431
0,1431
0.0741
0.0657
-0.1406
0.0077
0.1180
-0,0718
0.1394
-0*0504
-0.0718
0.1180
-0.0975
0.0012
-0.0583
0.0971
0.5412
0.0307
0*0249
0.0133
-0.1826
CHI *60.00
GAMMA" 1.5
ZETA*
0.80
X/H--2.00
Y/H- 0.
Z/H* 0,
ETA* 1.00
(WtL)
(UtL)
(WtD)
(UtD)
0,0222
0*0276
0.0167
0,6714
0.0476
0.1167
-0,0599
-0.0755
0.1479
0.0595
0.0335
-0.1450
0.0148
0,0933
-0.0710
0.1061
-0.0291
-0.0710
0.0933
-0.0914
0.0074
-0.0657
0.0877
0.5653
0.0328
0.0234
o.oni
-0*1816
CHI -75.00
GAMMA" 1.5
ZETA*
0.80
X /H* -2 • 00
Y/H- 0*
Z/H- 0.
ETA- 1.00
(WtL I
(UtL)
(WtD)
(UtD)
0.0305
-0.0011
0,0080
0*6650
0.0489
0,0956
-0.0663
-0.1010
0.1486
0.0439
0,0034
-0*1488
0.0115
0 1 0771
-0.0720
0.0795
-0.0134
-0.0720
0.0771
-0.0775
0.0190
-0*0781
0.0800
0.5856
0.0374
0.0185
0.0056
-0.1805
CHI*90.00
GAMMA- 1,5
ZETA*
0.80
X/H*— 2,00
Y/H* 0.
Z/H- 0.
ETA= 1.00
(WtL)
(UtL)
IWtDI
(UtD)
0.0378
0.0010
-0.0010
0.6615
0.0440
0,0767
-0.0767
-0.1223
0.1456
0,0280
-0.0280
-0,1544
0.0009
0.0727
-0.0727
0.0582
-0.0009
-0.0727
0.0727
-0.0582
0.0370
-0.0717
0.0717
0.6033
0 1 0440
0.0040
-0,0040
-0.1805
26
TABLE 3.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 0.B0, AND Tf = 1.00
(b) x/H = -1.00
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
ciosed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
CHI* 0. GAMMA* 1*5
ZFTA* 0*80 X/H = -U 00 Y/H * 0.
Z/H* OV
FT A* 1.00
-0.5706 -0.3170 0.4146 -0.4597 -0.1291
( 0 *L ) 0.3060 0.5046 -0,186 0 _ 0.4167 -0.5331
(W»BT~ — 0 . 2 ^92 -0.6026 0,3l43 —0.5331 0.4i&7
0.5185 0.4886 0.1240 0.5196 0.1095
-0.1109 0.1427
-0*110 7 0.0870
0,2539 -0.069A
-0.0011 -0.0310
CHI *15.00
GAMMA = 1.5
2ETA* 0.80
X/H*-]
L .00
Y/H*
- fW.U
-0.3625
“ ' -0.1342
0,3631
(UtLI
0.2658
0.4666
-0.0170
(W,D)
-0.1033“
-0.405C
0.2746
UJ.D)
0.5227
0.3343
-0.0063
CHT-30.00
GAMMA* 1.5
2FT A= 0 * 8 n
X/H=-l
.00
Y / H=
rffTLT
-0.2292
-0.0135
0.3554
IU.U
0.1933
0.4061
0.0685
rwrm
-0.0099
-0.2974
0.2030
1U.D1
0.5045
0.1940
-0.0870
0.
Z/H = 0.
eta* l.on
-0.2647
-0.1119
-0.0978
0.1 306
0.3787
-0.3425
— 0 . 1 1 ?9
0.0879
-0.3425
0,3787
0.2393
-0.0626
0.4085
-0,0107
0.1142
-0.0742
0 .
?/H = 0*
FT A= 1,00
-0,1393
-0.0680
-0*0899
0.1268
0.3142
-0.2379
”0 . 1 ?09
0.091 9
-0.2379
0.314?
0.??80
-0.0596
0.3006
-0.0806
0.2039
-0.1066
CHI =45 .00
GAMMA* 1.5
2 FT A= 0,80
X/H=-l
.00 Y/H* o.
7 /H= 0.
FT a* i,nn
(W,L)
(U.U
-0.1510
0.1089
0,0601
0,3456
0.3573
0,108?
-0.0668
0.2455
-0.0257
-0.1818
-0.0842
-0.1 366
0,1 260
0. 1 001
{ V » D )
fU.D)
'"0.0392
0.4881
-0,2431
0.0774
0.1261
-0,1318
-0.1818
0.2103
0.2455
-0,1109
0.2210
0.2779
-0.061
-o.l 328
CHT ■ 6TT. CTO —
“GAMMA* T. 5
ZFTA= 0.80
X /H=— 1
.00 Y/H* 0,
Z/H= 0.
FT A= 1.00
(W.L1
<U*L1
-CT.TII4
"0,0216
CY0979
0.3570
-0,0350
0,0074
-0.0764
0. 1 329
0.2971
0,1240
0.1847
-0.1520
-0.1631
0.1124
IwTBl
Rl,D>
0,0671
0.4820
-0,2223
-0.0167
0.0?49
-0.154?
-0,1 5?~0
0.1394
0.1847
-0. 1093
0.2191
0.3426
-0x5703
-0, 1 561
-It 7\rt
GAMMA* 1.5
ZETA* 0.80
X/H = - 1
.00 Y/H* 0.
L n i * t z> 0 UU
Z/H*. 0 ,
ETA* 1.00
(W.Ll
-0,0907
0 • 1090
0.3506
-0.0334
0.0305
-0.0573
0.1424
(U*L)
-0,0618
0,2659
0.1287
0,1419
-0.1351
-0.2037
6,1730
? w75 )
(U *D )
— 0.0883
0.4890
-0,2251
-0,0928
-0.0477
— 0. i 7 1 1
-0.1351
0.0867
0. 1419
-0.0836
0*2234
0,4023
-0,0900
-0.1 796
CHI *90,00
GAMMA* t ; T
"2 ETA* 0,85
X/H=-l
•CO Y/H* 0.
Z/H= 0.
FTA* 1.00
(W.L)
IU.L)
-0,0'663
-0.1078
5,1029
“”6.3 364
-0.0471
0.0471
-0.0191
0,1500
0.2457
0.1290
0.1223
-0*1223
-0.2300
0,1234
fwTDT
(U»D)
0.1078
0.5091
-0.2457
-0.T583
-0.1290
-0, 1223
0.1223
0.2300
-0.1234
-0.197“9 "
0.0489
-0.0489
0.4602
-0.207?
6^1-n
L-15^9
27
TABLE 3. - Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1-5. C - »J», AND i, = 1.00
(c) x/H = y/H = z/H = 0
8
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
f W * u
!UtLI
( W » D )
(U.D)
GAM«A= i.6 ?ETA=
O.tjO x/H* 0*
Y/H* C.
-1,3252
— 0 , 063 B
-1,0980
-0,5746
“0,7703
-0,0 roy
-1.2331
0.2602
2.13(1
-1.00o5
-0.0642
0.6519
Z/H =
0.
-1.0645
-0.0677
-1.2451
0.0091
ETA= 1.00
1.2006
-1.245 1
-0.0677
0.5315
-0.2607
0.0039
0.1471
-0.5838
0.2941
-0.003?
0.0098
0.2511
CHI* 3.00 GAMMA = i.5 ZETA= C.oO
X/H = 0.
Y/H* 0.
( Al . L 1
( U » L )
( . 0 )
(UtOl
-1 .3252
0,0638
-1 ,0317
-0.3963
-0.7/05
0,0709
0,3669
1 « o 0 2 7
0.0642
0.6519
Z/K. 0.
-1.0645
0,0677
-1.1894
0.1367
ETA* 1.00
0.9451
-1.1894
0.0677
0.5315
-0.2607
-0.0039
0.1578
-0.5330
0.2941
0.003?
0,0028
C. 2322
CHI * 1 5.00
f M . L )
( UtL )
( V . D )
U; . 0 1
GAMMA*
1.5
zeta* c.bo x/h« o. Y/H=
-1.2175
0.2903
-0.9062
-0.1290
-0.6496
0.3271
-0,^944
0.5106
1 . 3946
-0.7124
0.2919
0.5601
-0.950B
0.3103
-0.9842
0.3129
E T A= 1.00
0.5 358
-0.9842
0 • 3 1 0 3
0,4379
-0.2667
- 0.0200
0. 1761
-0.4420
0.3012
0.0167
-C.CIO‘1
0.1977
CH I = 3 !
3
GAMMA*
1.5
7 ETA* 0.80
< w • U
(U.L)
I W* D )
( U.D I
-0,9546 -0.3438
0,4254 0.608F
-C.4728 -3.6962
0.0139 0.5WT
0, Y/H*
O.
Z/H*
0.
1.0614
-0.3769
0.4291
0.3434
-0.6685
0*4710
-0.6695
0.3574
ETA*
1,00
0.2463
-0.6695
0.4710
0.2156
-0.2862
—0 .0455
0.1966
-0.3435
0.3246
0.0379
-0.0267
0.1596
CHI=45.0C
( W t L )
(U.L)
( 'a * D )
( U.D)
0AMMA=
1.5
ZETA* 0.80 X/H* 0.
Y/H® 0.
-0.7028
C.3600
-0,1989
0.0094
-0 ♦ 0 1 4 '
0.5152
-0.467*
0.3922
0.9384
-0. 1068
0. 366 B
0. 14 B 0
Z/H*
0.
-0.3820
0.4453
-0.4190
0.2663
FTA*
1,00
0.1550
-0.4190
0,4453
0.0131
-0.3208
-0.0852
0.2201
-0.2569
0. 367B
0.0699
-0.0487
0.1259
CH I *60 .00
( W * L)
(U.L)
! W.DI
(U.D)
GAMMA * 1.5 ZETA* 0.60 X/H* 0.
Y/H* 0.
-0.5793
0. 1649
-0.0184
-0.0328
0.2245
0.44^3
-0 . 360 3
0.2374
0.9185
0.0626
0.1773
0. 0634
Z / H =
0.
- 0.2101
0.3196
“-0.2741 ■
0.1437
ETA* 1.00
0.1474
-0.2741
0.3198
-0.0700
-0.3692
-0.1549
13.2557
-0.1765
0.4346
0.1231
-C.DB62
0.0937
CHI =75*
ou
( W . L I
(U.L)
( w • D )
(UtD)
GAMMA* 1.5 ZETA*
-0.5676
-0.0656
0.11B5
-0.0412
0.3635
0.4105
-0,3563
0.1 C4R
0.9285
0.1739
-0. 0464
0.0460
Z/H =
0.
-0.1569
0.2090
-0.1995
0.0532
ETA* 1.00
0.1522
-0.1995
0.2090
-0.0478
-0.4107
-0.2746
0.3180
-0* 094A
0.5204
0.2015
-0.1588
0.0566
CHI *90.00
{ W » L I
( U.L)
( W.D)
(U.D)
GAMMA* 1.5 ZETA*
X/H* 0. V ZH* 0,
-0,5643
-C.2603
0.2603
-n.OOOO
0.4490
0 • 440 3
- 0,4403
o , r» 0 o o
0.9429
0.2767
-0.2767
o« rnno
Z/H* o.
-0.1528
0.1528
-0.1528
-ft.
ETA* 1.00
0.1528
-0.1528
0.1528
n.
-0.41 15
-0.4131
G.4131
-n . nnro
0.6018
0.2875
-0.2875
O.noor
28
TABLE 3. - Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 0.80, AND tj =1.00
(d) x/H =1.00
8
,
Correc
tion foctors for correcting from a wind tunnel which is
closed
closed
on bottom
I only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
1 * r 1
. 1
CHI- 0*
GAMMA * 1,5
ZETA* 0,80 X/H*
1.00
Y/H- 0.
Z/H- 0.
ETA- 1,00
(W*U
(U*L)
(W.D)
(UiD)
-0.5706
-0.3060
-0.6465
-1*1117
-0.3170
-0.5046
-0.5227
-0.2040
3*2722
-0*5819
-0.3143
0*1240
-0*4597
-0*4167
-0*6309
-0*4116
2* 3292
“0,6309
-0.4167
0*1095
-0.1109
0.1107
-0*0156
-0*7001
0*1427
-0*0879
0*1082
0*2076
CHI-13.00
GAMMA- 1,5
ZETA- 0,80 X/H*
1.00
y/h= o.
Z/H- 0*
ETA- 1.00
(w.d
(U.L)
(W»D)
(U»D )
-0.8755
-0.2863
-0,8339
-1*0503
-0.5654
-0.4486
-0.6877
-0*0327
2.9307
-0.7607
-0*2944
0*2338
-0*7371
-0*3783
—0*0140
-0*3195
2.0159
-0.8140
-0.3783
0.2867
-0*1385
0*0920
-0.0191
-0*7308
0*1717
-0*0703
0*1271
0*2867
CHI -30.00
GAMMA* 1.5
ZETA- 0*80 X/H*
1.00
Y/H- 0,
Z/H- 0.
ETA- 1.00
(W.D
(u.u
(W.0)
(U *D )
-1*2159
-0.0405
-0.9034
-0.7282
-0.8364
-0.2592
-0.8108
0.081?
2.4150
-0,8219
-0,0484
0.5238
-1*0448
-0*1605
-0*9174
-0.1227
1*5072
-0*9174
-0.1605
0*4777
-0*1711
0*1200
0*0140
-0*6055
0*2084
-0*0907
0*1066
0*2039
CHI -45.00
GAMMA- 1,5
ZET A= 0*80 X/H =
1*00
y/h= o*
Z/H= 0*
ETA- 1.00
<W*L }
( U *L 1
(W.D)
(U.D)
-1*3201
0*4045
-0.7525
-0.4508
-0.7902
0.1724
-0.6633
0*3156
1*7692
-0*6631
0.3973
0*5275
-1*0781
0.2783
-0.7737
0.1137
0.8575
-0*7737
0*2783
0,4400
-0.2420
0*1261
0*0211
-0*5645
0*?87P
-0*1060
0.1103
0*2019
CHI-60.00
GAMMA- 1,5
ZETA- 0*80 X/H-
1*00
Y/H- 0.
Z/H- 0*
eta= 1.00
(W. L)
(U.u
(W.D)
(U.D)
-0*9846
0.5399
-0.3870
-0.4060
-0*1639
0.3364
-0.3077
0*3282
1*3976
-0*2930
0.5369
0,2291
-0*6069
0.4317
“0.4176
0.1238
0*4461
-0*4176
0.4317
0.0916
-0*3777
0* ! 08?
0*0306
-0*5298
0* 4430
-0*095'*
0*1098
0.2045
CHI *75.00
GAMMA* 1,5
ZETA* 0*80 X/H =
1*00
Y/H* 0.
Z/H- 0.
ETA- 1,00
(W.U
(U.L)
(W.D)
(U.D)
-0.9204
0*2184
-0,1337
-0*4943
0*3819
0*2089
-0*1514
0*2192
1.3884
-0*0567
0*2209
0*1897
-0.3300
0,2274
-0.2136
0*0060
0.3212
-0.2136
0.2274
0.0044
-0*5903
-0*0090
0*0798
-0*5004
0.7119
-0*0186
0*0621
0*2131
CHI -90.00
GAMMA- 1.5
ZETA- 0.80 X/H-
1*00
Y/H- 0.
Z/H- 0.
ETA- 1,00
(W.D
(U.L)
(W.D)
(U.D)
-1.0624
-0,1078
0,1078
-0.5091
0*7951
0*2457
-0*2457
0*1583
1 *5494
0.1290
-0*1290
0.1979
-0*2505
0*1223
-0*1223
-0,0489
0.2585
-0.1223
0.1223
0.0489
-0.8039
-0.2300
0*2300
-0*4602
1*0535
0*1234
-0*1234
0*2072
6 ^ 1-1
L-15^9
29
TABLE 3.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.80, AND 1) = 1.00
(e) x/H = 2.00
Correction foctors for correcting from o wind tunnel which is
8
closed
close d
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
1— T 1 ' '
CHI ■ O,
GAMMA- 1.5
zeta-
0.80
X/H*
2.00
Y/H* 0.
Z/H* 0.
ETA* 1*00
( W * L )
(UtL)
(W.D)
( U * D )
-0*1198
-0.1749
-0*2630
-0.9426
-0.0727
-0.2647
-0.1799
-0*1504
3.3903
-0.2194
-0*1812
-0.0952
-0.1092
-0.2330
-0.2402
-0.2707
2.4772
-0.2402
-0.2330
-0.0629
-0.0106
0.0581
-0.0229
-0.6719
0.0365
-0*0317
0.0603
0*1203
CHI 3 1 5*00
GAMMA- 1.5
ZETA-
0.80
X/H*
2.00
Y/H- 0.
Z/H- 0.
ETA* 1.00
(WtL)
(UtL)
( W »D )
(UtD)
-0*2339
-0.2242
-0.3476
-0.9578
-0.1723
-0.3282
-0.2677
-0.1677
3.2999
-0.2989
-0.2313
-0.0639
-0.2160
-0.2867
-0.3299
-0*2860
2.4000
-0.3299
-0.2867
-0.0191
-0*0179
0.0626
-0.0177
-0.6718
0*0438
—0 .0414
0*0622
0*1183
CHI-30.00
GAMMA- 1.5
ZETA*
0.00
X/H-
2.00
Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.D
(UtL )
(W.D)
(U.D)
-0.4431
-0.2606
-0.4547
-0.9261
-0.3532
-0.3909
-0.3720
-0.1418
3*1340
-0.3996
-0.2692
0.0372
-0.4140
-0.3412
-0.4449
-0 # 2 8 02
2.2424
-0.4449
-0.3412
0.0693
-0.0291
0.0806
-0*0098
-0.6459
0.0600
-0*0496
0.0729
0*1384
CHI-45.00
GAMMA- 1.5
ZETA*
0.80
X/H*
2.00
Y/H* 0.
Z/H- 0.
ETA- 1.00
{ WiL )
(UtL)
(W.D)
(U.D)
-0.8644
-0.2158
-0.6015
-0.8464
-0.7079
-0.3962
-0.5032
-0.0719
2.7743
-0.5377
-0.2269
0.2346
-0.8062
-0.3245
-0.5898
-0.2153
1.8862
-0.5898
-0.3245
0.2632
-0.0582
0*1087
-0*0117
-0.6310
0*0963
-0.0716
0*0066
0*1434
CHI -60.00
GAMMA- 1.5
ZETA-
0.80
X/H =
2.00
Y/H* 0.
Z/H* 0.
ETA- 1*00
(W.D
(UtL)
(W.D)
(UtO )
-1.3293
0*3341
-0.6070
-0.6051
-0.9706
0.0643
-0.4658
0.1576
1 .9707
-0.5299
0.3199
0.4193
-1.1793
0.1764
-0.5806
0.0103
1.0650
-0. 5806
0. 1764
0.4196
-0.1500
0.1577
-0.0273
-0.6154
0.2087
-0*1120
0*1148
0*1473
CHI -75.00
GAMMA- 1.5
ZET A-
0.80
X/H*
2.00
Y/H- 0.
Z/H* 0.
ETA- 1.00
(WtL )
(UtL I
(W.D!
(U.D)
-0.9410
0.3686
-0.2510
-0.6141
0.0549
0.1149
-0.0626
0.1551
1 .5113
-0.1643
0.3641
0.1204
-0.5021
0.2272
-0.2065
-0*0064
0.4831
-0.2065
0.2272
0.0300
-0.4389
0.1415
-0.0445
-0.6077
0.5570
-0« 1 123
0* 1440
0* 1615
CHI-90.00
GAMMA- 1.5
ZETA-
0.80
X/H*
2.00
Y/H- 0.
Z/H- 0.
ETA* 1.00
(WtL)
(UtL)
(WtD)
lUtO )
-1.1665
0.0010
-0.0010
-0.6615
0.6532
0.0767
-0.0767
0.1223
1.7401
0*0280
-0.0200
0.1544
-0.3064
0.0727
-0.0727
-0.0582
0.3064
-0.0727
0.0727
0.0562
-0*8600
-0.0717
0.0717
-0*6033
1*1596
0*0040
-0*0040
0*1805
30
TABLE 3.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 0.B0, AND rj = 1. 00
(f) x/H =3.00
s
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
_
open
floor
only
closed
closed
on bottom
only
to free oir
r— 1 1 — 1
to grour
id effect
CHI ■ 0,
GAMMA* 1*5
ZETA-
0.80
X/H* 3.00
Y/H*
0.
i/H S 0.
E i A- l.uu
IW.LI
<U»L )
(W*0I
(U.D)
-0.0235
-0.0963
-0.1371'
-0.7919
-0.0181
-0.1222
-0*0906
-0.G889
3.3958
-0.1018
-0.0904
-0.0847
-0.0295
-0.1188
-0.1176
-0.1650
2*4774
-0*1176
-0*1168
-0*0630
0*0060
0*0225
-0*0195
-0*6269
0*0116
-0*0033
0*0270
0*0761
CHI -15.00
GAMMA* 1.5
ZET A =
o.du
X/H* 3.00
r/H*
0.
Z/H* 0.
ETA- 1.U0
IW»L)
1U »L )
(W,D)
(U*0)
-0.0670
-0.1271
-0.1719
-0.5165
-0.0586
-0.1570
-0.1248
-0.0944
3.3569
-0.1346
-0.1297
-0.0759
-0.0726
-0.1512
-0.1578
-0.1787
2*4465
-0* 1578
-0*1512
-u *0537
0*0056
0*0241
-0.0141
-0*6378
0*0140
-0*0058
0*0330
0*0843
CHI *30.00
GAMM A= 1.5
ZETA =
0.80
X/H* 3.00
Y/H*
0.
Z/H* 0.
ETA= 1*00
1 W»L )
fU*L)
tW *D 1
t U *D 1
-0.1498
-0.1636
-0.2226
-0.8200
-0.1364
-0.2053
-0.1757
-0*0943
3.2867
-0.1827
-0.1670
-0*0628
-0.1543
-0*1966
-0*2113
-0.1888
2*3821
-0.2113
-0*1966
“0*0342
U.U044
0*0332
-0*0113
-0*6320
0*0179
-0*0087
0*0357
0*0945
CHI -45.00
GAMMA* 1.5
ZETA*
0*80
X/H* 3.00
Y/H-
0 •
Z/H* 0.
ETA- 1.00
fWtL)
tU*LJ
tW#DT
1 U *D )
-0.3347
-0.2135
-0*3028
-0.8232
-0.3065
-0.2796
-0.2497
-0.0904
3.1332
-0.2587
-0*2192
-0.0213
-0.3352
-0.2625
-0.2925
-0.1913
2*2338
-0*2925
-0*2625
0*0155
0.0006
0*0490
“0*0102
-0*6319
0*0288
“0*0171
0*0428
0*1009
CHI-60.00
GAMMA = 1.5
ZETA =
0.80
X/H* 3.00
Y/H*
0.
Z/H- 0.
ETA- 1*00
(WtL )
(U.u
(W.D)
(U.D)
-0.8799
-0.1966
-0.4489
-0.7788
-0.7855
-0.3334
-0.3717
-0.0450
2.6686
-0.3955
-0.2075
0.1645
-0*8556
-0*2889
-0*4315
-0.1497
1.7901
-0.4315
-0.2889
0.2122
-0*0243
0*0923
-0*0174
-0*6291
0*0700
-0*0445
0*0598
0*1046
CHI *75.00
GAMMA* 1.5
ZETA =
0.80
X/H* 3.00
Y/H*
0.
Z/H- 0*
ETA- 1*00
<w*u
(U#L)
(W.D)
(U.D)
-0.9777
0.4197
-0.2822
-0.6209
-0.3552
0.1451
-0.1088
0*1134
1.6341
-0.2041
0.4050
0.0755
-0*7173
0*2494
-0*2244
0*0046
0*6684
-0*2244
0*2494
0*0606
-0*2604
0*1703
-0*0578
-0*6255
0*3621
-0.1043
0.1156
0*1086
CHI *90.00
GAMMA- 1.5
ZETA*
0.80
X/H* 3.00
Y/H*
0.
Z/H- 0*
ETA- 1*00
(W.D
tu.u
<W*01
(U.D)
-1.1666
0.0258
-0.0258
-0*6794
0.0644
0.0212
-0*0212
0.0790
1.7902
0.0070
-0.0070
0.0942
-0.3183
0*0401
-0*0401
-0*0461
0*3183
-0*0401
0*0401
0*0481
-0*8483
-0*0143
0*0143
“0*6313
1*1027
“0*0169
0*0189
0*1271
6^1-1
31
TABLE 3.- Continued
LONGITUDINAL DIST R1BUTION OF INTERFERENCE FACTORS FOR > = 1-5. C = °' 80 ' AND „ = 1.00
(g) x/H = 4.00
8
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
— —
to free air
' ~ ~
to ground effect
CH 1 * 0.
GAMMA- 1.5
2ETA- 0.80 X/H= 4.00 Y/H* 0.
Z/H * 0.
ETA* 1.00
0.0049
0.0027
0.0136
0.0525
(W.L)
1U.ll
IW.D1
IU.DI
-0.0045
-0,0586
-0.0886
-0.6883
-0.0047 3.3979
-0.0647 -0.0568
-0.0553 -0.0585
-0.0566 -0.0564
-0.0097
-0.0674
-0.0688
-0.1091
2.4700
-0.0688
-0.0674
-0.0460
0.0052
0,0088
-0.0198
-0.5792
CHI =15.00
GAMMA- 1.5
ZETA= 0.80 X/H* 4.00 Y/H* 0,
Z/H* 0.
ETA* 1,00
-0.0322
2.4531
IW.L)
-0.0863
-0.0905
(U.L)
-0.0905
-O.0863
(W.D1
tU.DI
-0.1174
-0.0436
CHI -30.00
GAMMA- 1.5
ZETA= 0.80 X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
0.0071
0.0024
0.0185
0*0660
(W.L)
(U.L 1
IU.DI
(U.D 1
-0,0682
-0,1006
-0.1347
-0.7210
-0*0676 3.3367
-0.1111 -0.1009
-0,1010 -0.1010
-0.0584 -0.0530
-0.0746
-0.1135
-0.1195
-0.1245
2.4176
-0.1195
-0.1135
-0.0385
0.0064
0.0129
-0.0152
-0.5965
CHl«45.00
GAMMA- 1.5
ZETA= 0.80 X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA* 1*00
-0.1677
2.3360
(W.L)
-0.1574
-0.1640
(U.L)
-0.1640
-0.1574
(U.D)
(U.D)
-0.1299
-0.0259
CHI-60.00
GAMMA- 1*5
ZETA* 0*80 X/H- 4,00 Y/H* 0.
Z/H* 0.
ETA* 1.00
0.0231
-0.0054
0*0284
0.0755
(U.L)
(U.L)
(U.D)
(U.D 1
-0,4364
-0,1975
-0.2633
-0,7364
-0,4206 3.0089
-0.2425 -0.2243
-0.2204 -0,2012
-0,0539 -0.0112
-0*4438
-0.2371
-0.2487
-0.1294
2.0965
-0.2487
-0.2371
0.0244
0.0073
0.0396
-0.0146
-0.6071
CHI-75.00
GAMMA = 1.5
ZETA* 0.80 x/H* 4.00 Y/H* 0.
Z/H*. 0.
ETA* 1.00
0.1917
-0.0703
0.0687
0.0755
(W.L)
(U.L)
IU.DI
(U.D)
-1.1770
0,3688
-0.3212
-0.6008
-0.8725 1.8844
0,1543 -0.2614
-Q.2103 0.3532
0,0822 0.1558
-1.0642
0.2246
-0.2790
0.0067
0.9511
-0.2790
0.2246
0. 1883
-0.1128
0.1441
-0.0422
-0.6075
CHI-90.00
GAMMA- 1.5
ZETA* 0,80 X/H* 4,00 Y/H* 0,
Z/H* O.
eta* i«oo
1.1920
-0.0172
0.0172
0.0881
(U.L)
(U.L)
(U.D)
(U.D)
-1.1554
0.0296
-0.0296
-0.6521
0.3733 1.8224
0,0055 0.0035
-0.0055 -0.0035
0.0517 0.0560
-0.3187
0.0227
-0.0227
-0.0364
0,3167
-0,0227
0.0227
0.0364
-0.8367
0.0069
-0.0069
-0.6157
32
TABLE 3.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y * 1.5, C = 0.80, AND rj = 1.00
(h) x/H = 5.00
s
Correc
tlon factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
T " 1 — > 1 —
to grour
id effect
CHI* o.
GAMMA - 1,5
ZETA* 0.80
X/H* 5.00 Y/H= 0.
L/ H> 0,
ETA* 1.00
£ W »L )
(U.L)
( W • D )
(U*D)
-0.0007
-0,0389
-0,0651
-0.6097
-0.0013
-0,0396
-0,0368
-0.0388
3.3999
-0.0356
-0.0380
-0.0377
-0.0038
-0.0424
-0.0448
-0.0772
2.4642
-0,0448
-0.0424
-0. 0330
0.0030
0.0035
-0.0203
-0*5325
0.0025
0.0026
0.0080
0.0384
CHI >15.00
GAMMA= 1,5
ZET A = 0,80
X/H* 5.00 Y/H= 0.
Z/H* 0.
ETA= 1.00
(W,L >
(U.L)
( W *D )
(U»D)
—0 ,0143
-0.0504
-0.0773
-0.6267
-0.0149
-0.0514
-0.0487
-0.0391
3.3860
-0.0471
-0.0495
-0.0375
-0.0177
-0.0545
-0.0581
“0.0824
2.4533
-0*0581
-0,0545
-0.0322
0.0034
0.0041
-0.0192
-0*5443
0.0028
0.0030
0.0094
0.0433
CHI >30.00
GAMMA* 1.5
ZETA* 0.80
X/H* 5,00 Y/H= 0.
2/H= 0.
ETA* 1.00
CW,L)
£ U *L )
(W»D)
( U »D )
-0.0397
-0.0667
-0,0944
-0,6407
-0.0403
-0,0684
-0,0653
-0.0393
3.3606
-0.0636
-0.0656
-0.0372
-0.0437
-0,0718
-0.0761
-0.0868
2.4306
-0.0761
-0.0718
-0.0305
0.0040
0.0052
-0.0182
-0.5539
0.0035
0.0034
0.0108
0*0475
CHI >45.00
GAMMA* 1.5
ZE1 A= 0,80
X/H* 5.00 Y/H= 0,
Z/H = 0.
ETA* 1.00
£ W.D
(U.L)
IW*D)
(U.D I
-0,0952
-0,0923
-0.1212
-0.6526
-0.0957
-0.0958
-0.0915
-0.0394
3.3061
-0.0897
-0.0914
-0.0362
-0.1006
-0.1000
-0.1039
-0.0906
2.3785
-0.1039
-0. 1000
-0.0266
0.0054
0.0077
-0,0173
-0.5619
0*0049
0.0041
0*0124
0*0513
CHI >60.00
GAMMA = 1.5
ZETA* 0.80
X/H* 5.00 Y / H= 0.
Z/H = 0.
ETA* 1.00
(W*L)
<U»L)
(W.D)
(U.D)
—0 ,2566
-0,1400
-0.1733
-0.6625
-0.2557
-0,1510
-0,1416
-0.0387
3.1508
-0,1405
-0.1396
-0.0306
-0.2652
-0.1556
-0.1565
-0.0933
2,2257
-0. 1565
-0.1558
-0.0124
0*0085
0.0158
-0.0166
-0.5691
0.0095
0.0048
0*0149
0*0546
CHI =75.00
GAMMA = 1,5
ZETA* 0*80
X/H= 5,00 Y/H= 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-1,2027
-0.0186
-0.3187
-0,6206
-1.1023
-0.1359
-0.2581
0.0084
2.3071
-0,2755
-0.0275
0.1967
-1.1803
-0.1075
-0.2915
-0.0467
1.3798
-0.2915
-0, 1075
0.2453
-0.0224
0.0889
-0.0271
-0.5739
0.0760
-0*0284
0.0334
0.0551
CHI =90.00
GAMMA = 1,5
ZETA* 0. BO
X/H* 5.00 Y/H= 0.
Z/H = 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-1.1468
0,0290
-0,0290
-0.6091
0.8802
0.0013
-0.0013
0,0349
1.0353
0.0028
-0.0028
0.0381
-0.3168
0.0137
-0.0137
-0.0273
0,3168
-0.0137
0.0137
0.0273
-0,8300
0.0153
-0.0153
-0.5817
1*1970
-0.0124
0.0124
0*0622
6- tfSi-'i
L-15^9
3S
33
TABLE 3.- Concluded
LONCaTUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR Y * 1.5, C = 0.80, AND tj = 1.00
(1) Miscellaneous additional values of x/H
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
_ CM ■15*00
GAMMA* 1*5
ZETA- 0*80 X/H- 0.33 Y/H* 0*
Z/H- 0.
ETA* 1.00
(W*U
•1*3321
-0,7906 1 • 989Q
-1*0785
1*0702 .
_r0*253t
0*2879
ruti)
0*0945
-0.0015 -0.9101
0*0434
-1*1000
0*0511
-0*0449
fW.01
-1*0010
-1.0493 0.0921
-1*1000
0*0434
0*0990
0*0508
tU»D]
•0*4674
0.3081 0*6446
0*0722.
0*5322
—0*5596
Q»?359 —
4 CHI *30*00
GAMMA* 1*3
ZETA* 0*80 X/H* 0,7? Y/H* 0,
2/H«_ 0*
ETA* 1*00
• (tt'll
-1,33.59
-0*8392 2*0167
=1* 1061
1*1041
-0*2294
0*2673
fU*W
0.1725
-0.0138 -0.8311
0*0721
-0*9654
0*1003
-0*0860
(w« 6 t
•0*9193
-0.8740 0.1670
-0*9654
0*0721
0*0459
0*0914
ru #d )
-0 *5 23 6
0,2639 0.6096
0*0.452
0*5231
T0«5708
0*2187
CHI -45.ro
GAMMA = 1,5
ZETA* 0*80 X/H = 1./8 Y/M= 0.
7./H* 0.
FT i = 1.00
(W»L 1
-1.3376
-0,^221 2.0557
-1 .1523
1.1523
-0.1 8 *3
0.230?
(U»L)
"0*2227
'-0,0265 -0./154
0.0846
— u . 8 00 6
0.1381
-0,1111
1 — rw»D r _
"-U.VWA
-0.6647 0.2131
-0.4006
3.0846
0.0012
0111*8
1 U»D )
' -0.5840
o . 1 y m 7 0.3410
0.0073
0.4990
-0.5413
C • 1 8 7 4
CHI = 6 r ' 4 n n
GAMMA* 1.5
0 ,r 0 > /r= ',17 Y/p* ,.0a
?/hj= o,
_ JLI A = L* .? n . .
< W »L )
-1.3246
-1.0291 /.l 106
-1.2053
1 • ? o >■> *
-0*1193
C. 1 76’
( lit L 1
0,2124
-0.03*5 -0.3356
0.0629 __
-0.5n? ft
J),14 q 4
-0* 1014
“Tw *'D )
-7.6091
-5'.4'7 7 5 0.197 V
0*0624
-0.0264
0, ] 05?
(U.D 1
- j .6 50 2
L> . 1 0 V '/ 0.4197
- 0 • 0 2 6 v
0.4352
-0 ,0213
C. 1 366
CH I s 7 3 » L
GAMMA* 1,5
ZFTA= 0,80 X /M* 3.4? Y/H* 0,
Z/H= 0.
FT A= 1.00
( W » L )
-1.0374
-0,5 5 "4 1.7179
-0,844?
0. 76^7
-0*193?
0. ?88°
(U »L )
0,4229
0,1 b64 -0,2250.
0,2.684
-0. ?434
0.1 6 46
-0*QS.L£>
(h*D )
-u *2958
-0 , 1 4 ;■ 7 0.4067
-0.2434
0 . 2^8.4
-0,0524
0,0957
<U»D }
— 0 .6113
C.1023 0 . Oil 7 6
0.0095
0.0957
-0.6208
0.0928
TABLE 4
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 100, AND T} = 1.00
(a) x/H * -2.00
Correction factors for correcting from a wind tunnel which is
closed
closed on bottom
closed
closed on bottom
6^1 -1
L-15^9
55
TABLE 4.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = l*. K - *■». AND , - 1.00
(b) x/H * -1.00
1
8
Correction factors for correcting from o wind tunnel
which is
closed
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
IBBBMi
to free air
to ground effect
1 7
Gamma* 1.5
2 FT A* 1*00 x/H«-i. nn
(W,D)
-0.4510
(U*0)
0.8041
CHI =15.00
GAMMA = 1.5
ZETA =
(W.U
-0.3320
IU.LI
0.4597
(W*0J
-0.2544
(U.D)
0.7079
CHI *30.00
GAMMA = 1*_5
;fta =
( W , L )
-0.1911
(U»L)
0.3597
fwTcrr
-0.1533
-0*4? 98
0.617R
0. 101 1
-0^3594
-0. 5 AS')
0.7055
0.5469
0.0577
1 .00
X/H = -l .00
-0*2034
0.533 3__
-0 » 382 0
0 .497 9
0.2261
-0*1686
0.4 5'9 P
-0.07V
0.271 2
- 0.0737 _
' n • 3 5 v 7 “
-0. 1 At?
-0.5044
0,P898
-0. Ap'ofl
0,7452
Z/H = 0 .
-0*2749
0*6047 _
-0.3870
0,6667
7 / H - __0
-0.1R45
0 . 40 V 6
-6.2814
0 . M 78
- 0.2867
-0. * 898
0**898
0.0456
FT A = 1.00
-0. 2064
-0*3870,
0.6047
-o.nPi 7
FT A = 1 .HQ
-0. 1264
-0 . ? 8 1 4
0.4096
-0.1604
-0*0607
-0*0431
0.1 7AP
0.05R9
-0.0871
_ -0* Q45Q .
0.1326
0*141 ?
0*071 6
0*0786
0*0051
-0*0688
-0.0566
-0.0499
0.1281
0.2056
0*0726
0.Q3QR
0*0046
—0*0006
CHI *45.00
GAMMA* 1.5
7 FT A= 1.00
X /H 3 — 1 . OO Y /Ms 0,
7 / H = (
- — — — 7tfYL~T
-0.1145
" 670225
n . 3 n 7 o
-0 * 0557
(U.L)
0.2608
0.3551
-0 • 0 2 84
0 . V01
rwrcn
-0. 1009“
-0*2246
0*2 60 7
-0 .2265
(U*D)
0.5580
0*1917
-0*1761
0*2994
FT A=
- 0.0616 - 0.0687 0 * 07 R 2
- 0.2 26 6 - 0 . 0 59 °
” 0 « 3 7 01 0*1 266 0*0020
- 0.1766 0 * 2586 - 0*1 077
CHI *60.00
GAMMA* 1.5 ZFT As
1,00 __X/_H=-1
,00 Y/H=_0.
7/H= 0.
FTA=_1 .00
—
(W.L>
-0.0853
0.1680
0*0663
0*2867
0.3326
-0.0088
-0.0228
0.2448
-0.013?
-0* ? ° 84
-0.0624
-0.076°
(U*L)
0. ?44 R
0.1267
rwTCi
(U »D 1
-0.0721
0.5114
— 0 • 2 0 79 .
0*0853
-0.1 773
0.707?
-0. 1 6 fl 4
0.3047
0*089?
-0*0044
-0* 1213
ChT-^S.SO GAMMA* 1.5 ” ZETA'= 1*00 X/H=— 1 *00 Y/H= 0
|W*L1 -0.0873 0.08 1 8 0.3462
— ■ (U»L) 0.0829 0.2422 .. “0 *.001 2
( W.OT -0*050 7 -0*2010 0*0816
(U.01 0.4619 0*0036 -0.1639
' 7. / H *
0.
FTA = 1*00
-6.0250
0.1928
—0 .1830
O. 1 373
0.0711 -0.0623
-0.1810 rQtl099
0.1978 0*1323
-0.137^ 0*3446
0. 106«
_JLl04_93_
-0*0181
-0*1337
CHI *90.00
( W*L)
( U ♦ L )
(W.D)
(0*D)
GAMMA* 1.5 ZFT A = 1*00 X /Hg^liOO ^/Hf.
_n L 2./H= . C* —
-0.0924
0.027 2
-0.0272
0*4667
0.0813 0.360?
0*21 54 0.0026
-0.2154 ' ’ -0.0025
-0.0590 -6.1576
-0.0466 0.0466
__0,17_08 r.Q • 17Q8-
-0.1708 0 . 1 70 R
0.0854 -0.0854
-0*0458
0*1437
0*3813
0*12X9
n. 044.6
-Q« 0446
-0*1444
36
TABLE 4. - Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS
(c) x/H = y/H = z/H = 0
FOR y - 1.5, £ = 1.00, AND tj = 1.00
Correction factors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free olr
r ,
■
to grour
id effect
C I = - 3 ♦ 00 ' GA^‘X - 1 . 6 ?ETA“ 'T.
< W * L ' )
( W ♦ 0 )_
(u. 6'1
- 1.7720
0,1 046
-0, 3 Q «? ft
-1 . 5408
-0.1066
-r.”ol A6'
0. 1 75^
2.616?
-1.7540
-0.1047
0.8767
-1.6633
-0. 1056
-1.94*55
0.0 143
eta^ T.oo
1.8760
-1.9455
'-o;to5p
0.8305
-0. 1087
0.0011
"o.imi
-0.4140
0.1224
-o.oooe
“070770—
0.1610
__GaMMA = _1.5 ZE'TA= 1.00 X/H =
JWtlT
J U_* L r
(W.D)
1 0 , 0 )
-1 .7720
~d’i 1046
”-l .7541
- 0.1614
-1.5409
0.1066
-1 .“8330
0.3601
y/H- o.
2.1961
-1 .6630
“0-.T04T-
0.8767
-1.6633
0. 1058
7F57T5
•’7136
1.4767
-1.8 585
M . 1TT5H"
0.8305
-0.1087
-o.omi
0 . Tn 44
-0.3750
CHI* 15.00"
G AMM As jj 5 ?ETA = ‘ 1.00 X/Hs 0 .
< w . o r
(U » D }
-1.5973 “
0.479?
-*! . 42 79~
'-o,Tff42“
- 1.3597
0.4889 "
-1 76 T 5 ?~
CH I = 3 OV 0 O '" 'GAMMA- 1, 6 ' ' 7 pTA =
'l.oo
1.5207
-1.3349
“1T.4T9T '
0.7315
-1 .4857
.4F49
-T. 5 3 7y
0 *4890
’“TT.8371
-1 .5379
074849”
0.6841
0 » f 22 7
- 0 . 930 V
v;rrr6
-0.Q066
”0’.7'45l
^T;o‘27i -
*0‘.649fi
157722Q
0. 3876
J-1.0445
_ 077359 “
" -r .0460
0.5584
CHt *45 » 00 ~ “ GaM ">-» A = 1,5 2 FT As
1 W.LT
ru"« Li
UJ.O t
-0.T38 7
0.6697
-0.5321 '
0.2500 -
1 .00
-0.4354
0,7135
-0 . 6416
0.482T
0.8621
- 0 . 4397 T
"' 0767110 -
0. 0771
"-0.5968
0 75 95 7
'-0765 48
0.4160
0. 3B79
”-170460
0.7359
0.3368
F Tfi= 1.00
0.2 4?2
-0.6548
""O’. 6957“
0.0205
( V , L 1
JJJjrLJ
GAMMA = 1.5
-0.5041
1.00 X/H=
“0.1172
- 0.1245
_" 0. 5 34 3
- 0 . 42 X 5
y/h=
0.8312
—0 . 20ft 1
0.4477
-676468
T 7 h 7
-075783
074996
- 0.4283
67 274 ’?
0.2 303
- 0.4283
~ 0.4996
-071694
- 0.1117
- 0.0056
OillOO
-0.3040
0.1259
0.0040
0YC227
0. 1200
- 0.1220
- 0.0172
’071159
- 0.2308
- 0*1419
- 0.0260
“071727
- 0.1661
0.1 379
"O.OOTZ
“ 0. U1 89 “
0.1615
’ 0701 78
0.01“32
0.0660
- 0.1758
- 0.0527
0. lTTEJ - '
0.2037
0.0347
CH T7T5761T
Gamma = 176 "
ZfcTAs
l.no
X7H=
0. Y/H= 0.
Z/H= 0.
ETA = 1.00
—
—
fW.L)
-575X55“
— • —
0.076H
-
C7F30 3 “
-0. 0B37
" -0.7457
0.3265
—
fU.L)
I W iD]
1.TTT0“
6.3727
0. 2378
-0.3117
=07 2203
-TT. 71 5 ft
077770
(UfOl
0.0308 '
0. 1044
0.2107 " ■“
-0.0223
' -0.3117 '
0.0831
“6.5755
-0.0746
u.iby;
-0.0524
-070 2 73
0.0713
-
-
—
rMTs90.oo~ •
G A MMX's 1,5
7 FT A =
1 .00
X /8s
0, Y/H= 0.
Z/H= 0.
—
FTA= 1.00
—
1_ 1 w , L j
fU.U'"
( w * 6 1
-0.4762
'6.0273
-n“.077T“
0. 1 172
0.33SP
"TA ’ 0
0.8306
0.0075
-0.2387
0.2387
0.2387
-0.2387
-0.2374
-0.2114
0. 3509
0.0961
fii.ot
- 0.0000
0 . none- "
-0.0025
o. onoo
-0.2387
-0 .
0723 B 7
0.
6* 71 T4
-0.0600
=070161
070000
6+£l-l
L-15^9
37
TABLE 4.- Continued
LONQTUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 7 = 1.5, S = 1.00, AND f| = 1.00
(d) x/H = 1.00
Correction factors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
fl oor
closed
on bottom
only
(ground effect)
only
only
to free air to ground effect
» 0.
GAMMA* 1,5
ZET A* 1,00 X/H*
1.00 Y/h= 0,
Z/H* 0.
ETA= 1.00
<W,L )
r u • l j
1 W*D 1
(U *D }
-0,5651
-0 • 546 A
-0,7356
-1 .2228
-0,4298
-0,6178
-0,7046
-0,4121
4.6102
-0,6746
-0,5469
0,0577
-0,5044
-0,5898
-0.7606
-0*6052
3.7647
-0.7606
-0, 589H
0,0458
-0*0607
0.0431
0,0271
-0.61 75
. 0,0746
-0.0280
0.0560
0.1931
CH I « 1 5 • 00
GAMMA* 1.5
ZETA*
1,00
X/H=
1,00
Y/H" 0*
Z/H= 0.
ETA" 1.00
IW.LI
IU»U
(W,0 1
(U.Ot
-0.9320
-0,5649
-0,9720
-1.0672
-0.7876
-0,6645
-0,9802
-0,4132
4,2514
-0.9050
-0,5650
0.3270
-0.8670
-0,6220
-1,0223
-0,5480
3,4290
-1.0223
-0.6220
0.2594
-0.0650
0,0571
0,0503
-0,5192
0.0794
-0.0425
0.0420
0*1347
CHI "30.00
GAMMA= 1.5
ZET A"
1,00
X/H =
1,00
Y/H" 0.
Z/H= 0.
ETA" 1.00
(W*L >
lU.D
( W * D )
ru.o)
-1.4756
-0.4247
-1,2165
-0,8836
-1,2920
-0.5017
-1,2031
-0,1769
3.6130
-1.1436
— C, 4248
0.5973
-1.3918
-0.4706
-1.2597
-0*3551
2,8153
-1 • 2597
-0.4706
0,5742
-0,0839
0.0459
0.0432
-0.5284
0.0990
-0.0311
0.0566
0.1782
CHI "60,00
GAMMA* 1,5
ZETA =
1,00
X/H"
1.00
Y/H= 0.
Z/H* 0,
FT A= 1.00
(W,L)
(U»L )
( W«D )
IU.D)
-1.3540
0,7226
-0,6720
-0.2754
-0,9755
0.6393
-0.6612
0.3379
1.6526
-0.5863
0*7226
0.3228
-1.1785
0.6741
-0.7224
0.1769
0.8731
-0.7224
0*6741
0.2608
-0.1755
0.0485
0*0504
-0,4523
0.2030
-0.0348
0.0613
0.1609
CHI-75,00
GAMMA" 1,5
ZETA =
1.00
X/H"
1.00
Y/H" 0.
Z/H* 0.
ETA* 1.00
( W ♦ L )
(U#LI
IW»D)
IU.0 )
-0.8859
0,3544
-0.2636
-0.4166
-0.2261
0,3449
-0,2819
0,1508
1.3710
-0.1033
0.3548
0.1185
-0.5027
0,354?
-0.3302
-0.0010
0.5663
-0.3302
0,3542
0.0207
-0*3032
0.0003
0,0667
-0,4156
0.3566
-0*0093
0*0484
0.1517
CHI "90,00
GAMMA" 1,5
ZETA"
1,00
X/H"
1.00
Y/H" 0.
Z/H* 0.
ETA" 1.00
IW.LI
(U.U
(W.D)
<U*D>
-0.8599
0.0272
-0.0272
-0.4667
0.1430
0.2154
-0,2154
0.0590
1.3106
0.0025
-0.0025
0,1576
-0.4309
0.1708
-0,1708
-0,0854
0.4309
-0.1708
0,1708
0. 0854
-0.4290
-0,1437
0*1437
-0.3813
0.5740
0.0*46
-0.0446
0.1444
38
TABLE 4.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 7 = 1* 5 > C A** 0 = 1,00
(e) x/H =2.00
Correction foctors for
correcting from
o wind tunnel
which is
closed
closed floor
open
closed
s
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free oir
to ground effect
CHI ■ 0«
1
GAMMA* 1.3 ZETA* 1.00 X/H
* 2.00 Y/H*
3. Z/H = 0.
ETA* 1.00
I W #L )
-0.0989
-0.0616
4.7551
-0.0864
3.8753
-0.0124
0.0249
(U*L 1
-0.2272
-0.2691
-0.2103
-0.2572
-0.2552
0.0301
-0.0118
IW»D>
-0.2550
-0.2150
-0.2269
-0.2552
-0.2572
0*0003
0.0394
IU»DI
-0,9764
-0.1092
0 « A 2 0 6
-0,3272
-0,1076
-0.6492
0 . 1380
CHI *15.00
GAMMA* 1.5
ZETA*
1,00
X/H-
2.00
Y/H-
0.
Z/H* 0.
ETA- 1.00
IW.L )
IU.L >
Itf »D)
IU.DI
-0.2026
-0.2850
-0.3336
-0.9627
-0.1502
-0.3316
-0.2980
-0.1826
4.6708
-0.2926
-0.2848
-0.0642
-0.1887
-0.3245
-0.3467
-0.3529
3.8030
-0.3467
-0,3245
-0,0768
-0.0139
0.0395
0,0131
-0.6097
0.0305
-0.0071
0.0487
0.1703
CHI -30.00
GAMMA- 1.5
ZETA*
1.00
X/H*
2.00
Y/H-
0.
Z/H- 0,
ETA* 1.00
(W.L)
IU.L)
IW.DI
iu.dj
-0.4041
-0.3735
-0.4571
-0.9873
-0.3458
-0.4299
-0.4226
-0.2163
4.5081
-0.4115
-0.3733
-0.0243
-0.3824
-0,4123
-0.4679
-0.3663
3.6535
-0.4679
-0.4123
-0.0125
-0.0217
0.0388
0.0108
-0.6210
0.0365
-0.0176
0.0453
0.1500
CHI -60.00
GAMMA= 1.5
ZETA*
1.00
X/H*
2.00
Y/H-
0.
Z/H- 0.
ETA- 1.00
(W.L )
(U.U
(W.DJ
(U.DI
-1.8427
-0.1491
-0*8440
-0.7485
-1,6674
-0.2615
-0.7901
0.0024
3.1534
-0.7825
-0.1490
0.5974
-1.7682
-0.2221
-0.8521
-0.1543
2.3119
-0. 8521
-0.2221
0.5993
-0.0745
0.0730
0.0060
-0.5942
0.1008
-0.0395
0.0620
0.1568
CHI-75.00
GAMMA* 1.5
ZETA*
1.00
X/H =
2,00
Y/H-
0.
Z/H* 0.
ETA- 1.00
IW.L)
IU.L J
(W.Q)
(U.D }
-1.1645
0.4541
-0.3331
-0.5821
-0.6550
0.3163
-0,2485
0.1541
1.7577
-0.2561
0.4546
0.1131
-0.9356
0.3670
-0.3296
-0.0034
0.8890
-0.3296
0.3678
0.0630
-0.2289
0,0863
-0,0035
-0,5787
0.2805
-0.0515
0.0811
0.1575
CHI -90.00
GAMMA- 1.5
ZETA*
1.00
X/H-
2.00
Y/H-
0.
Z/H- 0.
ETA- 1.00
(W.L)
IU.L )
(W.O )
IU.0)
-0,9782
0.0266
-0,0266
-0.6488
0.1681
0.0776
-0.0776
0.0760
1.5079
0.0024
-0.0024
0.1432
-0,4919
0.0844
-0.0844
-0.0844
0.4919
-0.0644
0.0844
0.0644
-0,4663
-0,0578
0.0578
-0.5644
0.6600
-0.0066
0.0066
0.1604
6^1-1
L-15^9
39
TABLE 4. -^Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V '
(f) x/H = 3.00
1.5, £ = 1.00, AND tj = 1.00
—
—
Correction foctors for
correcting from
a wind tunnel
which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
Ch 1 ■ o.
(W.L)
(U.L )
• ' IW.D)
(U.D)
T
GAMMA* 1.5 ZETA* 1.00 X/H= 3.00 Y/H-
-'■■*0187 -0*0117 4.7624
-0.1062 -0.1203 ‘^1057
-0.1301 -0*1000 -0.1057
-o!ail9 -0.0968 -0.0892
0. Z/H = 0 *
-5*0196
-0*1201
-0.1215
-0.1877
ETA= 1.00
3.8622
-LJ. 1215
-0.1201
-0.0782
0.0010
0.0139
-0,0085
-0.6242
0*0079
-0*0002
0*0215
0*0909
CHI =15.00
(W.L)
(U.L)
(W.D)
(U.D)
GAMMA = 1.5
-C ,0 604
-0.1403
-0.1672
-0.8355
ZE 1' A* l.^JW X
-0*0506
-0*1525
-0.1343
-0.C963
/ H* 3 • u u Y / H
4*7241
-0.1369
-0.1398
-0.0917
0. Li H* 0.
-0*0603
-0.1536
-0. 1604
-0.2025
ET 4= 1.00
3.8319
-0.1604
-0.1536
-0.0730
-0.0001
0 .0 133
-0*0068
-0*6331
0*0097
0*0010
0*0261
0*1062
CHI s30.DC
(W.L)
(U«L)
( W » D )
(U.D)
GAMMA® 1*5
ZETA = 1*00
X /H® 3*00 Y/H* 0.
-0,1374
— 0 » 1 8 3 ^
-0.2147
*•0*8395
-0*1253
-0*2v36
-0.1861
-0*1585
4*6550
- j* 1825
-u. 1824
-0*v756
Z/H* 0*
-0*1369
-o* 2 oie
-0.2125
-0.2147
ET A = 1.00
3*7687
” 0*2125
-u.2018
-u.0621
-0.0005
0*0168
-O.UG22
-C.6248
0.0116
-0*0016
0*0264
0*1063
CHI -45*00
gamma. 1.S EETA- 1<» a/h* 3.00
Y/H- u*
(W.L)
(U.L)
* rw .0 1
(U.D)
-C .3383
-0.2528
-0.2928
-0.6476
-0.2881
-0*2829
-0,2623
-0*1114
4.5039
-0.2579
-0.2522
-0* -524
Z/H = 0 *
-0.3G53
-0.2787
-0.2922
-u.2237
E i A= 1.00
3.6234
-0.2922
-0.2787
-j. 0349
-0*0030
0 *02 60
-O.OOOo
-0.6239
0.0172
-0.0041
0.029b
0*1123
CHI 3&C.C0
(W.L)
(U sL )
rw»o>
(U.D)
GAMMA® 1.5
ZETA= 1*JC •< / H* 3,00
Y/H*
-0.6194
-0.3654
-0*4440
-0*8411
-0*77C5
-0.4217
-0*4055
-0*1005
4.0690
— L * 4 j4u
-.*3647
0*0534
Z/H* 0.
— 0 * 8 0 58
—0 *4u99
-0,4421
-0.2183
E T A= 1.00
3. 1931
— 0 , 4421
-0.4099
0.0772
-0.0137
0*0445
-0.0019
-0,6228
0*0353
-0*0118
0*0366
0*1178
CHI = 75 * UU GAMMA® 1*5
ZETA® 1*00
l W t L )
(U.L I
( W » D )
( U.D)
'1*6241
0*4906
•0.4297
•0*6046
—1 * 346u
0*3497
-0*3496
0*1380
3*00
Y t H- 0 «
/H= o •
2.2386
-^*3721
j *4912
0*2182
-1,5078
0 • 392u
-0*4108
0.0159
ETA- 1*00
1.3528
-0.41 00
0.3920
0.2220
-0.1162
0.0986
-0*0189
-0*6205
0.1619
-0*0423
0*0612
0*1222
CHI = 90 *'
>0
(W.L)
(U.L }
(W.D) '
(U.O)
GAMMA® 1*5 ZEiA=
-0.9074
0*0258
-- -0.0250
-0*6772
a / H = 3 • O '.' ' **
0.1861 1.5717
v*w226 0*0024
0*0226 -o.uo24
0,0647 0.0922
4- / H =
u «
ET A=
1.U0
—0. 4935
v *u4u7
-0*0407
-0*0611
0.4985
— 0. u4u7
0. 04U?
0.0611
-0.4869
-0,0150
0*0150
—0*6161
0*6846
-0*_0182
0*0182
0.1258
ho
TABLE 4.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 1.00, AND ij = 1.00
(g) x/H = 4.00
s
Correc
f.on factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
’ r
to grour
id effect
(W.L)
(U»L)
( W »D I
(U.D)
GAMMA- 1.5 ZETA- 1.00
-0.0036 -0.0028
-0.0603 -0*0639
-0.0829 -0.0578
-0.7055 -0.0585
X/H- 4.00 Y/H- 0. Z/H = 0.
4*7648 -0.0059
-0.0571 “0.0663
-0.0596 “0.0700
“0.0571 -0.1206
ETA- 1.00
3.8503
-0.0700
- 0.0663
-0.0515
0.0023
0.0060
-0.0129
-0.5849
0.0031
0.0024
0.0121
0.0621
CHI -15.00
(W.U
<U*L>
( W » D )
ru.D)
GAMMA* 1,5
ZETA- 1.00
-0,0249
-0,0245
-0,0797
-0,0814
“0.1006
-0.0783
“0,7251
-0.0555
x/H- 4.00 Y/H- 0. Z/H- Q,
4.7431 -0.0276
“0.0741 -0.0851
-0.0790 -0.0908
-0.0517 -0*1287
ETA- 1.00
3.8333
-0.0908
-0.0851
-0.0503
0.0027
0.0054
“0.0096
-0.5964
0.0032
0.0037
0.0125
0.0732
CHI -30.00
GAMMA- 1.5 ZETA- 1.00 X/H- 4.00 Y/H- 0.
f W ♦ L )
(U.L)
IW.OJ
I U .0 )
-0.0657 -0.0640
-0.1040 -0.1096
-0.1284 -0.1036
-0.7324 -0.0617
4.7041
“ 0.1012
“0.1033
“0*0550
Z/H* 0.
-0.0683
“ 0.1122
“0.1190
“0.1356
ETA* 1.00
3.7976
“0.1190
“ 0.1122
-0*0477
0.0026
0*0002
-0.0095
-0*5968
0.0043
0*0026
0.0153
0*0739
CHI-45.00
(W»L)
(U.L)
<W»D>
(0*0)
GAMMA- 1.5
ZETA- 1*00 X/H* 4.00 Y/H- 0.
Z/H* 0.
-0.1571
-0.1562
-0.1623
-0.1416
ETA- 1.00
3.7165
-0* 1623
-0.1562
-0.0415
CHI-60.00 GAMMA- 1.5 ZETA*
IW.L) -0.4121
<U*L) -0.2226
CW.D) -0.2526
(U.D) -0.7507
1.00 X/H- 4.00 Y/H* 0.
-0.4026 4.3774
-0.2411 “0.2226
-0.2247 -0.2214
-0.0626 -0.0365
Z/H- 0.
-0.4147
“0.2432
“0.2447
“0.1457
ETA- 1.00
3.4778
“0.2447
-0.2432
-0.0195
0*0025
0.0207
-0.0079
-0.6049
0.0121
0.0021
0.0199
0.0831
CHI-75.00
GAMMA* 1,5
ZETA*
1.00
IW*L)
(U.L )
(W.D)
(U.D )
-1.8791
-0.0979
“0.4719
“0.6817
-1,7734
-0.1847
-0.4216
0.0148
CHI-90,00
GAMMA* 1,5
ZETA-
1.00
(W.U
(U.LJ
( W »D )
(U.D )
“0.9785
0.0246
“0,0246
“0.6523
0.1983
0.0060
-0.0060
0,0477
X/H-
4.00
y/h» o.
Z/H- 0.
3.0554
-0.4317
-0.0965
0.3542
-1.0442
“0*1680
-0.4555
-0,0729
X/H-
4,00
Y/H= 0.
Z/H* 0.
1.5971
0.0023
-0.0023
0.0577
-0.4950
0.0214
“0.0214
-0.0427
ETA- 1.00
2.1560
“0.4555
“0. 1680
0.3833
“0*0350
0.0701
-0.0163
“0.6088
0.0708
-0.0166
0*0339
0.0876
eta* 1,00
0.4950
“0.0214
0.0214
0.0427
-0,4835
0.0033
-0.0033
-0.6096
0,6933
-0.0153
0.0153
0,0904
L-1549
L-15^9
4l
TABLE 4.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 100, AND TJ = 1.00
(h) x/H = 5.00
s
Correction foctors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
1 1 1 r
to grour
id effect
CHI- 0.
GAMMA- 1.5
2ETA- 1.00
X/H =
5.00
Y/H- 0,
Z/H- 0,
ETA- 1.00
( W«L )
(UtL)
(UtD)
(UtD )
-0.0006
-0.0389
-0.0600
-0.6255
-0.0007
-0,0394
-0,0375
-0.0392
4.7670
-0,0360
-0.0381
-0.0376
-0.0022
-0,0415
-0.0450
-0.0838
3. 8424
-0.0450
-0.0415
-0.0352
0.0015
0.0026
-0*0150
-0.5417
0.0015
0.0021
0.0075
0.0446
CHI-15.00
GAMMA- 1.5
Z£T A* 1.00
X/H-
5.00
Y/H- 0,
Z/H* Ot
ETA- 1.00
(WtL)
(UtL)
(UtD)
(UtD)
-0.0141
-0.0505
-0.0720
-0,6393
-0*0142
-O' ,0511
-0.0494
-0,0397
4.7531
-0.0476
-0,0497
-0.0377
-0.0158
-0.0534
-0*0579
-0.0885
3*8314
-0.0579
-0*0534
-0.0348
0.0017
0.0029
-0.0142
-0.5507
0.0016
0.0022
0.0065
0.0469
CHI-30.00
GAMMA = 1,5
ZET A- 1,00
X/Hs
5.00
Y/H* 0.
Z/H- 0.
ETA= 1.00
(WtL)
(UtL)
( W t D )
(UtO)
-0.0393
-0,0669
-0.0888
-0.6505
-0.0393
-C.0679
-0.0660
-0.0400
4.7279
-0.0640
-0.0661
-0.0375
-0.0413
-0.0705
-0.0754
-0*0926
3*8085
-0.0754
-0.0705
-0.0340
0.0019
0.0036
“0.0134
-0.5579
0.0020
0.0026
0.0094
0.0526
CHI -45.00
gamma- 1*5
ZETA- 1.00
X/H-
5.00
Y/H- 0,
Z/H- 0.
ETA* 1.00
(WtL)
(UtL)
(WtD )
(UtD )
-0.0941
-0.0932
-0.1154
-0,6603
-0,0939
-0.0949
-0,0923
-0,0404
4.6735
-0.0902
-0.0921
-0.0370
-0.0966
-0*0981
-0*1026
-0*0962
3.7563
-0*1026
-0.0981
“0.0322
0.0025
0.0049
-0.0127
-0.5641
0.0027
0.0032
0.0103
0*0558
CHI -60.00
GAMMA- 1.5
ZET A= 1,00
X/H-
5.00
Y/H- 0.
Z/H- 0*
ETA- 1.00
(UtL)
(UtL)
(UtO)
(UtD)
-0.2519
-0*1438
-0.1666
-0.6690
-0.2507
-0.1483
-0.1428
-0,0405
4,5184
-0.1407
-0.1424
-0.0347
-0.2557
-0.1526
-0*1543
-0*0993
3.6034
“0.1543
-0.1528
-0.0262
0.0037
0.0090
-0.0122
-0.5697
0.0049
0.0045
0.0116
0.0589
CHI -75.00
GAMMA- 1,5
ZETA- 1,00
X/H*
5.00
Y/H- 0.
Z/H- 0*
ETA* 1.00
(WtL)
(UtL)
(UtO )
(UtO )
-1,1580
-0.2765
-0.3210
-0.6707
-1.1307
-0.3118
-0.2896
-0.0330
3.6SQ8
-0.2913
-0.2743
0.0449
-1*1566
-0.3134
-0*3066
-0.0953
2.7678
-0.3066
-0.3134
0.0710
-0.0014
0.0368
-0.0144
-0.5754
0.0260
0.0016
0.0170
0.0623
CHI-90,00
GAMMA- 1,5
ZET A= 1,00
X/H-
5.00
Y/H* Ot
Z/H- 0*
ETA- 1.00
(UtL)
(UtL)
(WtDI
(UtD 1
-0.9704
0.0233
-0,0233
-0,6098
0,2062
0.0015
-0,0015
0.0338
1.6101
0.0022
-0*0022
0.0380
-0.4910
0*0122
-0*0122
-0,0306
0.4910
-0.0122
0.0122
0.0306
-0.4795
0.0111
-0.0111
-0.5792
0.6972
-0.0108
0.0108
0.0644
42
TABLE 4.- Concluded
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C c 1*00, AND t? = 1.00
(1) Miscellaneous additional values of x/H
Correction
factors for
correcting from
a wind tunnel
which is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to
free air
to ground effect
—
GAMMA* 1.5
ZFTA= 1 .00 X /M—
0.77 V/Hs
0.
2/H= 0.
FTA= 1.00
.
(W»L l
-1.7953
-1.5618
0.04 73
7.4278
-1.5430
-1 .6856
0.0572
1.6925
“1*7194
-0.1096
0.0H2
0.173°
-0.0098
(W,D ) ~~
( u ► p_i
-1.631U
-0.3001
-1.6638
0.2592
0.070?
■" 0.6777
- -
-1.7194
0.1033
Q._Q5 7 2
0.8315
0.0884
-0.40 3 a
0.0?5fi__
0. 1559 —
—
CHI » 3-.no
GAMMA = 1.5
Z ET A = _ 1.00 X
0,57 Y/H*
Z/H* .0.
FTA= 1.0Q.
^ 1 -
(W.L)
-1.8409
-1.5994
0.1024
-1.4621
0.2398
7.4588
-1.3510
0.1513
0.6606
-1.7781
0.1731
-1.5081
0.0781
1.7077
-1.5081
0.1731
0. 8167
-0.11 ?R
0*078?
0.0719
-0.43 1 5
0.1787
-0.0706 ...
( U * L 1
(W,D f
(UtD)
0.1514
-1.4362
-0.3534
0.0460
0.1617
. . .
- - .
— .. . 1 . .
. ^
CH I »45.0Q
GAMMA= 1.5
2 FT A= 1.00 X/H =
1,80 Y/Hs
n.
z/h = n,
> FTA= 1.00
■ ■ — '
(W.L)
{UtL )
-1.4627
-0.4066
-1.3031
-0.4996
3.6298
-0.9097
-1 .3975
-0.4645
?, R099
-0.9993
-0.0701
o.Q5?g__
0.0894
-0.0357
( W * 01
(U»0 )
-6.9750' ”
-0.8790
-0.9393
-0.1412
-0.4067
0.5043
-0.9993
-0.3111
—0.4645
0.4969
0.0243
-0,5678
0.0&00 ...
0.1690
. ..
..... ... .
- -
CHI-45.no
gamma = i.5
ZFT A = 1,00 ~ X/H=
: ?,5n Y/H
= 0.
7/H = 0
. F7A= 1.00
(W.L)
( U * L )
-0.4882
-0.3476
-0.4439
-0.3977
4,3854
-0.3758
-0 ,4744
3.5205
. _-C , 4216_
-0*0138
0.037«
0,0305
-Q.Q177-
rwTo>
-0*4168
-6.3820
-0.3472
-0.010H
-0.4716
-0*7854
-0.3851
0*0048
-0.6234
0.0396
0.133C
( UtD )
-0.9089
-0.1524
CHI-60.00
GAMMA- 1.5
ZFTA 2 1.00 X /H
; 1 . 73 Y/H
v o.«_
Z/H = 0
• f;TA_=__.u.aa_
(w.L)
(U.L )
-1.9839
0.1816
-1.7550
0.0615
7.70V2
-0.6280
-1.8879
_0*1 063_
1.8796
-0.9102
-0*1010
0.0752
0*1779
-0.0448
{ W » D )
(UtD)
-0 . 8968
-0.6134
-0.8436
0.1220
0.1815
0.6930
-6*9109
-0.0424
0.1063
0*6799
0,0141
-0.5711
0.0673
0*1644
....... . .
CHI-75.06
GAMMA* 1.5
lETA- 1.00
X/H
- ijjy
2/M* 0. ETA* 1«M
—
tw*rr
’ iu*ti
•I •4409
0.5043
~~^UI220
0 • 3360
2.0817
-0.3347
-1.3131
0*AOH_
i* m?
fit lift!
... 4**411
—ft. 4*7*
iw.6)
toibl
-0.34TS
-0.6017
-0.3109
0.1471
0.5050
-0.3T*4
0* 4036
-OtOlTB
0.1366
0.0147
0.1463
-4.6144
0*1524
6+i^T-l
L-15^9
43
TABLE 5
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V » 1-5. C * 150 ' ‘ 1 '°°
(a) x/H = -2.00
s
Correction foctors for correcting from o wind tunnel
which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
'
CHl * 0.
GAMMA* 1.5
ZETA*
1.50
X/H--2.00 Y/H*
( W *L )
(U.L)
(W.D)
(U.D)
-0.0502
0.2609
0,0443
0.8369
-0,0350
0.2710
0.0286
0.2399
-0.0204
0.0923
0.2575
-0.1791
CHT-15.00
GAMMA- 1.5
ZETA*
1.50
X/H*
-2.00 Y/H*
IW.L )
(U.L)
(W.D)
(U.D)
0,0030
0.2044
0,0256
0,7904
0.0176
0.2145
0.012?
0.1668
0.0399
0.0702
0.2011
-0.1848
CHl-30,00
GAMMA* 1,5
ZET A =
1.50
X/H*
-2.00 Y/H-
(W.D
(U.L)
(W.0)
(U.D)
0.0343
0.1595
0.0065
0,7565
0.049?
0.1702
-0,0052
0.1137
0.0787
0.04B3
0.1559
-0.1866
Z/H* 0.
ETA* 1.00
■0.0442
0.2701
0.0016
0.3930
-0.2788
0.0016
0*2701
-0.1760
-0.0059
-0.0093
0.0427
0,4439
0,0093
0.0009
0.0270
-0.1532
Z/H* 0.
ETA* 1.00
0.0086
0.2138
-0.0139
0.3218
-0.2014
-0.0139
0.2138
-0*1814
-0.0056
-0.0094
0.0395
0.4687
0.0090
0.0007
0.0261
-0.1550
Z/H* 0.
ETA* 1.00
0.0399
0.1697
-0.0305
0.2689
-0.1492
-0.0305
0.1697
-0.1826
-0.0056
-0.0102
0*0370
0.4875
0.0093
0*0006
0*0253
-0.1558
CH I *45 • 00
GAMMA* 1.5
ZETA*
1.50
X /H=-2 . 00
Y/H*
(W.L)
(U.L)
(W.D)
(U.D )
0.0515
0.1224
-0.0119
0,7299
0.0677
0.1347
-0.0226
0.0714
0.1044
0.0274
0.1182
-0,1851
CHI *60,00
gamma* 1.5
Z FT A =
1.50
X/H*-2,00
Y/H*
IW.L)
(U.L)
(W.D)
(U.D)
0.0579
0.0912
-0,0293
0,7081
0.0768
0,1068
-0,0399
0.0373
0.1218
0,0074
0,0860
-O.1803
CHI *75 .00
GAMMA* 1.5
ZETA*
1.50
X/H*-2.00
Y/H*
(W.L)
(U.L)
(W.D)
(U.D)
0.0545
0,0654
-0.0451
0.6892
0.0780
0.0874
-0,0574
0,0091
0.1333
-0.0117
0*0570
-0,1720
Z/H* 0.
ETA* 1.00
0.0573
0.1343
-0,0469
0 • ?272
-0.1122
-0.0469
0.1343
-0,1801
-0*0058
-0*0120
0.0350
0.5027
0*0104
0.0004
0,0243
-0,1559
Z/H- 0.
FTA* 1.00
0.0642
0.1069
-0.0629
0.1927
-0.0851
-0.0629
0.1069
-0. 1732
-0.0064
-0,0157
0.0336
0.5154
0*0126
-0.0001
0*0230
-0*1554
I
M
O
ETA* 1.00
0,0610
0.0897
-0.0781
0.1632
-0,0644
-0.0781
0,0897
-0,1596
-0.0065
-0.0243
0.0330
0.5260
0*0170
-0.0023
0*0207
-0*1541
CHI "90*00 GAMMA 3 1*5 ZETA*
(W.L)
(U.L)
tW.D)
(U.D)
0.0452
0.0583
-0.0583
0.6720
1.50 X/H—2.00
0.0730
0.0757
-0.0757
-0.0135
0.1404
-0.0298
0.0298
-0*1628
Z/H* 0.
0.0473
0.0917
-0.0917
0.1375
ETA* 1*00
-0.0473
-0.0917
0.0917
-0.1375
- 0.0021
-0.0334
0.0334
0*5345
0.0257
-0.0160
0.0160
-0.1510
44
TABLE 5.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.50, AND 0 = 1.00
(b) x/H = -1.00
8
Correc
tion factors for
correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
.
to grour
id effect
0.
_ ' fW.U
fu,u
rw,oj
(U.D)
GAMM As l # 5
-0,4784
0,8838
-0,4659
1.3319
Z ?TA*_ _ i*50 x/H =- 1 ,00 y/hs o,
-0.4352 -0,2264
b*8?73 “0,3 94ft
-0,4987 0,879 9
1.1198 -0.1971
— FTA=_ 1. 00.
-0,4584 -0,6635
_ 9 *993 9 _ —0 | 527?
-0,5272 0 , 89 3 9
1.1847 —0,7011
-0.020ft
-0.01 Oft
0.061?
0,147p
ft. 023 ?
... 0.0034
0, 0?ft*
-0,0644
CHI-15.00
GAMMA = 1,5
ZCTA= 1,50
fW.L)
(U.L1
-0,2301
0.7115
-0.1874
0.7256
-0.3516
0.B147
-0.0410
(W.G j
<u.n 1
-15,3203
1.0927
0 .- 7073 -
-0,2963
. CHI-30,00
_GAMM A - 1,5
7F"T A* lj|50 _
X/H 5 -I t 00 Y/J4 =
fW.L)
(U.L)
(w.or
(U.D)
-0,0859
0.5642
-0.2546
0,9181
-0*0408
0,5800
0,090?
_ _-0. 18 9 1
-0 * 28 51
0.5885
0,5594
-0,3432
2 /H = 0. FT A = l_.ftO
-0,2106 -0,4410
“0,3796
-0.3796 0.7721
0,8956 -0, 7997
-0,0197
-0.01 06
0.0593
0.1970
Z/H= 0.
-0.06*17
0*5/62.
-0.3124
0.6821
. ETA= 1.0ft
-0,7861
-0»3124_
0.5767
-0. 346?
-0.0706
0*0578
0,2360
CHI =45.00 OAMMA = 1,5 ZFTAs
(W»U -0,0096
fU»L) _ 0,4395
fW,0i '"-0,2273
f U.D) 0,7867
1.50 X /H=— 1 ,0ft Y/Hs 0,
0,041 4 0,1877
. -0.1661
■0.2581 0.4337
0.4144 -0,3533
Z/H =
0.
0,0]36
0 • 4 5 44
-0.PS42
0,6] H?
FTA = 1,00
“0,1776 _n,ft ? 31
-0.284? -0.0] 49
0,4644 0.0569
“0.3668 0.7604
0.0731
— Q.0035
0.0?80
-0,0809
0.0244
—0. QC_31L
0.0272
-0.0936
0,0?79
O.JIO 44
0*0767
-0, 1038
■ C H 60*j)0 G A MM A = 1,5
fW»L) 0,0150
U, * L J _ 0.3368
-0.2 186
(U»D| 0,6858
ZF J.*~ 1*50 X/H = -1,00 Y/h=
0,0/76 0,24/3
.0,3632 -0,1606
-0.2617 0,3 7.8 8
0.2771 -0,33??
0. 7. /H-r 0
0,0429
0,3678
-0,7766
0.3893
• FT A- J A 00
-0,097ft
-0.2756
0,8678
-0,3387
-0,0780 0.0347
-0.0210 HaOI154
0.0570 0.0740
0.?966 -0.H21
c .^L= 7 5j_0<L _GAMMA= 1,5
(W,LJ
(U.L )
(W.DJ
(U.D)
-0,0044
0,2574
-0,2161
0.6080
ZETA= 1.50 X/H=-1,00 Y/H= 0
0,0793 0.2 917
0*3002 -ft, 164?
“0.2561 0,2443
0.1687 -0,2847
2/H= 0, E Ta- i*o n
_ 0 .0312 _ “0.0379
0.2939 -0.7754
— 0 .7754 0.2979
0,7871 -0,7797
“0.0365
0.0593
0,3?09'
0*0Aai_
0,0063
0.01 9?
‘0*11 84
jCHI =90.00 GAMMA= 1,5
fW.L) “0,0454
<U._U 0.2084
rw.oi -0,2004
<U»DI 0,5463
ZE 1* = . 1 • ><} .. _ X /H_=-l_, 00 _ _Y / H = 0.
0,0624
_ 0 , 26 83 _
-0.2683
0.0865
0 , 3 72 3
■0.169 1
0,1 6' 91"
■0,2331
7 = . f}.*L FTA = 1,0ft
-0.0086 0 « 000 6
..0.7750 _ _ “0,775ft
-0,2750 0,?7 5 0
0,7063 -0.706?
-0,0368 0*0710
-0.0067
°»°666 0.0067
0.3400 -0*1198
6 t^T-1
L-1549
45
TABLE 5.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.50, AND TJ = 1.00
(c) x/H = y/H = z/H = 0
Correction factors for correcting from a wind tunnel which Is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHf=-3.00
bAM«A= 1.5
7FTA =
1.6(1 X/Hr
0. Y/H" 0.
z /h - n.
E T A - ! .on
(Will
-3,773?
— 3 , 7C 8 ?
4.8598
-3.7424
4.2210
-0.0307
0.0337
( u » L ]
-C.?37«
-0. 7381
-4. 7496
-C.23P0
-4.3775
0.0002
-0.0001
[ w'l'n'i' - '
zrzr."T77?
44“ 34 5 9
' -O'. 78 77
-7, .-3 775
“ -0.7380 “
" 0.0553
' '73.0715-'-
( U »D )
-0.2263
0.1309
1 .BR03
0.0371
1 . 8687
-0.2585
0.0987
CHI» 3.00
G>A^ M A = 1,5 '
7FTA =
1 Y7H=
0. Y77T=''0.
Z /H - 0.
ETA* 7 700 '
"7V.T7 '
-T. 773 2
fog?
T.9«ai
-3.7974
T-.7 22*
- —
-&7033T-
UMI
0,2 37R
0.53B1
-4.0525
0.2380
-4.1816
-0. 0002
o.nooi
( W ♦ D 5
• =7T7175Tr _
-G~ t T^TfVI -
'*■ 'nv 79 tt
— 6 . IP
777380'
0 7!T5'^9'
“Tr.T7i3
< i r , 0 1
0.2476
n, Bfop
T. 460?
0.6807
1 .8687
-0.2337
0.0891
chi - 1 6 . on
GA M ‘«A* 1.6
7ETA-
L'O X/H~
a. y/h^ 0,
' Z7H= D.
ETA= 1.00
f W f L )
-3,3744
-3, 3079
2.4R5R
-3*0477
1 . 8835
-0.0317
0.0348
|M,| )
i , oon 5
* , 09 1 4
-3.3293
1.0910
-3.4607
-0.0008
0.0003
( w*Di
-V.40 3 5"
—3,4238
1.089 9“
-3.4603
1.07T0 '
0.0568“
0.0'3T4“
iu»D)
0 . 9 ] 7 5
1.1716
• 1.5513
1 . 1 007
1 .5797
-0.1 877
0.0715
CH I = 3C * 00
GA MP -*A = 1.5
ZE T A =
*. R 0 X/H-
0 . y/h= 0.
Z / H ^ 0.
' ETA = T . 00
( W,L )
-P.3R51
-7.3115
1 ,4500
-7. 3600
0.8779
-0.0351
0.0385
( U»L)
1 .6539
1 . 6665
-3 » 2 2 1 1
1 , 0 * C. R
-7.3576
-0. 0019
0.0008
( W»D J
-2.' 1 9 5 9
^7. 3'? .2 4'
' T ,f R3 0 "
- -7, 7570
1 »"6"55“8
070577
OY03 12 -
< I i * D J
1.1157
1 . 30 c *
0.7710
1.2564
0,7570
-0*1407
0.0531
th L^.nO
Q w A - 1 , c
7ETA-
• , - 0 X /H ”
0. Y/H= 0.
Z/H= n.
eta= l.nn
f V*L )
-1 ,3860
-1.7966
1.1025
-1.3429
0.5451
-0.0421
0.0463
f 1 1 » L )
1.5614
1,4669
-1.3398
1 .5644
-1.4737
-0. nn40
0.0015
f w t D i
"-1,4146
-1.4426
“ “T. 5597"
-7.4-707' "
0756-84
0 , 77586
TTiOTOF”
f U * D )
0.8363
A. 9729
0,0616
0.936 1
0.0461
-0.0998
0.0368
CHI =60.00
GA'^ M A~ 1.6
7 4 T A =
1 , 4fl X/H-
0, Y/H" C.
Z / H“ 0.
E T A = 1.00
~ f tai * L »
-0,7948
-0,4767
1 .0478
-0.7386
0.5152
-0.0563
0.0623
(11. L!
1 . 1 1 4 5
7 . 1 774
-0*8297
1. 1242
-0.9636
-0. nr, 90
0.0033
{ W * D )
- 0 » 9 n 4 ?
-0. 9346
1.1114
-0 * 9 6 ?6 '
' I. 1247
0.0604
“0.71297
JU.D)
0,4477
0.4267
-0.2267
0.5051
-0.2^62
-0.0625
' — ' 0.0216
--"CHI a 7 5 . 00 __
G A M w A = 1.5
Z£TA=_
••.^0 X /H =
0. Y/h* c.
Z / f-f= 0.
ETA* 1.00
' '
( W * L )
-0,6371
-0.45 3.P
1.0593
-0.5516
0.5350
-0.0855
0.0978
(UiLI
0,7074
O. 74?4
-0.5674
0.7347
-0.7017
-0.0773
oLoron
f W, D )
- 0 . 6 ’ 4 4
-0.6780
0.6966
-0.701 8
0.7347
0.0.65R
tr.TTTTT “
( i J ♦ D >
0.1596
0. ’943
-0. 1451
n.i 83i
-0,1670
-0.0775
0-.CT777
_ rHl*oo,n;i
G A ‘ ‘ A “ 1 . K
7 1 T A~
' . c 0 X / H ~
n, Y/H- 0,
Z/H* 0.
ETa= 1,00
“ - - -
—
( 1,1 < L )
-0.6534
-0. 3^67
1.0467
-0.5371
0.5371
-0.1162
0.1605
( IJ i l )
0,
0 . c 3 O 3
—0,6041
‘ 0,6371
-0.3371
-n.nP63
— IT .71071 '
( W.D)
-0.^50 A
-0 . r - 3 0 3
' ' 0,4050
“ ' -n;6*7i ■
“'"TV. 5 777
0. 08 b 'i
-0.0021 —
f u«n >
-O.0000
0 . ^ 0 0 0
-0.0000
-0,
0 •
-o.nnno
o.nnno
h6
TABLE 5.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1-5°. AN 0 V = 100
(d) x/H = 1.00
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
*
CHI- 0,
l
GAMMA = 1.5
ZETA*
1*50
X/H=
1,00
Y/H* 0.
Z/H* 0.
ETA* 1*00
(W.L)
(U*L)
(W.D)
(U.D)
-0.4784
-0.8838
-0.9077
-1,5283
-0.4352
-0.8973
-0.9084
-0.8477
9.4824
-0.8602
-0.8799
-0*1971
-0.4584
-0.8939
-0,9397
-1*0161
8.6978
-0.9397
-0.8939
-0*2011
-0*0200
0*0100
0*0320
-0*5122
0.023?
-0.0034
0,0313
0.1684
CHI -15.00
GAMMA- 1.5
ZET A =
1.50
X/H*
1.00
Y/H* 0*
Z/H* 0.
ETA* 1.00
(W.L )
(U.L)
(W.D)
(U.D)
-0.9106
-1.0850
-1 .2648
-1.5656
-0.8598
-1.0839
-1,2529
-0.8742
9.1439
-1.2134
-1.0810
-0.0347
-0.8868
-1.0877
-1.2924
-1.0618
8.3826
-1.2924
-1.0877
-0,0125
-0*0237
0*0028
0*0276
-0*5038
0,0271
0*0038
0*0395
0*1876
CHI-30,00
GAMMA- 1,5
7.ETA*
1.50
X/H*
1.00
Y/H* 0*
Z/H* 0.
ETA* 1*00
t W *L 1
(U.L)
(W.D)
(U.D)
-1.693?
-1.2439
-1,6990
-1.4583
-1,6406
-1*2586
-1*7032
-0*8584
8,4887
-1 .6441
-1.2397
0.3666
-1 .6697
-1.2547
-1*7361
-1*0117
7.7432
-1,7361
-1,2547
0.3604
-0*0255
0*0108
0*0371
-0*4465
0*0292
-0*0039
0*0329
0*1534
CHI-45.00
GAMMA* 1.5
ZFT A =
1*50
X/H*
1 .00
Y/H* 0,
Z/H* 0.
ETA* 1.00
(W.L 1
(U.L)
(W.D)
1 U * D )
-3.1664
-1.0328
-2.2100
-1.1191
-3*0956
-1*0497
-2.2144
-0,5539
7.0523
-2.1517
-1 ,0280
1.1270
-3.1332
-1.0451
-2*2485
-0*7000
6.3223
-2.2485
-1.0451
1.1100
-0*0332
0*0123
0*0305
-0*4191
0,0376
-0*0045
0*0341
0*146?
CHI-60.00
GAMMA* 1.5
ZETA*
1.50
X/H =
1.00
Y/H* 0.
Z/H= 0.
ETA* 1.00
(W.L)
(U.L)
(W.0)
(U.0)
-4,0364
0.8981
-1.9651
-0,2635
-3.9288
0,8781
-1.9685
0*2678
4.1013
-1.9032
0.9035
1.3898
-3.9857
0,8837
-2*0042
0.1294
3.3847
-2.0042
0.8837
1.3743
-0*0507
0*0144
0*0391
-0*3930
0*0569
-0*0056
0*0357
0*1304
ChI-75.00
GAMMA = 1.5
ZETA*
1*50
X/H*
1.00
Y/H= 0*
Z/H* 0.
ETA* 1,00
(W.L)
(U.L)
(W.D)
(U .0 )
-1.7890
0.8051
-0,6861
-0.3886
-1*5733
0*7911
-0*6900
0*1044
2.3339
-0.6217
0.8078
0.1304
-1*6871
0.7957
-0.7264
-0*0235
1.6271
-0.7264
0. 7957
0,0976
-0.1019
0.0094
0.0403
-0.3652
0*1138
-0.0046
0*0364
0*1270
CH! -90,00
GAMMA* 1.5
ZETA*
1*50
X/H*
1.00
Y/H* 0*
Z/H* 0,
ETA* 1*00
(W.L)
(U.L)
(W.D)
(U.D)
-1.2613
0.2084
-0.2084
-0.5463
-0*8158
0.26B3
-0*2683
-0*0865
1.7710
-0.1691
0.1691
0.2331
-1.0657
0*2750
-0*2750
-0.2063
1.0657
-0.2750
0*2750
0.2063
-0*1956
-0.0666
0.0666
-0*3400
0*2499
-0*0067
0*0067
0*1198
6 ^ 1-1
47
£
I
TABLE 5.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = l * ~ l ' 50 > AN °
(e) x/H = 2.00
Correction foctors for correcting from a wind tunnel
which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
■
closed
on bottom
only
to free air
to ground effect
— T
(W.L)
I U f L 1
IW.DI
(U.D)
GAMMA* 1.5 ZETA- 1.50
X/H* 2.00 Y/H* 0.
-0.0502
-0.2609
-0.2612
-1.0289
-0.0350
-0.2710
-0.2499
-0.2752
9.5551
-0.2334
-0.2575
-0.1791
Z/H* 0.
-0.0442
-0.2701
-0.2734
-0.4223
ETA* 1.00
6.6698
-0.2734
-0.2701
-0.1760
-0.0059
0.0093
0.0122
-0.6066
0.0093
-0.0009
0.0235
0.1471
CHl »15 .00
(W.D
(U.Ll
(W.D)
(U.D)
GAMMA* 1.5
2ETA* 1.50 X/H* 2.00 Y/H* 0.
-0.1437
-0.3403
-0.3504
-1.0660
-0.1267
-0.3512
-0.3407
-0.3221
9.4739
-0.3201
-0.3367
-0.1840
Z/H* 0.
-0.1357
-0.3455
-0.3609
-0.4556
ETA* 1.00
8.6218
-0.3609
-0.3455
-0.1642
-0.0080
0.0053
0.0105
-0.6104
0.0090
-0.0056
0.0202
0.1334
CHI *30.00
(W.L )
IU.LI
fW.D)
(U.DI
GAMMA* 1.5
ZETA* 1*50 X/H* 2.00 7/ H* 0.
-0.3165
-0.4429
-0.4611
-1.0652
-0.2956
-0.4553
-0.4521
-0.3303
9.3227
-0.4285
-0.4386
-0.1429
Z/H* 0.
-0.3080
-0.4540
-0.4781
-0.4832
ETA* 1.00
8.4795
-0.4781
—0. 4540
-0.1396
-0.0085
0.0111
0.0169
-0.5820
0.0124
-0.0013
0.0260
0.1529
CHl *45.00
IW.L)
(U.L )
(W.D)
(U.D)
GAMMA* 1.5
ZETA* 1.50
X/H* 2.00 Y/H* 0.
-0.6989
-0.6132
-0.6390
-1,0745
-0.6702
-0.6293
-0.6300
-0.3487
8.9867
-0.6037
-0.6079
-0.0817
Z/H* 0.
-0.6869
-0.6272
-0.6574
-0.5033
eta* i.oo
8.1526
-0.6574
-0.6272
-0.0786
- 0.0120
0.0140
0.0184
-0.5712
0.0167
- 0.0021
0.0274
0.1546
CHI *60,00
IW.LI
(U.L)
(W.D)
IU.0)
GAMMA* 1*5
ZETA* 1.50 X/H* 2.00 Y/H* 0.
-1.8340
-0.9023
-0.9758
-1.0525
-1.7845
-0.9263
-0.9645
-0,3351
8.0101
-0.9370
-0.8946
0.1715
Z/H* 0.
-1.8126
-0.9225
-0.9945
-0,4912
ETA* 1.00
7.1841
-0.9945
-0.9225
0. 1738
-0.0214
0.0202
0.0186
-0*5613
0.0281
-0*0039
0.0300
0.1561
CH I *75.00
(W.L)
(U.L)
(W.D)
(U.D)
GAMMA* 1.5
ZETA* 1.50 X/H* 2.00 Y/H* 0.
-3.4570
0.9156
-0.9091
-0.5148
-3.3150
3.8735
-0.8881
0.192C
3.8638
-0.8631
0.9283
0.5093
Z/H* 0.
-3.3926
0.6820
-0.9243
0.0357
ETA* 1.00
3.0439
-0.9243
0.8820
0.4996
-0.0652
0.0335
0.0152
-0.5505
0.0776
-0.0086
0*0362
0.1563
CHI *90.00
(W.L)
(U.L)
(W.D)
(U.D)
GAMMA* 1.5
ZETA* 1.50 X/H= 2.00
Y/H* 0.
-1.3520
0.0583
-0.0503
-0,6720
-0.8263
0.0757
-O.C757
0.0135
1.9529
-0.0290
0.0298
0.1628
Z/H* 0.
-1.1216
0.0917
-0.0917
-0.1375
ETA* 1.00
1.1216
-0.0917
0.0917
0. 1375
-0.2304
-0.0334
0.0334
-0.5345
0.2953
-0.0160
0.0160
0.1510
48
TABLE 5.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 1.50, AND ij= 1.00
(f) x/H = 3.00
Correction factors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
o/>ly
to free air
' ' r ~ — —
to grour
id effect
CHI * 0.
GAMMA* 1,5
ZETA* 1.50 X/H* 3,00 Y/h* u.
Z/H* 0.
ETA* 1,00
(W»L>
CUtL 1
(W,D)
(U *D 1
“0 * UO 8 4
-0*1110
-0,1244
-0,8392
-0,0048 9,5594
-0,1152 -0,1041
-0,1096 —0,1094
-0,1184 —0,0985
-0*0079
-0,1164
-0,1248
-0,2244
8.6535
-0.1248
-0.1164
-0,0*53
-0,0005
0.0054
0.0004
-0.6147
0,0031
0,0012
0.0152
0.1060
CHI *15.00
GAMMA= 1,5
ZETA* 1,50 X/H* 3 , ou Y/H* o.
^/H* 0.
E f A* 1.00
(W*L)
(U»L)
(W.DJ
(U.D)
-0,0468
-0*1444
“v, 1592
-0,8536
-0,0426 9,5225
-0,1481 -0,1379
-0,1446 -0.1427
-0.1248 -0,0982
“J « 046u
-0.1497
-0.1612
-0.2362
8.6230
-0.1612
-0.1497
-0.0938
-0.0007
0.0053
0.0020
-0,6154
0,0035
0,0016
0,0166
0,1134
CHI =30*00
GAMMA* 1,5
ZEfA* 1,50 a/H* 3,00 Y/H* U,
4/H* 0,
E 1 A* 1,00
(W,L)
( W » D I
{U*0V
-0,0872
—0,2446
-0.1531
-0.9541
-0,1445 9.4226
-0.1426 -u.1309
-U,247y -0.2425
-0,0415 -0,0021
-0.1174
-u, 1976
-O.21o5
-0.25U0
6. 5597
-0.21u5
-0.1976
-0,0905
0.0302
-0,0470
0.0574
“0.7041
-0,0271
0,0550
-0,0365 .
0,2085
CHI»45.0Q
GAMMA* 1,5
ZE1A* 1,50 X/H* 3,00 Y/H* 0,
Z/H = 0.
ETA* 1.00
( W.L J
iU.LJ
“ fw#Dr
(U » Df
-0,2745
-0,2663
-0.2820
-0.8705
-0,2671 9.3042
-0.2738 -0,2587
-0.2685 -0,2636
-0.1404 -0.0881
-0.2728
-0.2751
-0.2868
-0.2604
8.4149
-0,2868
-0.2751
-0.0832
-0.0018
0.0086
0.0048
-0,6100
0*0057
0,0013
0.0183
0,1201
CHI-6Q.00
GAMMA* 1,5
ZETA* 1,50 X/H* 3,00 f/H* 0.
Z/H* 0.
EVA- 1,00
fW.L)
(U»Lr
-0.7245
-0.4154
-0.7104 8,8751
-0,4277 -0.4012
-0,7203
-0.42 90
-0.4314
-0,2690
7,9903
-0.4314
-0.4290
-0.0582
-0,0042
0.0136
0,0053
-0,6086
0,0100
rw*oi
(U»D|
-0,4260
-0.8776
-0.4115 — U,41o9
-0,145o -U.u652
0,0013
0.0199
0*1239
CHI -75.CO
GAMMA- 1,5
aETA* i»pC A/H* 3,00 Y/H* 0,
Z/H- 0,
ETA- 1.00
IW»L)
fU*L)
-3.3526
-0.7097
-3.2939 6.5375
-0.7422 -0.8211
-3,3291
-0,7408
5.6570
-0,8537
-0,0234
0,0353
{ W » J )
“ W • w ^ v
0,0311
-0.0014 ""
fU ♦ D J
-0,8322
-0,0957 0,4206
-0,2242
0.4295
o 0 ou;U
-0.6080
0» Ut «*o
0*1265
CHI *9 J.CU
GAMMA* 1,5
ZETA= 1.50 X/H* 3.00 Y/H* 0,
Z/H* 0,
EVA- 1,00
- ■ ~
(W.L)
iUtL)
- rw.or —
-1.3460
U.0252
-0,0252
-0,7979 2,0065
0*0203 — U*0o34
-0,0203 0.OO34
0,0458 0,u955
-1 • 1 u90
0,0360
-0,0360
— 0,u81O
1.1090
-0.0360
0. Q36u
0.0810
-0.2370
-0.0108
0,3111
-0,0157
fU » D )
-0,6824
0,0108
-0.6015
" ffV'015?
0,1268
6 -^ 1- 1
L-15^9
TABLE 5.- Continued
IS
k9
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1-T*, ? = 1.50, AND Tj = 1.00
(g) x/H = 4.00
Correction foctors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
GAMMA® 1.5 ZETA® 1.50 X/H = 4.00 Y/H® 0.
ETA- 1.00
< W.L I
-0.0016
-0.0010
9.5618
-0.0021
8. 63J5
0 . 0*05
(U.L)
-0.0609
-0.0621
-0*0581
-0.0636
1
0.0027
( W.D )
-0.0759
-0.0605
-0.0602
-o.n*’/
-0.0696
-0.0058
( U » D )
-0.7284
-0.0642
-0.058*
0.1384
-0. 0566
-0.5900
0.0011
0.0015
0.0095
0.0742
CHI * 15.00 r%t '
ZETA® 1.50 X/H* 4.00 Y/H® 0.
1/ H- 0. ETA* 1.00
(W.L)
-0.0226
-0.0220
9.5407
-0.0232
8.6159
0.0005
(U.L)
-0.0793
-0.0804
-0.0763
-0.0821
“0.0897
0.0027
(W.D)
-0.0944
-0*0796
-0.0785
-0.0897
-0.0821
-0.0047
(U.D)
-0.7393
-0.0658
-0.0579
-0*1451
-0.0565
-0.5942
0.0012
0.0017
0.0101
0.0793
CHI-30.00 GAMMA = 1.5
ZETA* 1.50 X/H= 4.00 Y/H® 0.
Z/H = 0* ETA® 1.00
( W.L 1
-0.0620
-0.0611
9.5017
-0.0626
8.5799
0*0005
(U.L)
-0,1051
-0.1068
-0.1022
-0.1085
-0.1 167
0*0034
(U.O)
-0.1207
-0.1057
-0.1042
-0.1167
-0. 1085
-0.0040
(U.O)
-0.7472
-Q.C68*
-0.0580
-0.1508
-0.0558
-0.5964
0.0015
0.0017
0.0109
0.0624
CHI *45.00 GAMMA = 1.5
ZETA® L. 50 X/H= 4.00 Y/H* 0.
Z/H =
0.
ETA* 1.00
t W * L )
(U.L )
( W *0 >
( U « 0 >
“0.1481
“0.1510
“0.1587
-0.1559
8*4980
-0. 1587
-0. 1510
-0. 0542
CHI *60*00 GAMMA® 1.5
X/H* 4.00 Y/H® 0.
Z/H = 0. ETA* 1.00
(W.L)
-0,3927
-0.3898
9,1754
-0.3932
8.2588
0.0005
(U.L)
-0.2272
-0*2315
-0.2222
-0.2344
-0.2388
0*0072
(W.D)
-0.2416
-0.2264
-0.2252
-0.2388
-0.2344
-0.0028
(U.D)
-0.7612
-0.0715
-0.0541
-0.1605
-0.0496
-0.6007
0*0035
0.0029
0.0124
0.0890
CHI-75.00 GAMMA® 1.5
ZETA® 1.50 X/H* 4.00 Y/H* 0.
Z/H* 0. ETA* 1.00
(W.L )
-1.7394
-1.7230
7.8692
-1.7358
6.9553
-0.0036
(U.L)
-0.4759
-0.4910
-0.4549
-0.4952
-0.4727
0.0193
(W.D )
-0*4760
-0.4582
-0.4698
-0.4727
-0.4952
-0.0033
(U.D)
-0. 7661
-0.0701
-0.0089
-0.1629
0.0017
-0.6032
0.0126
0.0043
0.0145
0.0928
CHI-90.00 GAMMA® 1.5
ZETA® 1.50 X/H* 4.00 Y/H* 0.
Z/H® 0. ETA* 1.00
(W.L)
-1.3338
-0.7812
2.0299
-1.0977
1.0977
-0.2361
(U.L)
0.0180
0.0053
0.0008
0.0170
-0.0170
0.0010
(W.D)
-0.0180
-0.0053
-0.0008
-0.0170
0.0170
-0.0010
(U.D)
-0.6539
0.0425
0.0581
-0.0510
0.0510
-0.6029
0.3165
-0.0117
0.0117
0.0934
50
TABLE 5.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 1.50, AND i) = 1.00
(h) x/H = 5.00
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
r 1 i—
GAMMA- 1*5
2LsA = 1*50
E7A- 1* .00
( « * L ) -0*u0«3
1 0 #L ) -y • y 38?
{ W i D } -0*0531
tU»D) -0*6464
— 0 * juu2
-0 *0389
"0 • 03 a 3
-u « J4J 7
*•5641
-u*0 368
—0 *0363
-o* u3»'J
“0 • GUQ7
-0*0399
-0 t 0444
-3 • uy 36
d*6219
“0* 0444
-a.G399
-u * 63 72
0*000^ 0*0003
. 0*0U.ii
-0*0067 0*U0oi
-0*352v 0*0329
GAMMA. 3 „1 . 3
£7 A- 1*00
{ W ♦ L ) -u#ul37
{ U »L ) -u*u_503
(W*0) -u#u649
SUtDJ -u*6558
-w*v>136
-o*u505_
-0*3501
-G*u413
9*5504
-U* U 484
-u*w49 9
-^•k.bbij
-0*0141
-Of Mill
— j • C5o7
-•^•0973
8 • 6 1 u A
.TV « v^o /
-0*0517
-3*0371
0* 6 JU5
__ v* 00.14
-0*0083
0*0003
. U»0012
0 • 006b
0*0300
CHI=3^*oL &AKMA= 1.5 itnA= 1*5 u a/H= 5*uu
E1A= 1*00.
( W » L )
( U » L )
I W »0 >
(U»0)
-0*4384
-0* «67 1
-w*^812
-0.663$
-0*0383
-0 *0 674
—0 • c665
-j*-423
9.5231
-0*0392
8*5871
0*0007
U * 00U o
-0*0644
-4*0664
-y* 0.736.
.OjiiiXiii
. CiOPlQ.
-w.0666
-u*0736
-0 « 0684
-0*0075
0*0073
— o • o 3 7 3
“G*10v4
-6*0369
-0*5635
U* 0381.
CHI=A5*uv> GAMMA- 1,5 4£iA= 1*50 a/H= 5*oJ _ >/H* o»
£_: A*. ..If 0-0
{ W *L ) -U*u925
< U *4. ) -0*0934
(w*D> -0*1074
tO»0) -0*6704
-0*0931
-0*0931
-0*0933
-v *0418
9*4706
-0*09.05
-0*0 92 8
“0*0374
-0*0935
-0*0952
-0* 1003
-0*1032
6* 5 344 O • OO 10
-Pi 1002 .0. 1.0 Oil.....
-u* U952 -0*0071
— 0* 0364 -0*5672
0*0003
__ 0*0 9*1
0*00 fO
0*0614
CHI =60* Ou GAMMA- 1*5 tE7 A= 1*50 _* 2 H = _ 5 • OU_ \t H= 0*
£TAr.._l*00
( W *L )
I 0 l L )
(W>0)
<U»L>)
-0*2482
-U * 1444
-0*1584
-u • 676v
-0*2478
— o *1449
—0*1434
-0*^426
9*3162
■w • 1 41 *.
>0*142 9
■0*0374
-0*2492
-V *1474
-0.1512
-0*1056
6*3811
-o*1312
-0*1474
-0*0351
Ofuolo
u *uu5»
-0*0072
-0.370J
0*0014
0*0023
o* up m
0*0634
CHI =75«Oo GAMMA 3 1*5
( W«L )
(0 f LI.
( WfQ )
uj*oi
i£TA= 1*50 X/h= 5*00
._A/W* v* . E,iA= 1.00
0*0013 0*0047
-0*0072 J ■ 0066
-0*5737 0*0655
CHI. ■90*0.0... GAMMA 3 1*5 <.£TA= 1*30 a/H = .5*.uO X/H=.ll* A/h=_ll*. EJA? 1*00-
( M *L )
-1*3252
-0*7720
2.0426
-1*0906
1*0906
-0*2346
0*3166
( u iLl
.0*0158
0 » vG 13
0*0014 . ....
QjUG92 ..
-0*_0092. . _
n*nn66
-0*0079 —
{ W»D)
-0*o 158
-0*0013
-0*0014
-0*0092
0*0092
-0*0066
0*0079
(U.D)
-O.6107
o*o324
U.U38U
-0*0345
0*0345
-0*5763
0*0666
6i£l-1
51
TABLE 5.- Concluded
LONC2TUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > - ^ ‘ 15 °’
(i) Miscellaneous additional values ot x/H
_ i,.nnnl Ulhirh i <*
s
Correction factors for correcting rrom a «m.u
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
to ground effect
1 ^ "
CHT-15.00 GAMMA* 1*5 ZETA=
1*5C X/H- 0.18 Y/H* 0*
£
H
I
( W * L )
IU.L J
(W.D)
(U.D)
-3.8243
0.1303
-3.8151
- 0.0201
-3.7581
0.1278
-3*0366
0.3286
4 * 4 445
-3*7436
0.1310
1.8837
CHI-30.00 fiAMMA* 1.5
ZETA* 1<
60
X/H* 0.39 Y/H* 0.
( W »L )
(U.U
IW.Dl
(U.D)
-3.9265
0.2227
-3.3439
-0.1459
CHl*45.00 GAHMA= 1.5
(W.L)
(UtL)
(W.D)
IU.0I
-4.0916
0.2875
-2.7683
-0.3154
CHI =60.00 GAMMA* 1*5
(W.L)
(U.D
(W»D)
(U.D)
-4.2839
0.2261
-2.0129
-0.5360
CHI *75 . 00 GAMMA* 1.5
(W»L)
(U.U
[W.D !
(U.D)
-3.8546
0.2168
-3.3617
0.2390
4.5921
-3.2743
0.2243
1.8530
1*50 X/H* 0.67
Y/H=
-4.0086
0.2760
-2.7803
0.1377
1*50
-4.1849
0.2032
-2.0125
0.0419
4.7580
-2.7021
0.2906
1.76B5
,16 Y/H*
5.0053
-1.9546
0.2325
1.5424
-3.0326
0.9396
-0.8355
-0.4955
ZET A= 1.50
-2.8729
0.8992
-0*8166
0*1903
X/H= 1.82 Y/H* 0.
3.5032
-0*7860
0.9514
0.3482
Z /H* 0.
-3.7927
0.1286
-3.8687
0.2324
ETA = 1*00
3, 8080
-3.9687
0. 1286
1.8718
-0.0316
0.0017
0.0536
-0.2526
0.0346
- 0,0008
0.0321
0.0962
Z/H* 0.
ETA= 1.00
-3.8923
0.2186
-3*3946
0.1336
3.9407
-3*3946
0.2186
1 . 8405
-0.0343
0.0041
0.0508
-0,2795
0*0377
-0,0018
0.0329
0.1053
Z/H= 0*
ETA* 1*00
-4.0522
0.2793
-2.8143
0,0159
4.0775
-2.B143
0.2793
1.7551
-0,0393
0.0081
0.0460
-0.3313
0.0436
-0.0034
0,0340
0.1218
2 /H* 0.
ET A = 1,00
-4.2375
0.2093
-2,0482
-0.1056
4,2667
-2.0482
O. 2093
; • 5300
-0.0464
0.0168
0.0353
-0.4312
0.0527
-0.0061
0.0356
0.1475
Z/H= 0.
ETA* 1.00
-2,9509
0.9082
-0,8542
0.0331
2,6989
-0,8542
0.9082
0,3336
-0,0737
0.0314
0.0187
-0.5286
0.0860
-0.0090
0.0376
0.157?
52
TABLE 6
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND rj = 1.00
(a) x/H = -2.00
8
Correc
lion factors for correcting) from o wind tunnel which is 1
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
»d effect
' \
, 4
fW*L 1
*U.L)
(W.D)
ruiD)
GAMMA* 1*5
ZETA* 2.00
-0*0265
-0,0194
0,2608
0,2647
0.0891
0.0840
0,8503
0.2365
X/H— 2,00 Y/H- 0. 2/ H» 0#
-0,04^1 -0*0236
0*1255 0*2651
0*2581 0*0618
-0,2074 0*3894
ETA* 1,00
-0*2933
0*0618
0,2651
-0*2061
-0,0029
“0*0043
0*0273
0,4609
0*0042
“0*0005
0,0221
“0*1529
CHI-15,00 GAMMA* 1,5 ZETA*
<W*U> 0*0242
tU*U) 0*2044
<W,D1 0,0561
*U»D) 0,8092
2,00 X/H*-2,00 Y/H= 0*
0*0311 0,0184
0,2083 0,0905
0*2016
0,1768 -0*2095
Z/H* 0*
0,0270
0*2068
0*0304
0*3307
ETA* 1*00
-0*2181
0*0304
0,2088
“0,2082
“0,0028
-0*0044
0,0257
0*4784
0,0042
-0*0005
0*0215
-0.1539
CHI *30,00 GAMMA- 1,5 ZETA*
(WpL.) 0,0545
fu *U 0,1596
fW*0) 0,0273
fU,D) 0,7784
2,00 X/H— 2*00 Y/H* 0,
0,0618 0,0588
0,0600
0*0237 0*1566
0,1321 -0*2097
Z/H* 0*
0,0574
0,1644
0*0028
0*2864
ETA= 1*00
-0,1677
0*0028
0*1644
- 0.2001
-0*0029
-0,0048
0,0244
0,4920
0,0044
-0,0006
0*0209
-0,1543
CHI-45.00
GAMMA* 1,5
ZETA* 2.00
X/H— 2 * 00
Y/H*
f W * L )
(u.n
(W*0l
f U *D J
0,0719
0.1227
0*0015
0,7539
0,0801
0.1277
-0,0016
0,0964
0*0860
0,0329
0.1192
-0.2078
CHI-60,00
GAMMA* 1,5
ZETA* 2.00
X/H— 2.00
Y/H*
(W.L)
fU.L)
fw*0l
(U*0)
0,0794
0,0923
“0,0220
0,7333
0.0895
0,0988
-0,0250
0.0666
0*1046
0*0079
0,0877
“0.2035
0, Z/H* 0,
ETA- 1,00
0.0750
0.1285
-0.0219
0,2508
-0. 1320
-0.0219
0* 1285
-0.2050
-0*0032
-0,0058
0.0234
0.5031
0*0050
-0*0008
0*0203
-0*1544
0* Z/H* 0.
ETA* 1,00
0*0031
0*1002
-0,0446
0,2207
-0.1059
-0.0446
0*1002
-0*2006
-0.0037
-0,0079
0,0226
0*5126
0*0063
-0*0013
0*0196
“0*1541
CHI-75, 00
<W*L1
<U,L)
fW.D)
fU.DJ
GAWA« 1,5 ZETA*
0,0775
0,0686
-0,0436
0,7150
X/H— 2,00
0.0912 0,
0.0787 -0,
-0,0474
0,0411 -0,
Y/H* 0. Z/H* 0.
'1173 0,0820
0155 0.0818
0615 -0.0659
1956 0,1944
ETA* 1.00
- 0*0862
-0.0659
0.0818
“0*1902
“0.0046
“0*0132
0.0222
0,5206
0,0091
-0.0032
0*0185
- 0.1532
CHT *90, 00
IW*U
(U*L )
<W*D|
(U»D)
GAMMA* 1,5 ZETA* 2.00 X/H— 2.00
0,0672
0,0627
-0,0627
0,6976
0,0860
0,0696
“0.0696
0,0202
0.1258
“0.0376
0.0376
-0.1850
Z/H* 0*
0.0700
0,0854
“0*0854
0.1708
ETA* 1.00
-0*0700
—0* 0B54
0,0854
-0.1708
-0*0028
-0*0227
0*0227
0*5268
0*0160
“0*0159
0*0159
“0.1506
6^1-1
L-15^9
53
TABLE 6.- Continued
LONCZTU1XNA L DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND tf = 1.00
(b) x/H = -1.00
fw.L )
_( U . L )
i w » d r
(u.n )
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
GAMMA = 1*5' ZFTA = ? .00 "x/H^i'.OO Y/h =
-0.3546
1 ,:''?49
-0,306 7'
1,6167
-0,3355
_ 1 ,0?9 3
-0,3196
1,346 f
-0, *903
c,fl Q
1 »'o”? 1 6
-0.4287
-0,3457
- Ls02?JL
-0.3457
: « *745
-O , R077
rO. 3457
1 , 0?on
-r, 4304
— C » 00 ao
-O,0Q4]
0 * n 3 c: n
0 • 1 0 7 7
0*0101
Qi.00.14. _
0 * .3 1 * 1
-0,077 s
CHI = 1 5 *00 G_AMMA=_ 1,5
( W * L 1
( U ♦ L I
rw.oi
fU.O )
-0.1204
0,8157
-0,2459'
1,3339
-0,1013
0.8703
-6 « ? 5 3 3 ' '
1,0160
-n. m 2 ?
0 , t? l p p
• 0,4 90 7
Z/M = .0
-0.1115
0.8700
-0*7539
1 • 1 063
ETA= UCLQ__
-C • 6 1 fl 3
-0.7839
0,3700
-0,49] 7
-0.C089
-0,00.43
0 , 0 3 p 0
0*7770
0,010?
. 0,0003
0,07 5 6
-0, 04
CHI *30, jCi
gamma = 1,5
2 FT A =
2,00 X/H=-
1.00 V /Hs 0 ,
Z/H = 0 ,
FT A = 1,00
f irf.LI
{ U » L 1
< * , 0 }
<U»D)
0,0157
0,6482
' -0*2376
1*1302
0,0361
0.6534
- 0 ,2444
0 , 7 7 6 1
-0.0559
-0.1809
0.6442
-0,515?
0.075?
0.6631
-0.2701
C. 8745
- 0.4774
-0.7701
0.6671
-0.5167
-0.0094
-0.0049
0.047?
0 . ? 6 67
OiOno
0,0003
0 • 0 ? 6 1
-0,0984
CHI =45.00
GAMMA = 1.5
ZFTA =
2, 00 X/H=-
l.on y/h= 0 ,
■?/H= 0,
FTA : 1,00
1 W.LJ
IU*L1
twior
(U »D >
0 ,0 881
0,517?
-0.741 6
0,9750
-
0,1118
0,5188
-0,25 38’"
0.5694
0,066 3
-0,1916
0.5074
-0,6128
0,0991
0 , 5 J R4
-0 , ? 7 « 3
0,6907
-0,701 p
-0 , 7 7R 3
0. R 1 84
-0. 0 ] 4?
-0.01 ] 0
-0,0061
0 • 0 -j 6 7
0.7797
0,01 ? 7
0*0004 ...
0,0746
-0 , 1 0 0 . 0
CH I =60.00
G A MM A = 1,5
2 FT A =
2.00 x/t-=-]
i • 00 Y/H = 0.
Z /H= 0.
FT A;: 1,0 0
1 WtL I
tU.L )
0,1114
0.4049
0,1416
0.4140
0, 153?
-0.2 ] 74
0 .’3 ofl O' -
—0,4837
0,1753
0.4137
-0.1977
-0.01 70
0,0166
rw.'oi
~-0,7(f0T“
0,857?
-?T*?T34
0.440?
— 0 , 7 9 70
-0.00PO
0,0003
(U.D1
-0. 7970
0,667?
0,4137
-0,4440
0.0360
0 , 7000
0,073a'
-0, 1 l ?0
CHI =75.00
GAMMAS 1,5
_Z_FT A =
2,00 x/H=-l
,00 Y/H= 0.
7/H= 0.
F T A= 1,00
( W«L )
<U,l)
< w.D) "
f U » 0 J
0,0892
0.3300
-0.2817
0*7528
0*1337
0.3*66
-0.7973
0.3177
0.7161
- 0,?^6 7
"""0.3181
— ^ » 4 ? 6 6
0.1 089
0.3469
-0,3190
0,4346
-0, 1 16?
- 0. 3 1 on _
0. 346 o' ”
-0, 4746
“0 • 0 1 98
01 69
0,0377
. 0,7107
0 , 0 ? 4 8
-0.0004
0,0? 1 6
-0, 1160
CHI =90,OI>
GAMMA= 1.5
ZFT A =
.2,00 X/m
,00 Y/H= 0,
7/H= 0.
FTA= l.oo
<W,L)
<U.L)
( * * 0 1
(U.OI
0.0333
0.2961
-01.2961
0.6694
0,1017
0,3226
-0,3276
0.2202
. 0.7637
-0.7585
0*2585
“ 0 , * 5 ? ?
0.0579
0.3376
-0.3376
0.3376
-0.067O
-0. 3376
0. 3376
-0. 33 76
-0#0?47
-.-0*0415
0.0415
0,3318
0,043?
.“0*0150
0,0150
“0,1174
- “
.
....
5 ^
TABLE 6,- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = l*. C ■ *#>, AND 1 - IM
(c) x/H = y/H = z/H = 0
Correction factors for correcting from a wind tunnel
which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
chi =-3.00
( W »L )
( U.L )
I W.D >
(U.D)
GA MM A = 1,5 ? E T A = 2.00 X/H* 0.
V /H = 0.
-6.6664
-0.4?30
-7 '.7441'
-0.1354
-6.6389 8.1136
-0.4232 -7,6858
--7. 754“8 ”-0.4235
0.1322 3*3276
Z/H*
0.
-6.6532
-A. 4232
-7.7822
0.0572
E TA= 1.00
7.5039
-7.7822
-0.4232
3.3221
-0.0132
0.0002
0.0381
-0.1925
0.0143
- 0.0001
‘ D.0‘274
0.0750
CHI= 3.00
f W . L }
( U.L)
(W.D)
(U.D)
GAMMA* 1.5 ZET A* 2.00 _ X/H* 0. _ Y .. .
Z/H=
0.
-6.6664
O , 4 ? 30
-7,3957
0.6809
-6.6389
0.427?
-7.4066
0,9223
6.5065
-7.3370
0.4230
3.32 i 6
-6.6532
0.4232
-7.4340
0.8546
ETA= 1.00
5.9069
-7.434H
0.423?
3.3221
-0.0132
- 0.0002
0.0383
-0.1737
0.0143
0*0001
0.0274'
0.0677
CH 1=15. 0C GAMMA* 1.5 7ETA= 2.00 X/H= 0.
Y/H* 0.
< W , L )
( U « L )
(W.D)
[ U i D )
-5.9563
1.9394
-6.1130
1 .8173
-5.9278
1.9397
-6.1241
2.0091
3.9308
-6.0539
1.9392
2.7415
Z/H* 0.
-5.9426
1.9396
-6.1516
1.9559
ETA* 1.00
3.3485
-6.1516
1.9396
2.7366
-0.0137
- 0.0002
0.0386
-0.1386
0.0148
0.0000
0 • 02 T9
0.053?
*30. no
r, iM«A= 1*5
Zf TA =
2.00 X/H*
0. Y/H*
(W.L)
(U.L >
(W.D)
(U.D)
-4.1930
2.9430
-4.1452
2.1298
-4.15T5”
2.9437
-WT566
2.2733
Z. 1157
-4,0858
2.94 2 5
1.3528
: *45 .03
GAMMA* 1*5
7 ET A*
2.00 X/H*
0. Y/H*
(W.L)
(U.L)
(W.D)
(U.D)
-2,4057
2.7817
-2.5799
1.5903
-2.3674
2.7830
-2.5917
1.6918
1.5171
-2*5204
2.7806
0.0884
Z/H= 0,
ETA* 1.00
-4.1778
2.9436
-4.1 841
2.2337
1.5518
-4,1841
2.9436
1.3473
-0.015?
-0. 00 C 6
0.0388
-0.1039
0.01S4
0.0001
OiT?7?
0.0396
Z/H* 0.
ETA* 1.00
-2.3873
2.7829
-2.6190
1 . 6641
0.9690
-2.6190
2.7829
0.0819
-0.0184
-0.0012
0.0391
-0.0738
0.0199
0.00C1
0.0274
0.0Z77
C H 1 = 60 .00 GAMMA = 1.5 ZET A* 2.00 X/H= 0.
Y /H- 0.
(W.L)
{ U.L >
I W.D)
(U.D)
-1.3362
1*9958
-1.6734
0.8515
-1.2856
1.9989
-1*6860
0.9145
1.4552
-1.6142
1*9933
-0.4291
Z/H* 0.
-1.3130
1.9986
-1.7130
0.8990
ETA= 1.00
0.9213
-1.7130
1.9906
-0.4377
-0.0252
-0.002B
0.0396
-0.0465
0.0274
0.0003
0.0270
0.0165
CHl = 75,0U GAMMA = 1.5
ZETA= 2.00 X/H- 0.
Y/h- 0.
I W.L)
C U * L )
(W.D)
(U.D)
-1.0226
1.2965
-1.2055
0.3121
-0.9342
1.3069
-1.2214
0.3381
1.4717
-1.1481
1.2831
-0.2864
Z/H*
0.
-0.9806
1.3062
-1.2467
0.3325
ETA* 1.00
0.9511
-1.2467
1.3062
-0.2986
-0.0420
-0*0097
0.0412
-0.0204
0.0465
0.0008
0.0253
0.0055
CH I = 9 0_. 0 C ' _ GAMMA = 1 .5
(W.L) -1.0255
(U.L) 0.9035
' "(WtD) -0.9035
| U • D ) -0,0000
ZETA* 2.00 X/H= 0. V/H=
-0.B610 1.4600
0*9418 -0 • B 5 8 4
-0*9418 0*8584
0*0000 0*0000
Z/H* 0.
-0*9549
0.9549
-O’. 9 549
- 0 .
ETA* 1.00
0.9549
-0,9549
0.9549
0.
-0.0706
-0.0514
0.0514
-o.nnoo
0.0940
-0.0131
” 0.75131
D. 00750
6 ^ 1-7
55
TABLE 6.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, ' = 2 00 ' A 1 ™ ” = 100
(d) x/H =1.00
8
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
— — i *
to ground effect
CHl- 0.
GAMMA* 1*5
Z FT A- 2.00 X/H-
1*00 Y/H= 0*
Z/H- 0*
FT A* 1,00
£
rH
1
(W,L)
(U#L)
(W»D>
(U.D)
-0*3546
-1*0249
-0*9947
-1.7720
-0*3355
-1*0293
-0.9967
-1.1524
16*2661
-0.9554
-1.0216
-0*4287
-0.3457
-1*0290
-1*0209
-1,3087
15,5013
-1,0209
-1*0290
-0*4304
-0,0089
0*0041
0.0262
-0*4633
0*0101
-0*0004
0*0242
0.1563
CHI-15.00
GAMMA- 1.5
7 FT A- 2*00
X/H-
1,00 Y/H* 0*
Z/H* 0*
FTA* 1,00
( W »L )
(U,L)
(W»D)
<U,D)
-0.7573
-1.2671
-1*332?
-1.7464
-0*7511
-1*3250
-1*3887
-1*3632
15.9691
-1*2908
-1.2637
-0*2044
-0.7548
-1*2979
-1*3868
-1.4118
15.2121
-1 , 3868
-1,2979
-0,3073
-0*0025
0*0308
0*0543
-0*3346
0,0037
-0,0271
-0,0019
O.OA85
CHI -30*00
gamma- 1.5
ZFTA- 2*00
X/H =
1*00 V/H« o,
Z/H- 0.
FT A- 1,00
(W»L )
(UtL )
(W,D)
(U»t>)
-1*5405
-1.6449
-1.8429
-1.8774
-1*5170
-1,6498
— 1 * 8462
-1,3216
15,3499
-1.7992
-1.6412
-0.0475
-1.5294
-1*6494
-1*8715
-1.4652
14.6141
-1.8715
-1 • 6494
-0.0500
-0*0110
0,0044
0*0286
-0*4123
0*0124
-0*0004
0*0253
0*1436 ..
CHI -45.00
GAMMA - 1.5
ZFTA- 2*00
X/H*
1.00 Y/H* 0.
Z/H- 0.
ETA = 1,00
( W »L !
(U,L)
(W»D1
(U«D)
-0*0141
0*0051
0*029?
-0*3915
0*0158
-0*0006
0*0250
0*1370
CHI -60.00
GAMMA- 1.5
Z.ETA- 2*00
X /H ■
1.00 Y/h= 0.
Z/H- 0.
ETA- 1,00
(W»L)
(UtL)
<W,D)
(UtOI
-7.0943
-0,8819
-3.3786
-0,9893
-7,0492
-0*8891
-3*3815
-0*4851
9,9899
-3.3310
—0 . 876 5
2.4029
-7*0729
-0*8883
-3*4083
-0.6173
9*2477
-3*4083
-0*8883
2*3970
-0*0214
0*0064
0*0297
-0*3720
0*0237
-0*0008
0*0268
0*1322
CHI -75.00
GAMMA- 1.5
ZETA- 2*00
X/H-
1*00 Y/H- o.
Z/H- 0.
ETA* 1,00
(W.L)
(UtL)
(WtO)
(UtO)
-3.7872
1.4781
-1.2889
-0.3656
-3.6930
1,4702
-1*2908
0*1113
4*2674
-1.2391
1.4836
0.2660
-3.7423
1 *4713
-1*3186
-0*0137
3*5559
-1*3186
1.4713
C , 2521
-0*0449
0*0069
0*0297
-0*3519
0*0493
-0*0011
0,0278
0,1250
CHI-90.00
GAMMA- 1.5
ZFTA- 2*00
X/H-
1.00 Y/H- 0.
Z/H- 0.
ETA- 1*00
(W.L)
(UtL)
(WtD)
(UtO)
-2.0843
0.2961
-0.2961
-0.6694
-1.8231
0*3226
-0*3226
-0,2202
2.6562
-0.2585
0.2585
0.3522
-1*9678
0.3376
-0,3376
-0*3376
1*9678
-0.3376
0,3376
0,3376
-0*1165
-0*0415
0.0415
-0*3318
0*1447
-0,0150
0,0150
0*1174
56
TABLE 6.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND tj = 1.00
(e) x/H =2.00
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
CHI* 0,
GAMMA* 1.5
ZET A*
o
o
X/H= 2,00 Y/H- 0.
Z/H* 0,
ETA- 1,00
(W»LJ
(U»L)
1 W *D J
IU»D )
-0.0265
-0*2600
-0*2675
-1*0666
-0*0194
-0*2647
-0,2618
-0,3333
16*2636
-0.2446
-0*2581
-0.2074
-0*0236
-0*2651
-0*2798
-0,4825
15,4013
-0.2798
-0.2651
-0.2061
-0*0029
0,0043
0,0123
-0,5841
0,0042
0,0005
0.0180
0.1493
CHI * 1 5.00
GAMMA* 1*5
ZET A =
2*00
X/H* 2*00 Y/H* 0,
Z/H* 0,
ETA- 1*00
IWt L }
tU*LI
IW.D)
t U *D )
-0*1127
-0*3323
-0*3456
-1.0738
-0,1050
-0,3363
-0,3406
-0,3496
16*1869
-0*3210
-0.3293
-0.1876
-0,1105
-0,3404
-0,3632
-0,5148
15. 3333
-0,3632
-0, 3404
-0,2011
-0.0022
0.0081
0,0176
-0,5591
0 , 00 56
0,0041
0,0225
0.1651
CHI-30.00
GAMMA* 1*5
ZETA*
2,00
X/H* 2.00 Y/H* 0.
Z/H= 0*
ETA* 1.00
(W*LI
1 U »L J
IW»D)
(U,0)
-0*2771
-0*4437
-0*4607
-1.1056
-0*2681
-0,4486
-0,4566
-0,3902
16.0358
-0*4348
-0.4403
-0.1917
-0.2734
-0.4489
-0.4758
-0, 5424
15.1912
-0,4758
-0*4489
-0.1907
-0,0037
0.0C52
0.0151
-0,5632
0.0053
0.0003
0,0192
0.1523
CHI *45*00
GAMMA = 1*5
ZETA*
2,00
X/H* 2.00 Y/H* 0,
Z/H* 0,
ETA* 1.00
• ( W ♦ L 1
(U.LJ
( W,D )
(U * D )
-0.6337
-0,6187
-0,6334
-1.1212
-0,6214
-0,6245
-0,6292
-0,4127
15.7030
-0,6061
-0*6144
-0.1675
-0.6285
-0.6250
-0.6493
-0.5664
14,8658
-0.6493
-0.6250
-0. 1661
-0*0052
0,0063
0.0158
-0.5549
0.0071
0.0005
0,0201
0. 1536
CHI *60*00
GAMMA* 1,5
ZETA =
2,00
X/H* 2.00 Y/H* 0*
Z/H* 0.
ETA* 1.00
1 W *L 1
CU *L >
(W.D)
CU.D)
-1.6669
-0,9642
-0,9621
-1.1301
-1 • 646b
-0,9727
-0,9573
-0,4285
14. 7412
-0.9331
-0.9579
-0.0794
"T . O J 04
-0.9732
-0.9784
-0.5831
-0.9784
-0.9732
-0,0780
-O.OObb
0,0090
0,0163
-0.5470
0.0114
0.0005
0.0211
0,1546
CHI *75*00
GAMMA* 1.5
ZETA*
2*00
X/H* 2.00 Y/H* 0.
Z/H* 0,
ETA* 1*00
4 W * L )
4U*L)
4 W #0 )
fU.D)
-7,4016
-0,6557
-1,8067
-0,8311
-7,3468
-0.6719
-1,7987
-0,1365
9.4478
-1.7746
-0.6436
1.5350
-7.3767
-0,6719
-1.8221
-0.2918
8,6241
-1,8221
-0,6719
1*5334
-0.0249
0,0161
0,0154
-0,5393
0,0298
-0,0000
0.0234
0.1553
CHI *90*00
GAMMA* 1,5
ZETA-
2,00 X/H* 2*00 Y/H* 0,
Z/H* 0.
ETA* 1*00
4W»L l
4 U » L )
(W,0)
(U.D)
-2.1182
0,0627
-0,0627
-0,6976
-1,8080
0,0696
-0.0696
-0,0202
2.7942
-0.0376
0.0376
0.1850
-1,9799
0.0854
-0.0854
-0.1708
1.9799
-0.0854
0,0854
0*1708
-0.1383
-0.0227
0.0227
-0.5268
0,1719
-0.0159
0,0159
0,1506
6 ^ 1-1
L-1549
57
TABLE 6.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR
1.5, C = 2.00, AND rj = 1.00
(f) x/H = 3.00
8
Correc
tion factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
■ —
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
CHIo J •
GAMMA* 1.5
2 tT A
= 2,00
x/h* s.oci yvh* o*
Z/H= 0,
ETA* 1.00
“ " iW*L >
IU«LI
{midi
(U»0)
-0,1103
-0,1222
-0,8546
-v ,uo23
-0,1121
-0,1125
-(»•, 1334
16.26o8
-0,1061
—0 • 1 090
•-0,1024
“0 • 0037
-0,1131
-0*1245
-0,2460
15.3484
-0.1245
-0.1131
-0.1010
-0,0003
0,0026
0,0023
“0, 6C68
C, 0014
0.0010
0,0U1
0*1126
_C H 1=15*00
GAMMA = 1,5
At. A ;
5 2 ,-C
A/H= 3.0J r/H* 0,
Z/H* 0,
ETA= 1.00
( W » L )
( U »L )
(W»0| ‘
(UtDI
— C » ^42 6
-o , i 46 7
-0,1597
-0 , 879 J
“0,0-387
- J • 1412
-0,1431
-0,1276
16,2234
-0.143C
-0.1453
-0.1 154
“0,0412
-0.1459
-0.1595
-0,2579
15.3172
-o. 1595
-0, 1459
-0. 1004
-0,0014
-0,-006
“O.0O02
-0.6211
0,0025
0,0047
0*01 04
0,1303
CHI =30.00
GAMMA = 1,5
aETA =
2,u0
x 7 H = 3*0 'j wh« u *
A/N= 0,
li T A = 1.00
(W*L)
I U » L }
"" (W.DJ
iU.D)
-0,1035
-0,2037
-0,1890
-0,8978
-0,1177
-0.1775
-0,2084
-0.1236
16.1476
-J.1717
-0.2-21
-0.C 764
-0.1112
-0.1926
—o ,2-74
--.2661
15.2531
-0.2074
-o. 1928
-0. 0992
0.0077
“0,0106
0,0164
-0.6297
-0,0063
0,0154
-0,0010
0,1444
CHI =45*CC
GAMMA = 1,5
ZET A =
i.vU
X/H= 3,00 Y/H= 0,
A /Ha 0,
I. TA= 1,00
IW,L)
iU,L>
■ fW.D)
(UiD)
-0,2641
-0,2641
-0 ,2772
-0,8809
-u,2ou9
-0.2670
—A ,2664
— 0 , 1543
16.0 06 5
-0.2593
— 0,262 u
, - 984
-0.2633
-0.2684
-0.2821
--.2772
15.1076
-0. 2621
“0.2664
-0.0964
-0.0006
0*0043
0- .0049
-u.6037
0,0024
0,00l4
0,0136
0*1229
CHI =60.00
GAMMA= 1,5
ZETA =
2,00
\/n- 3.CC Y/H = C*
4/H= -•
8 TA= 1.00
JW.L)
(U »L )
£W.D)
{ U *D )
-0,7008
-0,4103
-0,4190
-0.8876
-0,6951
-0,4149
-Cl ,41 Co
-0.1597
15.5776
-0.4005
-0 ,4069
-0.0910
-0.6991
-C *4168
-0,4245
-0.2854
14.6823
-0.4245
-0.4168
-0.0881
-0,0017
0.0065
G.0C54
-0,6022
0*0040
0,0016
0,0144
0,1256
CHI =75.00
GAMMA* 1.5
ZET As
2 , CO
- 7H= 3, CO r/H* 0,
Z/Hs 0.
E~A = 1,00
tW.L)
(U*l)
IW.D)
(U.0)
-3.0932
-0,8662
-0,8352
-0.8909
-3,0737
-0*8776
-0,8245
—0,1608
13.2566
-0.8151
-u ,8 578
-C ,OC2u
-3.-658
“0 , 88 04
“U ,8404
-0.2896
12.365-
-0. 8404
88o4
0.0030
“0.0074
0.0142
0.0052
“0.6013
0,0121
0,0026
0,0159
0,1286
CHI *90, OC
GAMMA= 1,5
ZETA=
2, -JO i
l -/H= 3,00 1 /H= 0.
Z/H = 0.
ETA = 1,00
(W#L)
(U.L)
(W»DJ "
(U,D)
“2,0947
0,0222
-0,0222
-0,6875
-1,7696
0,0171
-0,0171
0,0374
2,8334
-0*0046
0,0046
0,0989
-1.9514
u ,0302
-0*0302
-0,0906
1.9514
-0,0302
0,0302
0.0906
“0.1433
-C.OOaO
0.0060
-0,5969
0,1616
-0,0131
~ ' 0,(5131
0,1280
58
TABLE 6.- Continued
longitudinal distribution of interference factors for V = 1.5. t - 2 00 - AND 100
(g) x/H - 4.00
Correction factors for correcting from a wind tunnel
which is
s
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
*- —
to free air
to ground effect
'
(W.L )
IU.L )
IW.D)
IO.D )
GAMMA* 1*5 2ETA = 2.00
X / H = 4.00 Y/H* 0.
2/ H = 0.
-0*0008
-0*0606
-0*0724
-0*7401
-0*0004
-0*0612
-0*0613
-0*0662
16*2623
-0*0587
-0*0601
-0*0591
- 0*0010
-0*0621
-0*0691
-0*1482
ETA* 1*00
15*3230
-0.0691
-0*0621
-0*0584
0*0002
0*0015
-0.0033
-0.5919
0.0005
0.0009
0.0078
0.0000
CHI *15*00 GAMMA * 1.5 2ETA* 2.00
X/H- 4*00 Y/H* 0*
IW.L J
IU.L)
( W » D }
IU.D )
-0*0217
-0.0789
-0*0908
-0.7483
-0*0214
-0*0794
-0*0800
-0*0700
16.2413
-0.0769
-0*0783
-0*0588
Z/H* 0.
-0.0219
-0.0804
-0*0882
-0.1538
ETA* 1*00
15*3048
-0*0882
-0.0804
-0.0583
0.0002
0.0015
-0.0026
-0*5946
0*0005
0.0010
0.0081
0.0838
CHI-30.00
GAMMA * 1.5
iETA= 2.00 X/H* 4.00 Y/H* 0.
(W.L I
IU.L )
(W.D)
IU.D)
-0.0607
-0*1046
-0.1168
-0.7545
-0*0603
-0*1053
-0*1060
-0*0720
16*2024
-0.1027
-0.1039
-0.0589
Z/H =
0.
-0.0609
-0.1065
-0.1146
-0.1584
ETA* 1.00
15.2683
-0.1146
-0.1065
—0 » 0580
0.0002
0.0019
- 0.0022
-0.5961
0.0007
0.0011
0.0086
0.0864
CHI *45*00
GAMMA* 1.5 2ET A* 2*00 X/H * 4,00 Y/H “ °*
Z/H =
0.
(W.L)
(U.L)
(W.DI
IU»D 1
-0.1458
-0.1482
-0.1561
-U . 1626
ETA* 1.00
15.1859
-0.1561
-0. 1482
-U.0574
CHI *60*00
GAMMA* 1.5 ZETA* 2*00 X/H* 4.00 Y/H- 0
( W * L >
(U.L)
IW.D)
10.01
-0.3885
-0,2257
-0*2370
-0*7654
-0.3873
-0.2274
-0.2262
-0*0752
15.8762
-0*2224
-0*2244
-0.0576
Z/H =
0.
-0.3887
-0*2294
-0.2355
-0*1664
ETA* 1.00
14.9462
-0*2355
-0*2294
-0*0558
0*0002
0*0037
-0,0014
-0.5990
0*0014
0.0020
0.0093
0.0912
CHI *75.00 GAMMA* 1.5
ZETA* 2*00
X/H* 4*00 Y/H* 0*
IW.L)
(UtL)
(W.D)
IU.D)
-1*7597
-0.4504
-0.4636
—0.7663
-1.7548
-0.4554
-0.4722
-0*0720
14*6262
-0*4685
-0*4466
-0*0528
Z/H* 0.
-1.7590
-0.4592
-0.4622
-0.1658
ETA* 1.00
13.6982
-0.4822
-0.4592
-0.0485
-0.0006
0.0088
-0*0013
-0.6004
0.0042
0.0038
0.0100
0.0938
CHl*90.00 GAMMA* 1*5
ZETA* 2*00 X/H* 4*00 Y/H* 0*
(W.L >
IU.L)
(W.D)
<U.D)
-2*0790
0*0141
-0*0141
-0.6551
-1.7506
0*0044
-0*0044
0.0402
2.8569
0.0003
-0*0003
0*0586
Z/H= 0*
-1*9358
0.0136
-0*0136
-0*0545
ETA* 1.00
1*9358
-0*0136
0*0136
0.0545
-0.1431
0.0005
-0.0005
-0.6006
0*1852
-0.0092
0.0092
0.0947
6 ^ 1-1
L-15^9
59
TABLE 6.- Continued
LONGITUDINAL. DISTRIBUTION OF INTERFERENCE FACTORS FOR » - !•*, C " 2.00, AND q • 1.00
(h) x/H = 5.00
Correction factors for correcting from a wind tunnel
which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 '
to ground effect
CHI = ^*.
(jAMM A = 1*5
i-ETA= 1*00 a/m= 5*00 .Y/H.® 0*~-
. ..Z/Jt= 0*
ETA- 1*00....
-- "
( W#L )
( U * L )
< W #L> 1
(UiD)
— 0# J0v 1
“0*0385
-u * 0496
“L *6569
-u.uLu.
— 0 *038b
-U*G365
1 o • 643
-0*0371
— 0 *0003
-0*0352 .. .
15* 3090
. -0#043i. . — •
0*0002
Q.Q007
0* 0002
. . U-..U UU6 .
O.0050
0*0370
-0.0383
-0*0381
-0.0435
-0.098b
-0.0392
-0. 0378
-0*0060
-0*5561
CHI =15* GO __
GAMMA= 1*5
ZET A= 2*00
X/H = . 5*00 Y /H* Ot.
2/H- 0# ...
.... ETA- 1*00
—
1 W *L )
(U*L)
( wl f D )
(U»D)
—0 * 1 3 5
-0*0501
-J *0613
-0 • b64u
-0*0135
-0*0502 .
-0*0503
-0*0423
16*4 508
— 0 * ^ 4 8 7
-0*0490
-0*03o 1
-0*0137
. _-0i0509
-0*0556
—0 • 1 U 1 8
13*2972
-0*0536
-0*0509
— u* 03 77
0*000*.
. o*.oau6 . .
-0*00 jo
-0*36*:*;
U.UUUZ
. ...0*19110.1
0*0039
0*0395
CKl = 30# 00 _
GAMMA* i*5
ZcJA= 2*00
A/h = 5*00 1 / h= 0*
£/H= 0*
£TA= 1*00
—
i w»u
1U iL 1
(M»D)
(U.D)
-„*0377
. _ .. — L * u6B J
—0 # j 766
-0.6721
-w *037t
-0*0681
-0*0655
—0 *04 3 a
16.2249
-0*0639
-0*0677
-0*0361
—0 *0386
-0*0675 — -
-0*0723
-J* 1 043
15*2736
-0.0723
— 0 « 06 7 3
-0*0376
0*0010
■■■-0*0009 -
“0 *00h5
-0*56/*
0*0010
. -0*0007
j.OUOb
0*0391
CHJ *45 #00
GAMMA* 1*5
ZETA = 2*00
X/H= 5*00 Y/h* 0*
Z/H = 0*
ETA= 1*00
.... .
(WtL )
I U *L )
(WtDI
(U*D 1
—0 * 09^ 6
—0 * 0939
— C * 0987
-0*1065
i 5 • c a 0 7
-0 • 0987
-0.0939
-0« 0375
CH 1*60# 00
GAMMA* 1*5
ZtTA* 2*00
X/H* 5.00 Y/H* 0.
2/H = 0*
ETA= 1*00
_ _. ... -
(WtL)
(U»L)
( w #0 )
< l)*D 1
-0*2474
-0*1434
-0.1545
-0*6793
-0*2472
— 0 • 1 4 3 6
-0*1434
—0*04 3o
16*0166
-0*1416
-0*1428
-0.0379
-0.2476
-0*1 **32
-0*1493
-0*1085
15*0671
-0* 1493
-0*1432
-0*0370
0*0004
0*0C1q
-0*0u51
—0 • 3 706
0* 0006
0»0lil3
0*0060
0*0650
CHI =75*00
GAMMA* 1*5
ZETA* t»j0
X/H= j*00 y/h= 0*
Z/H - 0.
ETA= 1*00
(WtL )
(U»L )
|W*D]
IU»0)
-1*0649
-0*2930
-0.3023
-0 *6636
—1*0839
—0 *2943
-0*2910
-0*0433
15*1806
-0*2892
— u • 2 y 1 4
-U*w367
-i *0o55
. — 0 # 2 9 1 6
-0.297A
-0*1104
14.2321
-0*2973
— U* 29 76
“0 • v 344
0*0007
. JO* 0 046. . .
-0*0050
-0*3731
0*0016
_Q*.£l05*
0* Owo J
0* Uu66
CHI =9 0# 00
GAMMA* 1*5
ZtTA= 2*00
X/H= 5.00 Y/H* 0.
Z/H = 0*
tTA= 1*00
.. . _
(WtL)
( U »L )
(W.D)
<UiD)
-2*u697
0*0120
-0.012 w
-0.6112
—1*7406
0*0011
-0*0011
0*0318
2.6693
0*0010
-0 * 001 0
0.0381
-1*9273
0*0072
-0*0072
-0.0360
1.9273
-0*0072
0.0072
0.0360
-0.1423
. 0*0046
-0*0048
-0*3752
0*1866
^0*0061
0*0061
0*0678
6o
TABLE 6, - Concluded
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 2.00, AND 77 = 1-00
(i) Miscellaneous additional values of x/H
s
Correc
tion factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
-1 1
1
CHI “15*00
GAWMA= 1.5
ZETA = 2.00
X/H= 0,13 Y/H= 0*
Z/H* 0*
eta- 1.00
<W»L)
<U»L)
(W*D)
IU»0)
-6*7526
0*3003
-6*8356
0*2919
-6*7242
0*2997
-6*8458
0,5484
7*2413
-6*7778
0.3007
3*3295
-6*7390
0*2998
-6*8732
0*4771
6*6342
-6.8732
0.2998
3*3246
-0.0136
0.0005
0*0376
-0*1852
0*0147
-0*0001
0*0274
0*071?
CHI-30,00
C A MM A = 1,5
ZETA* 2.00
X/H= 0,29 Y/H» 0,
Z/H= 0*
ETA- 1.00
fV/*LI
<U»LI
fW,0|
(U«D)
“6,9327
0*4243
-5*9976
0.0552
-6.9014
0*4230
-6*0070
0,3418
7*5665
-5,9409
0.4254
3*2759
-6,9177
0.4232
-6*0344
0*2625
6*9474
-6*0344
0.423?
3.2706
-0*0150
0*0012
0*0368
-0*2073
0.0163
-0*0002
0*0274
0*0793
CHI -45,00
G A MM A = 1,5
ZETA = 2*00
X/H* 0,50 Y/H* 0.
Z/H* 0*
eta- 1*00
tw»u
<U*U
I W #D )
fU*D)
-7,2196
0*5311
-4,9686
-0.2036
-7,1025
0*5283
-4,9764
0.1396
7,8440
-4.9138
0.5332
3*1248
-7.2018
0,5287
-5,0038
0,0456
7.2010
-5*0038
0*5287
3*1188
-0*0178
0*0024
0*0352
-0*2492
0.0193
-0*0004
0*0274
0*0941
CHI *45,00
GAMMA= 1.5
ZETAs 2*00
X/H= 0.75 Y/H= 0*
Z/H = 0.
ETA= 1*00
IW*L)
ru -l >
(WfOI
(U*D1
-5.5863
-1*8541
-3.9649
-1.5698
-5.5523
-1*8585
-3.9705
-1*1251
11.9244
-3*9143
-1*8507
1.9925
-5*5701
-1*8580
-3*9973
-1*2445
11*2396
-3*9973
-1.8580
1 * 9876
-0.0162
0*0039
0*0324
-0*3254
0*0176
-0*0005
0*0268
0*1193
CHI -45,00
GAMMA 1 * 1,5
ZETA* 2*00
X/H= 1,?5 Y/H- 0*
Z/H* 0*
ETA= 1.00
IW*L I
<U*L>
(W«D)
(U,D)
-1*9092
—1*5344
-1 ,6606
-1.5886
-l*8e39
-1*5408
-1*6618
-0*9919
14,8401
-1*6201
-1*5296
0*0308
-1*8974
-1.5403
-1*6865
“1*1417
14*0821
-1,6865
-1*5403
0.0289
— 0.011B
0*0059
0*0260
-0*4469
0*0135
-0*0004
0*0247
0* 1498
CHI-60,00
GAMMA= 1.5
ZET A= 2*00
X/H= 0.87 Y/H* 0*
Z/H* 0*
ETA= 1*00
IW.LI
f U »L I
(WtOI
(U*D)
-7*5562
0*3775
-3*6098
-0,5251
-7.5083
0,3713
-3.6140
-0,0654
8.2772
-3.5598
0*3821
2.7268
-7* 5334
0*3721
-3*6412
-0.1877
7*5852
“3*641?
0*3721
? • 71 99
“0.0228
0*0055
0*0313
-0*3374
0*0251
-0*0000
0*0277
0*12?3
CHI-75,00
GAMMA = 1,5
ZETA= 2,00 X /H= 1,37 Y/H« 0*
Z/H* 0*
ETA= 1.00
tW.LI
(UtL )
( W • D 1
(U*D)
-5.3256
1 *6269
-1.4986
-0.3802
-5.2433
1*6139
-1*4957
0*2062
5.573?
-1.4554
1.6363
0.6118
-5*2867
1*6150
-1*5227
0*0595
4*8188
-1*5227
1*6150
0*6019
-0.0389
0*0118
0*0241
-0*4397
0*0434
-0*0012
0*0270
0* 1467
L-1549
L-1549
6 1
TABLE 7
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND ij = 1.00
(a) x/H = -2.00
CH! ■ 0.
GAMMA- 1.5
ZETA* 4,00
X /H*“2, 00
Y/H*
0,
Z/H- 0.
ETA- 1,00
tw*u
IU.L1
(W.0)
(U.D)
-0.0042
0,2477
0,1708
0,8293
-0.0033
0.2481
0.1711
0.1870
-0.0541
0,1882
0.2467
-0,2337
-0,0038
0.2485
0,1597
0.3402
-0.2050
0.1597
0,2405
“0.2336
-0.0004
“0,0000
0.0111
0,4891
0,0006
-0,0004
0.0114
“0.1531
CHI-15,00
GAMMA* 1,5
ZETA* 4,00
X/H--2.00
Y/H*
0.
Z/H* 0.
ETA- 1,00
(K.L)
ru.u
f W*D )
ru.oj
0.0449
0.1920
0,1209
0,8067
0,0459
0.1925
0.1213
0,1563
0.0038
0.1378
0.1911
“0.2339
0,0453
0,1929
0,1102
0,3096
“0.2210
0.1102
0.1929
-0,2337
“0.0004
-0,0009
0.0107
0.4971
0.0006
-0.0004
0.0112
-0*1533
CHI-30,00
GAMMA- 1.5
ZETA- 4.00
X/Hs-2.00
y/h=
0.
Z/H- 0,
ETA- 1.00
(W.L)
tu.u
(W» D )
tU.Dl
0,0752
0,1472
0*0799
0.7091
0*0763
0.1470
0.0805
0.1323
0.0410
0.0965
0.146 2
“0.2336
0,0756
0,1482
0.0695
0,2856
-0.1788
0.0695
0. 1482
“0,2334
“0,0004
“0,0010
0.0104
0.5035
0,0006
-0.0004
0,0110
“0*1533
CHI-45, 00
GAMMA- 1.3
ZETA* 4,00
X/H--?, 00
Y/H-
0,
Z/H* 0.
ETA- 1,00
1W.L)
(UtL)
(W.0)
(U.D)
0,0939
0.1096
0,0446
0,7745
0,0952
0.1103
0.0453
0,1124
0.0659
0,0608
0.1084
-0,2330
0.0944
0.1108
0.0344
0.2657
-0.1497
0.0344
0.1108
“0,2327
“0.0005
“0.0012
0.0102
0,5088
0*0007
-0*0005
0*0109
“0.1533
CHI-40,00
GAMMA- 1.5
ZETA- 4.00
X/H--2.00
Y/H-
0,
Z/H* 0.
ETA* 1,00
( W*L >
(U.L)
fW.D)
(U.D)
0.1045
0*0776
0.0128
0.7618
0.1062
0.0786
0.0136
0.0952
0*0827
0*0287
0.0759
•0,2316
0.1052
0.0793
0*0029
0,2483
-0.1292
0. 0029
0.0793
-0.2312
-0*0007
-0.0016
0.0100
0,5134
0.0010
-0.0007
0.0107
“0*1532
CHI-75,00
GAMMA* 1,5
ZETA- 4,00
X/H— 2,00
y/h»
0.
Z/H- 0.
ETA* 1.00
(WtL)
(UtL)
(WtD)
ru.Di
0.1081
0.0519
-0,0167
0,7503
0,1100
0,0536
-0.0160
0.0797
0.0937
-0.0012
0.0409
-0,2204
0,1091
0.0549
-0.0265
0.2326
-0.1147
-0.0265
0.0549
“0.2278
-0*0010
“0.0031
0,0098
0.5176
0*0016
-0*0014
0*0106
“0*1530
CHI-90.00
GAMMA* 1,5
ZETA- 4,00
X/H— 2*00
Y/H-
0,
Z/H- 0.
ETA- 1.00
(W.L )
(UtL)
(WtD)
(U.D)
0.1028
0.0446
“0,0446
0,7389
0*1084
0*0445
-0.0445
0.0661
0,1007
-0,0298
0.0298
-0,2216
0.1039
0.0545
-0.0545
0.2180
“0. 1039
“0.0545
0.0545
“0.2180
-0.0012
-0,0099
0,0099
0,5209
0*0044
-0*0100
0*0100
“0*1519
62
TABLE 7.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, < = *°<>- AND >, = 1.00
(b) x/H = -1.00
Correction foctors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free atr
r 1
to ground effect
2E1 A= 4*00 X/n--l» 00 Y /Vi- Q.
{ W • L ) -0.0y5&__
{u;n ' 1.-599
( w « D ) 0*7636
( <J * D ) 1*8162
-0*0930 -0.7 971
“T70603 0.2913
0*2619 l_^0b_88.
],4595 -0*ft?4?
1/ H = 0. FTA= 1*00
1.0606 0*2973
0.2973 1.0606
’ 1,6676 -0*8295
-0.0012
-0*0006
0*0168
0.?6fl6
-0.0003
0.019 6 ' .
-0.09B?
(W»l)
iU »L)
' (W*D1 ’
< U » D )
GAMMA 3 1.5
0*1067
0*6395
0.1375
1*5962
X/H=-l ,00
0.1092
0 399
"0*1359
1.21 <6
-0.5062
0*16 96 _
0*6 33 3
-0*« 32 5
Z/H» 0
0.1079
0._i->352 _
6.1215
1 *3?^0
FT A= 1*00
-0.8725
- 0.0012
-0.0007
. R35?
• 332 7
0.0160
0.2752
0*0199
-0*1039
C H l * 3 u • 0 u
( W »L >
1.3
9*2262
0.2310
-0*317?
0*2296
.0*6376
-0. 6706
. -0*0013
0*0015
(U.L )
0*6569
0*6573
0*0 5 3 3. -
0*6555
— 0 . o 3 1 1
Q.Q159
0*014?^
( vJ * D )
< U. D )
*i.'27 2
1 . 4 ? 4 r
• '256
i *03 c 1
1*1457
-0.8323
0*2886
-0.1Q.X6.
1.00 Y/H = 0*
0*_
GAK'^A 3 1*5
7 r - A =
4*30
x /(+=-;
'
U.L)
0.2936
0,3019
-0.1763
—0 . 0456
0*300?
-n# ^7 81
-0*0016
-0*0010
0.0018
-0.0009
(U.L)
0*5132
0 . 5 1 3 F
—
0.514?
-0. R2 33
0*0157
0*0141
( w * b y
(U*0)
-0.-J71&
"1*3031
— U *u7 34~
0.6115
-0,823]
1.0031
0*3000
“0*1110
_ ...
4*00
X/H = -
1*00 _0 •
Z/H = 0.
FTA= _1.00
CHI=6G*uC
GAMMA® 1*5
ZET A =
( W »L 1
(U.L)
0.3305
0*3993
0.3350
0*4001
-0.0780
—0,1371
0*3326
_0*4O07
-0.4237
-0* 1.78 5. _
0.4007
-0.8075
-0*0071
=G*0.QI4
0*0024
-o.nnoA
0*0140
(W.DI
" < U *0 >
-0.1629
1.1929
-0 • 1 645’
0,7687
0,3969
-0*6 02 7
-6*1785
0,8828
0 • 3 1 01
-0*1 141
CHI =75.00 GAMMA 3 1.5 ZFTA = 9.00 X/H = -1 .00 Y_/H=_ 0. l /H l-°* f TA S — .L* 00.
{ Vi »L 1
(U*0 — '
0*3246
0.3244
0*3322
0*3260
-0*0049
-0.2277
0.3281
0.3272
—0 .3449
-0.2635
-0.0035
-0.0079
1 U * D ) ”
{ U.D )
-0*2479
r.C96_fl_~
-0 • 2 4 9 B
0*6607
0.31VH
—0.7605
-0.7635
0.7775
-0. 7507
0._3J_93_,
.
—
— ■
—
0.0091
0.0JJL7 .
-0* 116»_
"CHI = 90.00
CAMSlA^TT? ZEYA*" 9.00 X/Hs-l^OO Y/H= 6.
Z /H =
0.
fW.CT
(U.L)
— r¥7cn
auDi
C.2T2F "(J7.Z918 01H7ROO
0.3259 0.3251 - 0*31516 0*^ 6
-0*3259 -0.3291 0.3016 _._-0* 3416
1,0099 0.5656 _ *0 . 6865 6.6033
F T A 3 1.00
—0 * 2 800 -0.007 3 ~~ 0.01 1 7
-0*3416 " -6. 0163 -0*0126 —
0.3416 0.0163 0*0126
-0.6833’ 0*3266 _ -0*1177 —
6+^1" T
L-15^9
63
TABLE 7. - Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C - 4.00, AND V 100
(c) x/H = y/H = z/H = 0
8
Correction factors for correcting from 0 wind tunnel
which is
— 1
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
on bottom
only
to free air
1 1
j to ground effect
-3.00 6avma= r.s z£TA= 4. 00 X /-= o._
Y/h= 0, '
< id , l j
1 l)*L)
‘ -26.6144
' - 1 *6925
-26.6108
-1.6921
(W.D)
(U « D )
— -3\.im ■
0.T326
—31*1132
0.2663
CH 1 =' 3.00
6 AMma= 1.5
Z£TA = 4.00 X/H=
( W »L )
( U * L )
' -26.6144
1 .6925
-26. bl06
1.6927"
< W.D)
tu.o}" '
759,7185
3.1517
779 ,T2 {13"
3.4525
cHi-israo •“
GAMMA = 1.5
ZETA= 4.00 X/'^
(W»L)
f U ♦ L 1
-23.77 22
7.7685
-23.7665
7.7588
( WiD )
(U.Dl
-24.5W8
7,7548
7.8503
ch i =30 *00“
GAMMA = 1.5
2 ETA= 4.00 X/hi =
< W , L )
{ U * L >
fw'.Ui
1 u # D )
-16.7132
11.7744
-T5 * 7 TB 1 ?
8.8831
-16.7092
11,7744
-16.7208'*
8.9546
CHi=45.C0
GAMM A = 1.5
ZETA= 4.00 X/H=
( W . L )
f U 1 L 1
-9.5517
11.1114
-9 • 5467
11.1314
< w*bi
<U.D»
— 8 7
6.6195
-10.46135*
6.6707
CH 1=60.00
GAMMA=' 1.5
Z E T A = 4, 00 ' X/*
-5'.'24H5“"“
7 . 9v42
' -6 . 6'TF5 '
3.6010
rw .'H
(U.L )
-7.255 5
7.9941
( W * D 1
( U . D 1
-6*8 346
3.5684
CH1=75.0^
GaMma= 1.5
ZETA= 4_.0 £ X/h
( W.L)
(U.L)
-3.9269
5.2238
-3.9159
5.2242
{ w*b’f
t u * 0 »
-4 ,9693
1.3191
-5*. 971 T
1,3340
CHI = 90.0C
GAMMA= 1.5
ZETA= 4.0C X/ ■
— ( W » L 1
{ U » L 1
-3.8391
3.B006
-3 , 7949
3.806C
— — — tj - ■R*'z;*i»r — '
1 W*D1
( U» D )
-3.8606
-0.0000
- 3 • 8 U 0 U
0. '"000
30. 5846
-31.D8CZ
-=T.6TZ5 _
13.2893
7/H = 0
-26.6127
-1.6926
“-irnTST''
0.2286
ffA= 1.00 _
30.0157
-31.1 287
— -in. TTE ~
13.2883
-0. 0017
0.0001
‘TT.TTT7Zjr“
V /H = 0.
Z/H= 0.
24.1912
-29. 68^2
r;69?5
13.2893
Y/H = 0,
13.9491
-24.5576
7, 7554
10.9469
-16.6876
“ -11.7743''
5.3899
-26.6127
1.6926
" -29.7359
3.4184
Z/H = 71.
-23.7704
7.7585
— 2 4 ."6 06 2
7.8234
Z/H- O'.
-16.7113
11.7744
-I6^“TJ64
8.9347
ETA* 1.00_
23.6274
-29.7359
"T76?76 —
13. ' 8 P. 7
.00
4.4138
-10.4773
11.1712
0.3285
4.2T5T '
-6.80 37
* 7.9T36"'
-1,749 6
, Y/H =
4.328?
-4 .9380
- 5. 2227T"
-1.1922
4. 3346
-3.7714
-'*7.7714'“
-0. "OO 0
Z/H = 0
-9. 5493
11.1315
-10.4761
6.6564
- 5. 21
7.9943
13.3941
-24.606?
- 7.758 5
10,9463
FTA = 1.00
6.2070
-16.7364
n .7744
5.3892
ETA* 1.00
3 . 8759
-10.4761
' ' 1 1 . I 3 1 5
0.3277
7 « sim -
-6.8520
7. '974 7“
-1 . 7507
Z/H = 0
-3.9226
5.2246
■ ■=Tr.-9'B _ EB'
1.3302
-3.8197
3.6197
-7. 8T77
ETf.= 1.00
3.5044
-4. 9868
“5.7746
-1.1943
-0. 0017
-0.0001
'7171175 '
-0. OR 67
-0. 0018
-o. nooo
0 • C 174
-C .0686
- 0.00 2 0
-0.0000
0. 0174
-0.0516
0.TT175
-0.C769
•' *0977074-
-0. on 02
— error 75 “
-0.0236
-0. 0063
-0.0008
- OiiriTT "
-0.C1 11
3.3197
-3.3197
“9 i'8197 "
r .
0.0018
-0.0001
■ 'O'.' 01-55“ -
0.0377
0.0018
0.0001
070175“
- 0.0194
- 0.0191
0.0019
-C. onoo
•-070156 '
0.0268
0 . 0 C 2 1
-C.0CO0
0*0156 '
0.0201
0.0026
- 0 . onno
' “ 070156 “
0.0143
-090056“
-0.0001
“ O.UT56
0.0090
0.0067
- 0.0004
“ U.Ulbb
0 • 00 39
0.0748
-0.0137
■ U.U1 37 •
6k
TABLE 7.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 4.00, AND n = 1.00
(d) x/H = 1 .00
Correction factors for correcting from a wind tunnel which Is
to free air to ground effect
CHI ■ 0.
“1
GAMMA* 1.5
(
ZET A= 4.00
1 —
X/H*
1.00
Y/H* 0.
Z/H- 0.
1_
ETA= 1.00
(W*L)
(U.L)
(W.D)
(U.D)
-0.0955
-1 .0599
-1.1053
-2 i 3233
-0.0930
-1.0603
-1.1060
-1*7923
62*3453
-1*0825
-1.0588
-C.8242
-0.0943
-1.0606
-1.1193
-1.9301
61.6054
-1.1193
-1.0606
-0.0245
-0.0012
0.0006
0.0139
-0.3933
0.0013
0.0003
0.0132
0.1378
CHI-15.00
GAMMA* 1.5
ZET A* 4.00
X/H*
1.00
Y/H* 0.
Z/H = 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-0*4393
-1*3464
-1 .4232
-2.3818
-0.4447
-1.3758
-1.4547
-1.9812
62.0678
-1.3998
-1.3452
-0.7453
-0.4421
-1.3615
-1.4528
-2.0591
61.3330
-1.4528
-1.3615
-0.8045
0.0028
0.0152
0.0296
-0.3227
-0.0026
-0.0142
-0.0019
0.0780
CHI *30*00
GAMMA* 1,5
ZETA* 4*00
X/H =
1.00
Y/H* 0.
Z/H* 0.
ETA* 1.00
(W»L)
(U,L)
IW.D)
(U.D)
-1.0949
-1.7949
-1 .8889
-2.5361
-1.0920
-1.7953
-1.8898
-2.0393
61.4866
-1*8650
-1 .7936
-0.7624
-1.0935
-1.7956
-1.9033
-2.1697
60.7650
-1.9033
-1 . 7956
-0. 7626
-0.0014
0.0007
0.0144
-0.3663
0.0016
0.0003
0.0136
0.1304
CHI -45.00
GAMMA * 1,5
ZET A* 4.00
X/H*
1.00
y/h= 0.
Z/H= 0.
ETA* 1.00
(W.L)
iu*u
(WfO)
(U.D)
-2*5159
-2.4990
-2*5824
-2.6211
-2.5121
-2.4995
-2.5833
-2.1380
60.1805
-2.5581
-2.4974
-0.6640
-2.5141
-2.4999
-2.5970
-2.2654
59.4633
-2.5970
-2.4999
-0.6644
-0.0018
0.0008
0.0]46
-0.3557
0.0020
0.0004
0*0137
0.1274
CH 1*60*00
GAMMA= 1,3
ZETA* 4.00
X/H*
1.00
Y/H= 0.
Z/H- 0.
ETA* 1.00
( W.L)
( U»L )
IW.D)
(U.D )
-6.6354
-3.8917
-3.8989
-2*6784
-6,6299
-3.8923
-3.8997
-2.2078
56.3547
-3.8741
-3.8895
-0*3114
-6.6328
-3.8928
-3.9136
-2.3324
55.6434
-3.9136
-3.8920
-0.3120
-0.0026
0.0011
0.0147
-0.3461
0.0029
0.0005
0.0138
0.1246
CH I -75*00
GAMMA 3 1.5
ZETA* 4,00
X/H*
1.00
Y/H* 0.
Z/H- 0.
ETA* 1.00
(W.L)
(U.L)
{ W *0 )
(U.D)
-29*5122
-2*6056
-7.2737
-1*5040
-29*5007
-2*6866
-7*2744
-1,0455
35.2018
-7.2485
-2.6821
6.1350
-29.5067
-2.6874
-7.2885
-1.1672
34.4962
-7.2885
-2.6874
6.1336
-0.0055
0.0016
0.0148
-0.3368
0.0060
0.0008
0.0141
0.1217
CHI *90*00
GAMMA* 1.5
ZET A* 4.00
X/H*
1.00
Y/H= 0.
Z/H* 0.
eta* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-7,9510
0.3254
-0.3254
-1.0099
-7.8815
0*3291
-0.3291
-0.5656
8.6157
-0.3016
0.3016
0*6869
-7.9195
0.3416
-0.3416
-0.6833
7.9195
-0.3416
0.3416
0.6833
-0.0315
-0.0163
0.0163
-0.3266
0.0379
-0.0126
0.0126
0*1177
6 ^ 1-1
L-15^9
iS
6 5
TABLE 7.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 7 = 1.5, C = 4.00, AND tj = 1.00
(e) x/H =2.00
Correction factors for correcting from a wind tunnel which is
closed
close d
on bottom
only
open
closed floor
only
{ground effect)
open
floor
only
closed
closed
on bottom
only
'
to ground effect
CHI- 0.
GAMMA * 1.5
ZETA*
4.00
X/H* 2.00
y/h* o.
Z/H* 0.
ETA* 1.00
(W.L)
(U*L )
(W.D)
(U.D)
-0.0042
-0.2477
-0.2684
-1.1438
-0.0033
-0.2461
-0.2665
-0.4414
62.1462
-0.2549
-0.2467
-0.2337
-0.0038
-0.2485
-0.2763
-0.5928
61.2918
-0.2763
-0.2485
-0,2336
-0.0004
0.0008
0.0079
-0.5509
0.0006
0.0004
0.0098
0.1514
CHI - 15*00
GAMMA* 1,5
ZETA*
4.00
X/H= 2.00
Y/H* 0.
Z/H* 0.
ETA* 1.00
IW.L )
lUtL)
I W*0 1
(U.D )
-0.0867
-0.3161
-0.3394
-1.1415
-0*0856
-0.3165
-0.3377
-0.4450
62.0694
-0.3255
-0.3151
-0.2146
-0.0875
-0.3217
-0 . 3526
-0.6150
63.2191
-C * 3526
-0. 3217
-C.2331
0.0009
0.0056
0.0132
-0.5265
0.0019
0.0051
0.0149
0.1700
CHI-30.00
GAMMA * 1.5
ZETA-
4.00
X/H* 2.00
Y/H* 0*
Z/H* 0.
ETA* 1.00
(W.L )
(UtU
(W.D)
(U.D)
-0,2441
-0.4248
-0.4497
-1.1727
-0.2431
-0.4256
-0.4484
-0.4816
61.9176
-0.4354
-0.4237
-0.2319
-0.2437
-0.4259
-0.4584
-0.6338
61.0730
-0.4584
-0.4259
-0.2320
-0.0004
0.0011
0.0087
-0.5390
0.0006
0.0003
0.0100
0.1521
CHI-45.00
GAMMA= 1.5
ZETA*
4,00
X/H* 2.00
Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.DI
(U.DI
-0.5837
-0.5915
-0.6156
-1.1849
-0. 5822
-0.5922
-0*6140
-0.4977
61,5844
-0*6009
-0.5901
-0.2299
-0.5831
-0,5927
-0.6244
-0.6504
60. 7438
-0.6244
-0.5927
-0.2297
-0.0006
0.0012
0.0088
-0.5345
0.0009
0.0005
0.0103
0.1527
CHI -60.00
GAMMA- 1.5
ZETA*
4.00
X/H* 2,00
y/h* o.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-1.5557
-0.9159
-0.9331
-1.1958
-1.5534
-0.9169
-0.9316
-0.5126
60.6218
-0.9181
-0.9138
-0.2234
-1.5547
-0.9176
-0.9421
-0.6656
59.7848
-0.9421
-0.9176
-0.2232
-0.0010
0.0017
0.0090
-0*5302
0.0013
0.0007
0.0105
0.1530
CHI-75.00
GAMMA- 1.5
ZETA*
4.00
X/H* 2.00
Y/h- 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L )
(W.D)
(U.D)
-7,0385
-1.8336
-1.9198
-1.1895
-7,0331
-1.8354
-1.9181
-0.5100
55.6265
-1.9044
-1.8294
-0*1942
-7.0361
-1.8368
-1.9289
-0.6632
54.7929
-1.9289
-1.8368
-0.1939
-0.0024
0.0032
0.0091
-0.5263
0.0030
0.0013
0.0107
0.1533
CHI-90.00
GAMMA- 1.5
ZETA-
4.00
X/H* 2,00
Y/H- 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-7.7810
0.0446
-0,0446
-0.7389
-7.6981
0.0445
-0.0445
-0.0661
8.5685
-0.0298
0.0298
0.2216
-7.7434
0.0545
-0 *0545
-0.2180
7.7434
-0.0545
0.0545
0.2180
-0,0376
-0.0099
0.0099
-0.5209
0.0452
-0.0100
0.0100
0.1519
66
TABLE 7.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 4.00, AND l\ - 1.00
(f) x/H = 3.00
8
Correction factors for correcting from o wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
r— t ~
to ground effect
1
CHI = 0.
GAHMA= 1.5
ZET A=
4*00 X/H =
3*00 Y/H*
0.
Z/H = 0.
ETA= 1*00
( W iL }
< U«L )
(W.D)
(U*D)
-0.0006
-0.1076
-0.116<j
-0.8816
-0.0003
-0.1078
-0.1126
-0*1599
62.1206
-0.1079
-0.1071
-0.1056
-0.0005
-0*1082
-0.1193
-0.2817
61.2033
-0.1193
-0. 1082
-0.1054
-0.0001
0.0006
0.0025
-0*5999
0.0002
0.0003
0.0067
0*1216
CHI *15.00
GAMMA- 1.5
ZET A =
4.00 X/H*
3.00 Y/H*
0.
Z/H = 0.
ET A= 1.00
(W«L)
<U*L)
{W»0l
IU*D 1
-0.0379
-0.1415
-0.1503
-0*8936
-0*0372
-0.1385
-0*1447
-0*1590
62.0637
-0.1412
-0.1411
-0.1061
-0.0376
-0.1405
-0.1524
-0.2889
61. 1696
-0.1524
-0.1405
-0.1053
-U*0003
-0*0010
0*0021
-0*604/
0.0004
0.0020
0.0076
0*1299
GAMMA= 1.5
-j _ i i ; i V / H s
0.
Z / H = 0.
L7A= 1.00
CHI =30*00
Z 1 3 A =
s.00 X/H=
3 e o • / n “
(WfL)
(UtL)
(W.DI
iu*o>
-0.1068
-0.1856
-0.195b
-0.8922
-0*1065
-0*1859
—0 • 1 9 1 to
-0*1695
62.0161
-0.1664
-0.185 1
-0.1034
-0*1068
-0.1663
-0.1986
-0.2949
61.1039
-0*1986
-0.1863
“0.1082
-0*0001
0.0007
0.0030
-0.5973
0.0002
0. 0004
0.0070
0*1254
CHI-45. 00
GAMMA = 1*5
ZET A -
4.00 X/H-
J.OO Y/H*
0.
Z/H- 0*
E TA = 1.00
(WfL 1
IU*L>
- TM»D>
(U»DJ
-0.2571
-0*2585
-0.2684
-0.8964
-0.2567
-U .2590
-0*2645
-0*1734
61.6665
-0.2591
-0.2579
-0.1052
-0.2570
-0.2595
-0*2716
-0*3001
60*9564
-0*2716
-0.2595
-0.1049
-0.0001
0.0009
0*0032
-0.5962
0*0003
0*0005
0*0072
0*1268
CHI-60.00
GAMMA = 1.5
ZET A =
4*00 X/H=
3.00 Y/H*
0.
Z/H= 0.
E7A = 1.00
1 W »L )
(U.L)
' iw.DJ
( U * D >
-0.6874
-0.3997
-0.4087
-0,9002
—0*6866
-0*4004
-0.4046
-0*1769
61.4374
-0.3992
-0.3986
-0.1046
-0*6872
-0*4011
-0*4121
-0*3049
60.5292
-0.4121
-0.4011
-0. 1043
-0.0002
0.0013
0.0034
-0*5952
0*0005
0*0007
0*0073
0*1280
CHI =75 *00
GAMMA= 1*3
ZETA =
•+ . GO X/H =
: J.OO Y / h =
i 0.
i/H= 0.
ETA* 1.00
(W.L)
(U*U
( W *D 1
IU.D)
-3.0122
-0.8164
-0.8192
-0*9036
-3*0106
-0*8178
-0*8153
-0*1602
59*1 159
—0.8095
-0.6142
-0.1015
-3*0117
-0*8191
-0*8227
-0* 3095
58.2095
-0.8227
-0.8191
-0. 1008
—0*0003
0.0026
0.0035
-0.5944
0,0011
0*0014
0*0074
0*1293
— “CHI *90.00
GAMMA* 1.5
ZET A ;
= 4.00 X/H* 3.00 Y/H'
■ 0.
Z/H- 0*
ETA* 1.00
rw.u
1 U.L I
u.or
(U.D)
-7.7285
0*0132
-0*0132
-0.6947
—7 .6415
0.0097
-0*0097
0*0279
6.3682
—0 .0036
0.0036
0.1040
-7 *od93
0*0170
-0*0170
-0*1018
7.6093
-O.Oi 70
0.0170
0.1018
-0.0392
-0.0038 .
0.0036
-0.5926
0*0480
-Q*0 9J2
0*0072
0*1297
l-15^9
67
TABLE 7.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, K ¥ 4.00, AND T| = 1.00
<g> x/H = 4.00
s
Correction factors for correcting from a wind tunnel
which Is
—
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1— i — “i “
to ground effect
CHI* 0*
1
GAMMA* 1.5
ZETA* 4.00
X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
<U*L>
(W.D)
(U.D)
-0.0001
-0.0600
-0.0666
-0.75S3
- 0.0001
-0.0601
-0.0613
-0.0751
62.1191
-0.0595
-0.0598
-0.0596
-0.0001
-0.0604
-0.0657
-0.1637
61.1677
-0.0657
-0.0604
-0.0595
0.0000
0.0004
-0.0009
-0.5947
0.0001
0.0003
0.0044
0.0865
CHI *16*00
GAMMA® 1.5
ZETA* 4.00
X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA* 1.00
(W.L)
(U.L)
(W.D)
(U»D)
-0.02X0
-0.07S1
-0*0848
-0.7625
-0.0209
-0.0782
-0.0796
-0.0764
62.0979
-0.0776
-0.0780
-0.0596
-0.0210
-0.0785
-0.0841
-0.1668
61.1482
-0.0641
-0.0785
-0,0595
0.0000
0.0004
-0.0007
-0.5957
0.0001
0*0003
0,0045
0.0904
CHI *30.00
GAMMA* 1.5
ZETA* 4.00
X/H* 4.00 Y/H* 0.
L/H- 0.
ETA- 1.00
(W.L)
IU.L )
(W.0I
(U»DI
-0.0598
-0.1037
-0.1105
-0.7658
-0.0597
-0.1039
-0.1053
-0.0776
62.0598
-0.1033
-0.1035
-0.0596
-0.0596
-0.1042
-0,1099
-0.1694
61.1114
-0.1099
-0.1042
-0.0595
0.0000
0.0005
-0.0006
-0.5963
0.0001
0.0003
0.0046
0.0918
CHI *45.00
GAMMA* 1*5
ZETA- 4.00
X/H* 4.00 Y/H* 0*
Z/H* 0.
ETA= U00
(W.L)
(U.L )
(W.D1
(U.D)
-0.1443
-0.1451
-0.1509
-0.1717
61.0281
-0. 1509
-0.1451
-0.0394
CHI *60.00
GAMMA- 1.5
ZETA* 4.00
X/H* 4.00 Y/H* 0.
Z/H- 0.
ETA* 1*00
(W.L)
(U.L)
(W.D)
(U.O)
-0.3861
-0,2235
-0.2301
-0.7713
-0.3859
-0*2238
-0.2249
-0.0796
61.7334
-0.2227
-0.2231
-0.0595
-0.3861
-0,2243
-0.2297
-0.1738
60.7871
-0.2297
-0.2243
-0.0593
0.0000
0.0006
-0.0004
-0.5975
0.0002
0.0005
0.0046
0.0942
CHI *75.00
GAMMA- 1.5
ZETA* 4.00
X/H* 4.00 Y/H* 0.
Z/H- 0.
ETA- 1.00
(W.L)
(U.L )
(W.D)
(U.O)
-1.6927
-0,4553
-0.6608
-0.7738
-1.6923
-0.4560
-0.4556
-0.0804
60.4270
-0.4534
-0.4545
-0.0591
-1.6927
-0.4571
-0.4605
-0.1757
59.4817
-0.4605
-0.4571
-0.0586
0.0000
0.0017
-0.0003
-0.5981
0,0004
0.0011
0.0049
0.0953
CHI *90.00
GAMMA- 1.5
ZETA- 4,00
X/M= 4.00 Y/H* 0.
Z/H- 0.
ETA- 1.00
(W.L)
(U.L)
(W.D)
(U.D )
-7.7075
0.0075
-0,0075
-0,6567
-7.6193
0.0024
-0.0024
0,0379
8.6067
-0.0000
0.0000
0.0594
-7.6683
0.0073
-0.0073
-0.0583
7*6683
-0.0073
0.0073
0.0563
-0.0392
0.0002
-0.0002
-0.5984
0.0490
-0.0049
0.0049
0.0962
68
TABLE 7.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 4.00, AND rj = 1.00
(h) x/H = 5.00
Correction factors for
correcting from
a wind tunnel
which is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI- i.«
- : h ... , , W
i , f i-
—
c. ’ M = A * V 9
1
t **L >
IO*L >
1 .-i 1 0 1
■WiwJCJ
- w « 6 / 2 6
•yiJiBO
-w • 34 Ifc
6 2 « 1 2 -• 6
- J « w 3 3 /
“ c/ • UUOO
"olUC^
-V • 4-414
--.Kb/
Oil 1 J V ^
-v • w* m
• u 3 H ^
~ w • 4/ Ji K i
UHiJOvL
• 0 u <j t
" ^
— ^ • 2 O ^ 7
i- *UuuG
0 *0006
u*0029
\J • 0c>32
CHi -
3 A V M A = J. , ‘j a.
CM- 4*w W
i - 3 • o C Y / H =
W, „/h = V.
(L i 6 = 1*40
< vi »L 1
< U * L >
! W » 0 )
( O *0 )
— 0 • ]. 3 4
-u ,
/
, 0 1 ’} 4
-u • 0449
62*14/5
- U * U 4 9 3
“ J • 4 i 3 4
“4 * - 1 -i
■U.V331
o i • 1 3 / a
- j* 0p3a
-o*
— O * o 3 O 1
u.wJoU
0 * 00 v 2
-0*06/i.
9* 0000
CHI =30, ' ".J
viA M MA= 1*3 a'
r 7 A = 4jL'0 X /
M = 7*00 -'/H =
0* t/H= 4.
t 7 A = i.OO
< W » L t
f U t L )
( w » ■_> )
( U *0 )
-u, ^44/
-0 • <J 54fc
— u • 64 i 7
■0iw514
h z ! i M ^ 6 r
— .J « w (U: j
- '' C* *•
“L.'JlI.i
-W • W A SO
"Lii-i u
o 1 * 1 i 4 V
“O' * L'O 13
- O • iw J 1< 1
*0132
“0 » \J 1 J2
Chl»4b*Oo
6 M MM A = 1,3 a.
tl*= 4*Jv a/
i = 5 m \j\j f / M “
4. 4/n= w *
L . H= A ♦ v C
( vJ * L )
1 U »L J
U » D J
(U»U)
-I- » -• V 2 2
-w. *-i924
- ^ ^
— J • 6 6 1 •'
6 2 « J 2 V 6
-0*492 3
-0*4362
• -923
“0 * v 9tb
—4 *uv3i-i
“U • 1 I vi9
oi.voK
“ V * U>JO
“Of J 4 2 6
JiL/uuJ
# U W >J
U 1 L/lU J
>W# iJO Jw»
0 « tub;
C H i = 6 U « 0 o
dAMMA= 1.3
LiA = 4,00 a/I
-1= 6.0u 7/h =
4. t/r= C.
E7A= it -C
( W » L >
(U*L»
t W t L) )
(0*0 f
-U* 1426
-v*l4b6
-v • fe ri 3 V
-C* 14/ f.:
-■■j • 1 4 J 1
— w • w.44 <
u 1 « o 7 * 1
-0.1421
“U • 1 42 6
- u • o 3 6 t
-0*24/0
“0 • 1432
-0, 1462
-U • i 1 20
6o , 4w66
“0 • 1 402
“O » 1432
-o * C 3 « 1
J • UU4u
0 • 00 -/ 4
—0*0024
-0.0719
'J • 004 *
O*00«H
0*0031
C H I = V 0 * J 0
ijAMM A = ... a.)
liA - ,,J U A,l
■i - 3 * 4 u / / i-i —
0 * > / H = u •
l~A= 1*00
I W * L I
(0»L 1
1**0 )
1'<*U)
-1 *u629
-l *246/
-wuiiL
-l*'-629
-o*29u7
-w> •*
61*03/9
-0.2 b 9 7
— 6 • i. >43
“v.UJOi
-1 * 06 3u
"0*29 j.6
“w * 2430
“«* 2 9 3b
“o « 29 aO
“ o * 0 J . 7
O.GOCi
0&JUU9
-O • JOi.3
-4 • 37 30
0*0001
W 4.0 0033
CHI » 90
oA MV A = i « p 21
:. 1 A- 4 • 0 0 A /h
5 • 0U // h=
0* 4/M= L ♦
tTA= 1*00
( t* * L )
1 U * L )
( W * p )
<o»u )
-7,69/1
J » u u o 1
-o*oC 61
-6 • oi 1
- <
0, OOC'6
6.0 J <15
J * 0 O' w J
4.4302
-7*6561
u « j C 3 6
-0 • 0../36
“O'* V 1 iti
7*6361
“0 * 00 j a
0*0036
-*-j /6
-0*03 90
0*0023
-uKCtj
-u • p y 4i
0*0453
“0*0032
0.UUJ2
0*0odo
6^T-T
l-1549
69
TABLE 7.- Concluded
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 7 = l- 5 « S " 4 00, AND ^
(i) Miscellaneous additional values of x/ H
Correction foctors for correcting from a wind tunnel which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floe r
only
closed
closed
on bottom
only
to free air
to ground effect
— — “
r-
ch 1 • 1 5 • 00
GAMMA = 1.5
2FT A = 4.00
y/H =
0.07
Y/H= 0.
Z/H = 0.
FTA = 1.00
0*001 O
0*0000
0.01 55
0.0366
! W.L >
(U*L1
(W.D1
(U.O)
-26.9778
0.6302
-27.5040
1 .*054
-26.9741
0.6302
-27.5059
1.4357
? R . 1 906
-27.4730
0.6303
13.3149
-26.9760
0.630?
-27.6213
1.3990
27 . 6220
-27.6213
0,6302
13,7143
-0.0018
0.0000
0*0177
-0.0976
CH! =30.00
GAMMA= 1.5
?ETA = 4, on
X /H =
0.17
Y/M= O.
Z/H = 0.
pT fti 1,00
(W.L )
(U.L>
(W*0)
(u.nj
•27 .0 A0?
4.411 O
-23.7790
2. 9267
-27.076!
4*4100
•2 3 .7806
3.0530
23.7747
-73 ,7480
4*4111
12.6640
-27.0782
4.4109
-23.7963
3.071 1
23. 1 653
-77*7963
4*4109
12*6634
-0.0020
0*0001
0.0173
-0.OQ46
0*C0?1
0*0000
0.0> 6*
0*0369
CHr=45«no
GAMMA* 1.5
ZFTA = 4.0C
X/H.
n*26
Y/H* 0.
Z/H* 0.
ETA” 1.00
(w.u
(Ufl )
I W.D1
iu.ni
-2B . 609 P
2.115!
-19.9951
0.0566
-? ft. 8048
2.1150
-1 9. <3998
0*2312
29.3934
-19.9676
2.1165
1 2.4760
-28 .8074
2*1149
-70.015?
0.1823
28 * 8074
-20.0162
7*1140
17 1 47 5 7
-0.0074
0.000?
0.01 71
-0.1267
0*0076
0*000!
0*01 64
0*04 B 9
CHI =60. OC
GAMMA = 1.5
7 FT A= 4,00
X /•- =
0.43
Y/H* 0.
Z/HS 0.
FT A= 1.00
<W »L )
fU.L 1
(W.D)
UNO!
-30.1169
1 .9143
-14.5653
-0.7798
-30.1101
1*9141
-14. 5670
-0*6^79
90.4197
-14.6756
1.9162
1 n, p -740
-30.1136
1.9139
-14.6822
-0.6052
29,8068
-14.582?
1,9139
10.8779
-0.0073
0.0004
0.0166
-0.1746
0*0036
0*0002
0.015?
0.0673
CH 1=75.00
GAMMA* 1*5
ZETA = 4.00
X / H =
0 . 68
Y/H* 0.
Z/H = 0.
ETA* 1.00
(W.L )
f U . L)
l W*D )
( LJ * D 1
-20.9424
6.4571
-6.0415
-0.0111
-20.9296
6.4566
-6.0428
0.325!
19.7612
-6.0133
6.4592
2*3399
-20.936?
6 .4561
-6*0576
0*2331
19* 1094
-6.0576
6.4561
;■* 3379
-0*0062
0*0010
0.0161
-0.2442
0.0066
0.0004
0.0148
0.0970
70
TABLE 8
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, X = 10.00, AND rj = 1.00
(a) x/H = -2.00
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
“ ■ “ ' 1 — i —
— ■■I
to grour
id effect
chi* o.
GAMMa- 1,5
ZETA- 10,00 X/H=-2.00 Y/H- 0,
Z/H* 0*
ETA- 1,00
ru*u
tV* 01
-0,0003
0,2404
0.2154
0,7913
-0,0002 -0,0433
0,2404 0,2220
0,2159 0,2402
0,1313 -0,2384
-0,0003
0,2405
0,2114
0*2842
-0,2609
0,2114
0,2405
-0,2384
-0,0000
-0,0001
0,0040
0,5070
0,0000
-0,0001
0,0044
-0,1530
CHI *15*00
GAMMA- 1,5
ZETA- 10,00 X/H*— 2* 00 Y/H- 0,
Z/H- 0,
ETA- 1,00
tV*L)
tu,u
(WfO>
fU»D)
0,0488
0,1848
0,1607
0,7825
0*0489 0.0092
0,1849 0.1672
0,1612 0,1847
0,1195 -0*2184
0,0488
0,1850
0,1568
0,2725
-0,2060
0,1568
0,1850
-0,2384
-0,0000
-0,0001
0,0039
0,5100
0,0000
-0,0001
0,0044
-0,1529
CHI *30,00
GAMMA- 1,5
ZETA- 10,00 X/H*-2,00 Y/H- 0,
Z/H* 0,
ETA- 1,00
<W*L)
(U*L)
<w»0)
(UtD)
0,0793
0,1396
0,1160
0,7755
0,0793 0,0425
0,1397 0,1225
0,1165 0,1395
0,1101 -0,2384
0,0793
0,1398
0,1121
0,2630
-0,1708
0,1121
0, 1398
“0,2383
-0,0000
-0,0001
0,0039
0,5125
0,0000
-0,0001
0*0044
-0,1529
CHI ■43*00
GAMMA- 1,5
ZETA- 10,00 X/H--2 « 00 Y/H- 0.
Z/H* 0,
ETA- 1,00
IW»L)
(U»L)
IW.O)
IU,0>
0,0985
0,1010
0,0776
0*7696
0,0986 0,0641
0,1011 0,0840
0,0782 0,1008
0,1022 -0,2383
0,0985
0,1012
0,0738
0,2550
-0,1475
0*0738
0,1012
-0, 2383
-0,0000
-0,0002
0,0038
0,5145
0,0001
-0,0001
0,0044
-0,1529
CHI-60, 00
GAHMA- 1,5
ZETA- 10,00 X/H— 2,00 Y/H- 0,
Z/H* 0,
ETA- 1,00
tW» L)
IU*L)
iu*oi
0,1103
0,0669
0,0432
0,7643
0,1104 0*0781
0,0670 0.0496
0,0438 0,0665
0,0951 -0,2381
0,1103
0,0671
0,0394
0,2480
-0, 1320
0,0394
0,0671
-0,2381
-0,0000
-0,0002
0,0038
0,5164
o,oooi
-0,0001
0,0043
-0,1528
CHI-75, 00
GAMMA- 1.5
ZETA- 10,00 X/H— 2,00 Y/H* 0,
Z/H- 0,
ETA- 1,00
l«*U
(U »L )
1 w*o>
(U,0)
0.1164
0,0364
0,0112
0,7595
0,1166 0,0865
0,0366 0.0175
0,0117 0.0358
0,0886 -0,2377
0, 1465
0,0368
0,0074
0,2414
-0,1222
0*0074
0,0368
-0,2377
-0,0001
-0,0005
0,0038
0,5101
0,0001
-0,0003
0,0043
-0,1528
CHI-90,00
GAMMA* 1,5
ZETA- 10,00 X/H— 2,00 Y/H- 0,
Z/H- 0,
ETA- 1,00
fW»l)
(U,L>
(W,0i
iu,bi
0.1165
0.0197
-0,0197
0,7547
0,1174 0,0906
0,0193 -0,0135
-0,0193 0,0135
0*0826 **0,2358
0,1167
0,0235
-0,0235
0,2352
“0,1167
-0,0235
0,0235
H), 2352
-0,0002
-0,0038
0,0038
0,5195
0,0007
-0,0043
0,43043
-0,1526
6 ^ 1-1
L-15^9
71
TABLE 8.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y =1.5, C = 10.00, AND tj = 1.00
(b) x/H = -1.00
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
)d effect
1 .5 ZETA * 10.00 x/H=-l . GO _ V/h= 0 .
( W i L I
(U»L )
Mf*r> i
-0 • ..'0ft 2
0.98 H
‘0*7183
1.5976
-0.0050
0.9H11
0.7180
1.1836
-0.7574
n, 7?fi9
0,9*09
-0,9441
-0.COM
0.9H 3 7
0. 71 7?
1. ^940
-1. inn
0,717?
0.957 ?
-0,9441
-0,000 1
-0.0001
0,0041
0.0001
-0*0001 ...
0.006*
0 , ~ •"•94
-0.1104
C H i = i 5 , o ■
jAi'ii'.A = 1.5 ....
. 7 E T A_=_l 0.00 X/H«-
UOji V_/H= 0.
2/H= 0.
E T A = 1,00
0,6062
0,7690
-0 • ? 4 4 ?
( A * L )
<U«L>
( to , u )
< I.J * D )
j • 7 5 a 9
".5112 "
: .3019
0. bvo
O.5110
1 .0546
-0.519 1
c It*
C.' « 7 5« 7
— 0 , 7 4 /
0.1 6P. 5
.0*7690
0 . 6052
1 . 1 969
-0.0003
-o.ro 01
o.nri6'~
0. ■’■0 5 0
0,0001
. -.“£'j.OCOJ
0.0065
-0*1 1 70
CHI = 3' ,
OA'^A* 1,5
ZPTA- 10,"',
[_• r r v/h-
: 0.
7 /h= n .
c T a = i,nn
< lv , L )
(U.L )
(to 1 D )
( U » 0 )
; 5 . : " 9 7
0.5795
0.3417
1.43o4
0.3099
0 . 5 1 ? 3
0.3435
1.0063
--
-0.3624
0.3522
0 « 6~7 5> ; r
- 0 . >- 4 :• 6
0. 3 098
0.5 •' r 6
0.5557
I • 1 2 Cl
-0. 7099
0.335?
0. 5 796
-0, '435
-0,0001
-0.0001
0.0060
0.3] 07
0,000]
-Q.0OQ1 _
0,0058
-0*1139
ch r *45.
O.A V^ A =_ 2 , 5 _
. L. f _T.a=_k . 00
,.100, Y/H=
.0,
//H= 0,
FM = 1,00
( to , L )
(U.L)
( W .0 )
( U.D 1
0 , ■! & 5 6
0,4? 8 3
v, 1958
1.3706
0,
0.4?ci
0 , 1 ■» 5 5
0, 940 6
-0.2 46 I
0.2 06 3
0.4280
-0.741 H
0. c
0,4?P4
0. 1 H9h
1 .0660
-0,6009
0 • 1 0 q R
C. 4?84
-0,94 1 8
-0.0001
-0,0001
0.0060
0.3147
0,0001
-0,0QQ.l .
0*0058
-0.1 1 65
CH 1 *60.00
GAMMA* 1,5
ZE TA= 10,00
X/H=-l
•00 y/Hs
0.
Z/H* 0.
E“A= 1,00
( W»L 3
(U.L 1
(W.D)
(U,D)
0.4305
0,2986
0.0648
1.3184
C .*+308
0*2986
0,0646
0. 6634
-0, 1 8? R
0.075 1
0*298]
-0," '■>(* ]
0.4307
n.?gP7
O.HRRn
0,
-0,6353
0*05*8
0.7987
-0. 93R?
-0.0001
. . -0*0002
O.H060
0.3186
0.000?
rQjQQQl
0*0057
-0.1 164
—
■ -
CHI *75.00
GAMMA= 1,5
zeta* 10,00
X /H=-l ,
.00 Y/H=
0.
Z/H* 0,
FT A* 1.00
( W » L )
(U.L)
rw.Dj
(U.OI
0.4499
0.1934
-0,0573
1.2709
0.4505
0.1935
-0.0575
0.8311
-0.1330
-0.0470
0.1926
-0.9294
0.450?
0.1937
-0.06 32
0.9486
-0.473?
-0.063?
0.1937
-0.9?9S
-0.0003
“0,0004
0.0059
0 • 3??3
0.0003
-0,000?
0.0057
-0,11 76
CHT »90,00
GAMMA* 1*5
ZETA* 10.00
X/H*-l,
,00 Y/h=
0.
Z/H* 0,
FTA= 1,00
..
(W.L)
(U.L )
0.4356
0,1741
0,4387
0.1745
-0.1745
0.7821
-0.0989
-0.1639
0.1639
-0.9009
0.4368
-0.4368
-0.001 2
0.001 Q
(W.03
(U.D)
-0.1741
1.2260
0. ] 801
-0.1801
0.9004
-0.1801
3. 1801
-0.9004
-0.0060
0.0060
0.3256
“0,0056
0.0056
“0, 118?
72
TABLE 8.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - l-«. ?
(c) x/H = y/H = z/H = 0
10.00, AND rj = 1.00
8
Correction factors for correcting from o wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
r
to ground effect
C H I s- 3 ._00 ~GAMMA»~ 1*5
( W ♦ L)
{ U t L_j_
t W » 0 1
f U.D J
-166.3292
-T0.57F8
- Y9 4 . 5 A 76
' 1 ,7885
7 FTAx"10.'ftg~- X/H.=
-166.3290
^ -10.5790
- -1947 5 4071 '
1 .4453
IBB. 13^
-194.5350
"-T0V5TRB -
S3.05?l
“Z7HS ' 0 .
-166. 3291
75 » 5 759
4T94I554T5' '
1 .4289
FTA- T.nO
197.5983
-194.5545
-1U.57H9
83.0520
- 0. 0001
O.OTTOl
- U.UU6H"
-0.0403
0.0001
-■a.oooi
070054"
0.0165
CHI- 3.00
{ W » L !
< U ♦ L 5
( W ♦ D )
{ U.D )
3AMMA= 1 , 5_
-166.3292
10.5758 '
-185.642 4_
"‘21 ,'32W4 -
2ETA= 10.00 ' 'X7H
-166.3Z50
’ 10.5790“
— 1 B5 « 8427
2 f". 174 9-
ETA^ 1 , 00
t w * u
( u . u
t vi t L> )
(U.D)
GAMMAS 1.6
-148,565 1
48 .4906
-153.7623
48,8691
l e j ;,= 10.00 X/H=~ 0 . ... Y/H=
4/H*
0 .'
-148.5649 04,2492
48.4906 - 153.7696
-T53.76 2’6 “ " '"4B.4906
48.9073 66.4143
-148.5650
48.4906
^lssrtew
E tA* 1 .00
83.7132
-153.7890
' ~"5B 75935“
68.4143
-o.oooi ' a.ou'Oi
-o.oooo -o.nooo
0. U06 ' 8 0TTJTT54"
-0.0274 “0.0108
I W * L )
(U.U
( W t D >
{ U ♦ D J
GAMMA = 1.5
-104.4455
73.5900
1 0 4 , 5 « 5 5
55.8213
Z E T A =_
X /H = 0.
v / h = 0, ___ 2 / H - _0_.
-104.4463 39*3263
73.6900 -104.5828
-i 04,5969" 7T75 900
56.R5C0 33.6826
-104.4454
73.5900
“ ^T0'4.60 2 2'
55.8419
E T A = 1.00
38.7940
- 1 04 • 60 ? 0
— "73 ,'5900
33.6827
-0.0001 0.0001
-O.COOC _ -o.oooo
(TiTtiTAT ' O.nuRJT
-0.0706 0.0081
CHI =45.00 GAMMA * 1.5.
(W.L) -59,6833
(U»L) 69.5/1/
( W» D I -65.4070
(U.D) 41,5877
Z FT A = 10.00 X/ H = 0»
y/H- 0. Z /h= P .
-59,6829 24.753B
69.5/17 _-65.4562
-ou .4o9j "6'9.57 1 i
41.6063 2.0481
-59.683!
69.5717
-65.4757
41.6025
ETA- l.O0_
24.2246 -0.0002
-65.4757 -0.0000
69. '5717 0YTTD68
2.0480 -0.0148
0.0002
-0.0000
U.1J06 4"
0.0038
CH 1=60.00
(W.L)
J.U.U
( W » D )
) U.D)
GAMMA* 1.5 It TA* 10.00
X/H= 0. _V/H-
-32.8259
49,9642
-42.8184
22.4405
-32..S255
49*9642
t:477B7 60
22.4538
23.5579
-42.8057
49.96'Tl
-10.9418
0.
Z/H = 0. ETA= 1.00
-32.8257 23.0316
49.9642 -42.825?
44 2", B 25 2 49'. 9642
22.4500 -10.9419
- 0. 0002
-o.nooo
‘~avnTT&B
-0. 0095
0.0002
-o. nnnn
— — OTTTtnsrc"-
0.0037
- CHI =75. 00 GAMMA- 1.5
(W.L)
(U.L)
‘[V.DT
{ U.D 5
-24.5164
32.6540
43T. 1609
8.3090
;PTA= 10.00 X/H- 0.
Y/H= 0. Z / H - 0.
-24.5155
32.6540
4TI7TC17 '
8.3155
24.3009
-31. I4H2
“32'. 6578
-7.4640
-24.5160
32.6540
-31.1676
8.3137
E T A= 1_.00
23.7773
t3 1 . 1676
12.6540
-7.4641
-0. 0004
-0.0000
0.0068
-0.0046
0.0005
-O.DOOO
- 0.0 CT4
0.TIC18
"CHI *9 07 Off” GAMMA- 7.5
TW7CT -277*7®*
1U.L) 23.8664
TTTCn 423,8864
(U.D) -0,0000
7 ETA- 10.015 * "X“/H= 0.
Y/H- 0.
- - ^T3.86T7 24.3937
23.8669 -23.8538
-7T. 8669“ ?3i8338
0,0000 -0.0000
- -23.8732
23.873?
= 23.97 3?
- 0 .
— — 23v8T3?
-23.8732
23.87 3?
0.
- 0 . 0 09* -OrDDArO
-0.0069
0. 0009 0,00 63
-0.0000 0.0000
6t£T-' 7
L-15^9
73
TABLE 8.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 7 = 1.5, 5 = 10.00, AND q = 1.00
(d) x/H = 1 .00
Correction factors for
correcting from
a wind tunnel
which is
closed
close d
on bottom
only
open
closed floor
only
(ground effect)
open
fl oor
only
closed
closed
on bottom
only
to ground effect
GAMMA* 1.5 ZETA* 10.00 X/H* 1.00 Y/H* 0.
(W.L)
-0.0082
-0.0080
383.4458
-0.0081
3 8?, 7?56
-0.0001
0.0001
(U.L >
-0.9811
-0.9811
-1.0729
-0.9812
-1 .0885
0.0001
0.0001
(W.O)
-1 .0828
-1*0829
-0*9809
-1.0885
-0*9812
0.0057
0.0055
IU.DI
-2.8215
-2.3429
-0*9441
-2.4591
-0,9441
-0.3574
Oil 26?
CHI * 1 5 • 00
GAMMA*
1.5
ZETA* 10.00
> /H*
1.00
Y/H= 0.
Z/H* 0.
ETA= 1.00
(W.L )
(U.L)
(W.D)
(U.D)
-0.3483
-1.2914
-1.4058
-2.9615
-0.3361
-1.2537
-1.3604
-2.3483
383.1476
-1.3959
-1.791 7
-1.0294
-0.3422
-1.7726
—1 *3888
-2*6440
3 67.431?
-I « 3888
-1.7726
-0.943?
-0.0061
-0.01 R«
-0.01 70
-0.4176
0.0061
0.0189
0.0284
0.1957
CHI =30.00
GAMMA*
1.5
ZETA* 10.00
x/h*
1.00
Y /H* 0.
Z/H* 0.
r T A = 1*00
(W.L )
(U.L )
(WiD)
(U.D)
-0.9653
-1.6866
-1.8017
-2.9483
-0*9651
-1*6867
-1.8019
-2.4840
38? .553R
-1.7917
-1 .6864
-0.941 1
-0.9652
-1.6867
-1.8076
-2.6070
’81, 8404
-1 • 8075
-1 • 6867
-0.941 1
-0.0001
0.0001
0.0058
-0.3413
0.0001
0.0001
0.0056
0.1230
CHI *45.00
GAMMA* 1,5
ZETA* 10.00
X /H =
1.00
Y/H= 0.
Z/H= 0,
ETA* 1.00
(W.L)
(U.L)
(W.O)
(U.D)
-2.3191
-2.3478
-2.4613
-2.9994
-2.3189
-2*3479
-2*4615
-2.5407
38) .227?
-2.451?
-2.3476
-0.9366
-2.3190
-2.8480
-2.4672
-2.6624
’ 5 0.5168
-2 i 467?
-2.3480
-0. 9366
-0.0001
0.0001
0.0058
-0.3369
0.0001
0.0001
0.0057
0.121 9
CHI *60.00
GAMMA* 1.5
zfta= 10.00
X/H*
1.00
Y/H= 0.
2/H* 0.
ETA* 1.00
(W.L)
(UiL )
(W.D)
(U.D)
-6.1952
-3.6309
-3.7276
-3.0462
-6.1949
-3.6309
-3.7278
-2.5925
377*3850
-3.7175
-3,6305
-0.9250
-6.1951
-3*6311
-3.7335
-2*713?
376.6766
-3.7335
-3.6311
-0.9250
-0.0002
0.000?
0.0059
-0.3330
0.000?
0.0001
0.0057
0*1206
CHI *75.00
GAMMA* 1,5
ZETA = 10.00
X /Hr
1,00
Y/H= 0,
2 /H = 0.
E~A = 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-27.1383
-7.4408
-7.4260
-3.0902
-27.1377
-7.4409
-7.4262
-2.641?
356,5082
-7.4153
-7.440 1
-0.8591
“27*1380
-7.4411
-7*4319
-2.7608
355.3020
-7.4319
-7.4411
-0.8591
-0.0003
0.0003
0.0059
-0.3294
0.0004
0*0002
0.0057
0.11Q6
CHI-97.00
GAMMA* 1*5
ZEYA* 10.00
*/H =
1.00
Y/Hs 0.
Z/H= 0,
E T A = 1.00
(W.L )
(U.L)
(WiD)
(U.D)
-48.1884
0.1741
-0.1741
-1.2260
-48.1770
0.1744
-0.1744
-0.7821
48,8864
-0.1639
0*1639
0.9009
-48,1 R3?
0.1 801
-0.1 801
“0.9004
4 8 . 1 8 9 ?
-0.1801
0.1801
0.9004
-0.0052
-0.0060
0.0060
-0.3256
0.006?
-0*0056
0*0056
0*118?
Jk
TABLE 8.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, K = 10.00, AND tj = 1.00
(e) x/H =2.00
Correction factors for correcting from a wind tunnel which is
CHI* 0,
GAMMA* 1.5
2ETA- 10*00
X/H-
2.00
Y/H-
0*
1 / H« 0.
ETA- 1*00
iw*u
(U*L 1
(H*D)
(UtOl
-0.0003
-0*2406
-0*2555
“1*1989
-0*0002
-0*2404
-0.2548
-0.5149
383.0319
-0.2495
-0.2402
-0.2384
-0.0003
-0.2405
-0.2590
-0.6671
382*1873
-0.2590
-0.2405
-0*2384
-0.0000
0.0001
0.0035
-0.5318
0*0000
0*0001
0.0042
0.1523
CHI *15*00
GAMMA* 1*5
ZETA* 10.00
X/H*
2.00
Y/H-
0.
2/H- 0.
ETA- 1*00
tw.u
IU*Li
IW.Di
(U»0)
-0*0845
-0*3148
-0.3315
-1.2140
-0*0644
-0.3148
-0.3309
-0*5323
382.9531
-0.3255
-0.3146
-0*2492
-0*0836
-0.3130
-0.3321
-0.6774
382* 1112
-0*3321
-0.3130
-0.2364
-0*0008
-0*0018
0*0006
-0*5365
-0*0008
-0.0019
0*0012
0*1449
CHI *30*00
GAMMA* 1*5
ZETA- 10*00
X/H*
2.00
Y/H-
0*
2/H* 0.
ETA* 1.00
iU*L )
<UtL)
( W »D )
<U*D)
-0.2391
-0.4135
-0.4315
-1*2126
-0*2390
-0.4155
-0*4309
-0*5334
362*8085
-0.4255
-0*4153
-0.2383
-0.2391
-0*4156
-0*4351
-0*6860
381*9680
-0.4351
-0*4156
-0.2363
-0.0000
0.0001
0.0036
-0.5268
0*0001
0*0001
0*0042
0*1526
CHI *45.00
GAMMA* 1*5
ZETA* 10.00
X/H*
2*00
Y/H-
0*
2/H* 0*
ETA- 1*00
tU»L)
(U*L)
(H*D1
ru.D)
-0*5768
-0*5 768
-0*5949
-1*2182
-0*5767
-0*5789
-0.5943
-0*5408
362*4727
-0.5668
-0.5786
-0.2382
-0.5768
-0.5790
-0.5985
-0.6934
381*6338
-0*5985
-0.5790
-0*2362
-0.0000
0.0002
0.0036
-0*5248
0*0001
0*0001
0*0042
0*1526
CHI *60*00
GAMMA* 1*5
ZETA* 10.00
X/H*
2*00
Y/H-
0*
2/H* 0*
ETA- 1*00
CW*L)
IU.L)
(W«D>
IU*D i
-1*5439
-0*8947
-0*9100
-1.2231
-1.5437
-0*8948
-0.9094
-0.5475
381*5030
-0.9038
-0.8943
-0.2379
-1.5438
-0.8949
-0*9137
-0*7001
380*6656
-0*9137
-0*8949
-0.2379
-0.0001
0*0002
0*0037
-0*5230
0*0001
0*0001
0*0043
0.1527
CHI*75.00
GAMMA* 1*5
ZETA* 10.00
X/H*
2*00
Y/H-
0*
2/H* 0*
ETA* 1*00
1W»U }
1U*L)
IW»D)
IU*D 1
-6.7691
-1*6216
-1*8328
-1*2278
-6*7688
-1*8220
-1*8322
-0.5537
376.2790
-1*6266
-1.8211
-0*2368
-6.7689
-1*8223
-1*8365
-0.7065
375*4429
-1*8365
-1*8223
-0*2368
-0.0001
0*0005
0*0037
-0.5213
0*0002
0*0003
0*0043
0*1527
CHI *90*00
GAMMA- 1*5
ZETA* 10*00
X/H*
2.00
Y/H*
0.
2/H* 0*
ETA- 1*00
(M.U
tU*L J
(W.D)
(U »D i
-47*6690
0*0197
-0*0197
-0*7547
-47*8555
0.0192
-0.0192
-0.0826
48.6965
-0*0135
0.0135
0.2358
-47*8628
0*0235
-0*0235
-0.2352
47*8628
-0.0235
0.0235
0.2352
-0*0062
-0*0038
0.0038
-0.5195
0*0074
-0*0043
0*0043
0*1526
6tfCT-l
75
TABLE 8.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR r * 1 -&, C = I0 00 ' ” = 1 00
(f) x/H = 3.00
ON
T*
Correction foctors for
correcting from
a wind tunnel
which is
close d
closed floor
open
closed
§
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
■ "T
CHI * 0.
'
GAMMA® 1.5 ZETA’ 10*00 X/H = 3.00 Y/H»
—
0.
Z/H = 0.
eta= 1.00
(W.L)
( U » L )
( W »D )
lUtDI
-O.uGOC
-0*1064
-0.1112
-0*8906
-0*0000
-0*1064
-0.1096
-0.1768
382 .9967
-0.1074
-0.1063
-0 *1061
-O.OUOO
-0.1 U65
-0.1125
-0*3039
302*0015
-0.1125
-0 • 1065
—0 *1061
-0.0000
0*0001
0*0013
-0*5948
w • 0000
U*00oi
0*0029
0*1270
CHI»15.0u
GAMMA= 1*5
L t7A= 10 *0 u a
7H* 3.00 f/H=
0 «
Z/H = 0.
ETA’ 1*00
(W.L)
IU»L )
(W.O)
(U.D)
-0.0379
-0*1417
-0.1466
-0*9120
-0*0362
-0.1355
-0.1307
-0*1676
3B2.9504
-0.1428
-0.1416
-0.1179
-0 * o371
-*.1386
-0*1440
-0.3070
302*0372
-0. 1440
-0.1386
-0. 1061
— 0 • GOG 0
— J *00 30
-0*0018
— O*oO30
0*0009
0*0032
0*006 1
0*1394
CHI ’30*00
GAMMA’ 1*5
ZETA* 10.00 a
/H= 3.^ </H*
U «
i/H* v.
t . A* l»uu
(W.L )
( U »L )
■ - - f W » D )
(U.D)
-0*1062
-0*1841
-u * 1891
-G *903 1
-0.1061
-0.1841
-u.1075
-0* 1812
382*0839
-0*1852
-0*1840
-u.1061
-O.lobl
-0*1842
-0.1 904
-w* 3u96
581.9709
-0. 1904
-0.1042
— u . 1060
-u.UOOO
0*0001
0*0014
-0.5935
0*000o
0*0001
0*0029
0*1284
CHI =45*00
GAMMA = 1*5
Z£TA = 10.00 X
/H ■ 3*00 V/H= 0*
i/H» 0
ETA* 1*00
(W.L)
< U*L )
(W.O )
(U.D)
—0*2562
-0.2565
-0.2615
— G. 9049
— 0 *2562
-0*2566
-0*2600
-0*1820
302*7401
-0.2676
-0.2564
-0.106 1
-0.2562
-0.2567
-0.2629
-0.3118
Jbl. 0360
—0*2629
-0.2567
-0. 1060
-0.0000
J . 000 1
x 0.0014
-0.5931
0*0000
0* 000 1
0*0030
0*1290
CH I =60*00
GAMMA= 1*5
ZETA’ 10*00 *
/ H = 3 . Oo Y/H* 0.
Z/H = 0
, t T A= a. 00
(W.L)
iL.l )
^W.D)
/(U»DI
-0 .686 G
— C * 3965
-0*4014
-0*9065
-0*6859
-0*3966
-0*3999
-0*1 844
382.3186
-0.3975
-0 .3964
-0.1 060
-0.6859
-0.3967
-0.4028
-0.3139
301.4U73
-0 . 4u28
-0.3967
-0.1060
-0.0000
0.0002
0.00 i4
-0.5927
O*0000
O*0001
0*0030
0*1295
CHI =75.00
GAMMA’ 1*5
Z£7A= 10*00 A/H* 3*00 t/H
= w.
t/ h = *
* £ \ A= 1.00
(W.L J
(U.L )
(W.D)
(U.D)
-3*0000
-0.0072
-G.8114
-0*9060
—3 * 0079
-0*8073
-0*8099
-0*1058
379.9939
—0 .00/5
-0.8068
-0.1059
-3. 0000
-0.8076
-0*8129
-0*3158
379. 0833
-0.0129
— 0 * 8 o 76
-0. 1059
-0*0000
0*0004
0*u015
-0*5923
0*00ux
U » JOU 2
D • DU 30
0*1299
CHI =90*00
GAMMA’ 1.5
ZETA’ 10*00
X/H= 3.00 Y/H* 0.
Z/H* 0* ETA= 1*00
(W.L)
(U.D
(W.D)
(U.D )
-47.0050
0.0055
-w.u055
-0*6972
-47*7903
0*0040
-0*0040
0*0249
40.7073
-0.0U16
0.0016
0.1057
-47.7986
0*0070
—0 • 0070
-0.1054
47.7906
-0.0070
0.0070
0.1054
—0*0064
-0*0015
U*u0l5
-0*5918
0*U0 78
-0*0030
0*0030
0*1303
76
TABLE 8.- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 10.00, AND r; = 1.00
(g) x/H = 4.00
s
Correc
tion factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CHI- 0.
GAMMA- 1,5
ZETA* 10.00
X/H = 4.00 Y/H- 0.
Z/H- 0.
ETA* 1.00
(w.l)
<u*u
(W*D)
(U.D)
-0.0000
-0,0597
-0.0626
-0.7694
-0.0000
-0.0598
-0.0605
-0.0795
382.9949
-0.0597
-0.0597
-0.0597
-0.0000
-0.0598
-0.0624
-0.1730
302.0418
-0.0624
-0.0598
-0.0597
0.0000
0,0001
-0.0002
-0*5964
0.0000
0.0000
0.0019
0,0935
CHI *15. 00
GAMMA- 1.5
ZETA* 10.00
X/H- 4.00 Y/H* 0.
Z/H- 0.
ETA* 1.00
(W»L)
< U*L >
<W»D)
(U.D)
-0.0209
-0.0778
-0.0808
-0.7710
-0.0208
-0.0779
-0.0786
-0.0801
383*0045
-0.0778
-0*0778
-0.0598
-0.0208
-0.0779
-0.0806
-0.1743
382.0521
-0.0806
-0.0779
-0. 05y7
-0.0000
0.0001
-0.0002
-0.5967
0.0000
0.0000
0.0019
0.0942
CHI-30.00
GAMMA- 1.5
ZETA- 10,00
X/H- 4.00 Y/H- 0.
Z/H- 0.
ETA- 1.00
(w.u
I U *L )
( W * D )
(U.D)
-0.0597
-0.1034
-0.1064
-0.7724
-0.0597
-0.1034
-0.1043
-0.0806
382.9665
-0.1034
-0*1034
-0.0597
-0.0597
-0.1035
-0.1062
-0.1754
382.0147
-0.1062
-0.1035
-0.0597
-0.0000
0.0001
-0.0001
-0.5969
-0.0000
0.0001
0,0019
0.0948
CHI =45,00
GAMMA- 1.5
ZETA* 10.00
X/H- 4.00 Y/h= 0,
Z/H* 0.
ETA- 1.00
(W.L)
(U.L >
(W.D >
(U.D)
-0.1441
-0.1443
-0.1470
-0.1764
381.9349
-0. 1470
-0. 1443
-0.0597
CHI -60.00
GAMMA- 1.5
ZETA- 10.00
X/H- 4,00 Y/H* 0*
Z/H* 0.
ETA- 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-0.3858
-0.2229
-0.2257
-0.7746
-0.3858
-0,2229
-0.2237
-0.0815
382.6048
-0.2228
-0.2228
-0.0597
-0.3858
-0,2230
-0.2257
-0.1772
381.6539
-0.2257
“0.2230
“0.0597
0.0000
0*0001
-0.0001
-0*5974
0.0000
0.0001
0.0020
0.0958
CHI -75.00
GAMMA- 1.5
ZETA* 10.00
X/H- 4.00 Y/H- 0.
Z/H- 0.
ETA- 1.00
(W.L 1
(U.L)
(W.D)
(U.D)
-1.6919
-0.4536
-0.4564
-0.7756
-1.6919
-0.4537
-0.4543
-0,0818
381.3066
-0.4534
-0.4535
-0.0597
-1.6919
-0.4538
-0.4563
-0.1780
380.3560
“0.4563
-0.4530
“0,0596
0.0000
0.0002
“0.0001
-0.5976
0.0000
0.0002
0.0020
0.0962
CHI *90.00
GAMMA- 1.5
ZETA- 10.00
X/H* 4.00 Y/H* 0.
Z/H* 0.
ETA- 1.00
(W.L )
(U.L )
(W.D 1
(U.D)
-47.7814
0.0030
-0,0030
-0.6572
-47,7670
0.0009
-0,0009
0.0371
48.7239
0.0000
-0.0000
0.0596
-47.7749
0.0029
-0.0029
-0.0595
47.7749
“0*0029
0. 0029
0.0595
-0.0065
0.0001
-0.0001
-0.5978
0.0080
-0.0020
0.0020
0.0966
6 ^ 1-1
L-1549
77
TABLE 8 .- Continued
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR
(h) x/H = 5.00
1.5, ? = 10.00, AND 17 = 1.00
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground
effect
>. n 1 = u •
oAMM * =
3 • l v ■ 7 n = w ■
t T A - A * L J
U t L 1
1 1
( * * Li }
tU*L> 1
“b • 4
-k, » 662 i
i 8 3 • j l 3 9
“ llu jot
- u • 0 3 o 2
“ b *uJJl,
“0 » j 3 H*
- 62 . 0 8 lb
-v • <j J VO
— w • vJi-i
Li A WH A = 1 » 2
X / H =
5 * 0 j i" / H * v •
t/H= 0 ,
•0 t A = 1,00
1 w i L )
iu»L)
i A t 0 )
1 J • J )
- u • w ]. 3 j
- u • 4 y a
-- »w522
—j .6 83 8
-J • ;
-0 * ^
-U*
— k. • j *+ > t
- w , b J « 2
-O.wlAJ
— u * U3li
■jiliiTi;
3a.., 0 1 1>/
— 'J * UH V CJ
-u • Co 04
W.4ULU
U.Liul
— C . uO j,0
C H 1 = 3 v • iw ■,
it A= IwiLt.
,/H =
3..C, : /H=
t/H= w.
l7A = hul
i . L ]
( O »L )
f W « U )
10 tD 1
-0.j379
"H'v'bb
— - tboAA
-0,03 V <
—0 , 0 6 6
-0 , Li 4 4
3 63, jibe
- v « b654
-0, 0 6b 9
— 0 * 3 J / 2
— b • i^obi
- l , 0 C 7 o
“v • i 1 ✓ E
362, Oh-31
- j • 0 6 To
— L * UOUi.
-o,03”2
L- • jCtL j
U.OUli J
“O.OQuh
- u * 6 f i 6
l_ r-t I ■ 4 3 , u u
- — A.P
*/H =
5*wl I'/m= v *
t / h - «i ■
4 i A = iiul.
1 « t L J
< 0#L )
( w » D )
t U 1 0 |
— j « j 9 2 2
-j.l947
- j • 6 8 5 V
j rt 2 , v 5 v ^
-0.0921
-l , 0 92 2
- 0,0362
-J, 092.5
-u,l.9a7
“0, 1132
3 n l » > a -j a
-0.0^37
-J. 0923
- u • C 3 8 i
-uikiUUU
0 *OOUi
-u, 00 K.
-0,5724
0, OOOL
0, U bo 1
CHI =ou. vu
u A '-AM A - 1 » 3
iti A« 10, J.J
A / H =
5,00 r /H= 0*
4/H- 0.
1 7 A= 1,00
U»«L )
<U*L )
1 M * 0 J
<U»D)
-0*2469
-v. 1426
-o,l4Sw
— 0 « 6 6b 6
-0. 142t
-J*142t
3 o 2 * / 7 *• **
-0*1424
-0.1426
-0*0382
-U.2469
-0.1426
-0.1441
-C.1137
381,5013
-0.1 44 1
-0.1426
-0.0382
0.0000
0,0001
-0,0009
-0.5725
0, uOUU
0*0001
0,0013
0,0665
CHI =75*00
GAMMA= 1.5
Z £ T A= 13,00
X/H:
5.00 Y/H = 0.
Z/H= 0.
E7A- 1.0C
IV»*L >
tU*L)
( W «D J
(OiD )
-I.C828
-0,290?
-0*2926
-0,6875
-1 .0 8 26
-0,290.
-0*2904
-0.0453
381,9237
-0.2900
-0.2902
-O.C382
-1*0828
-0,2903
-0,2516
-0.1141
Jbu.9309
-0.2916
-0.0362
0,0000
0.0001
—0 , uUL".f
-0.5734
0 • 000b
Jib 'J b 1
L- • J i j 1 .
C * 0 b J ....
CHI = 9u.0Li
GAMMA * i*5
«l£ i A- lU.JO
X/H =
5.00 Y/H* 0.
Z/H = 0 ,
£TA= 1.0C
f W # L I
tO.L f
i l'i * v )
t - » « )
-47,7711
0 , ■■ ■ 0 2 4
— J , J U 2 4
-■"'•6119
-4 7. :'36o
■:j, J002
—0 * J Ob 2
J.uJl _
4B. 7361
0.0002
— 3 • b J u 2
0*0382
-4 7. 76*47
0# 001 5
-0.0016
-0,0381
47.7647
-0.0015
0. 0015
0. G361
-0.0064
0,0005
-0,0009
-0.5736
0,0080
-0*0013
0*0013
0*0691
78
TABLE 8.- Concluded
LONGITUDINAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = AND rj = 1.00
(i) Miscellaneous additional values of x/H
8
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
\ 1
to ground effect
CHI -15.00
GAMMA- 1.5
ZETA* 10.00
X/H- 0.03 Y/H* 0.
Z/H= 0.
ETA- 1.00
(W.L )
(U.L)
tw.oi
(U.D)
-168*5075
0.3914
-171.9965
5.3403
-168.5072
0.3914
-171.9969
5.5936
179.9587
-171.9839
0.3914
83.1319
-168,5074
0*3914
-172.0033
5.5786
179,4168
-172,0033
0.3914
83.1319
-0.0001
0.0000
0,0068
-0,0381
0.0001
0,0000
0,0064
0,0150
CHI-30.00
GAMMA- 1.5
ZETA- 10.00
X/H- n,06 Y/H* 0.
Z/H- 0.
ETA* 1,00
(W.L)
IU*L )
IW.01
(U.D)
-173.0519
7.1214
-150.8490
4.0280
-173.0537
7.1214
-150.8493
4.0865
180*0648
-150.8363
7.1214
81.8403
-173,0538
7,1214
-150.8557
4,0700
1 79.5209
-150.8557
7,1214
81.8402
-0,0001
0,0000
0,0068
-0,0420
0,0001
0,0000
0,0064
0.0165
CHI-45.00
GAMMA- 1.5
ZETA* 10*00
X/H* 0.10 Y/H* 0.
Z/H* 0.
ETA- li00
(W.L)
(U.L)
(W.D)
(U.D)
-180.0463
13.2182
-125.0885
1.0887
-180.0460
13.218?
-125.0888
1.1590
180.5947
-125.0758
13.2183
77.9696
-180,0462
13.2182
-125,0952
1.1392
180.0462
-125.0952
13.2182
77.9698
-0,0002
0.0000
0.0067
-0.0504
0.0002
0.0000
0,0064
0,0198
CHI -60.00
GAMMA- 1*5
ZET A* 10.00
X/H= 0.17 Y/H* 0,
Z/H* 0.
ETA- 1.00
1 W.L J
(U.L)
( W.D )
(U.D)
-187,9307
14.6183
-91 .1887
-2.9405
-187,9303
14.6183
-91.1891
-2.8430
103.5144
-91,1761
14.6183
67.8093
-187.9306
14.6182
-91.1955
-2,8705
182.9551
-91*1955
14.6182
67.8092
-0.0002
0.0000
0.0067
-0.0701
0,0002
0,0000
0*0064
0*0275
CHI -75.00
GAMMA- 1.5
ZETA- 10,00
X/H- 0.27 Y/H- 0.
Z/H* 0,
ETA- 1,00
(W.L)
(U.L)
(W.D)
(U.D)
-129.5527
40.3139
-37.6487
1.3223
-129,5518
40,3139
-37.6490
1.4620
118,9856
-37,6362
40.3141
14,1906
-129,5523
40,3139
-37,6554
1.4227
118,4097
-37,6554
40,3139
14, 1905
-0.0004
0,0001
0,0067
-0,1004
0.0005
0.0000
0.006A
0.0393
6^T-1
l-15^9
79
80
TABLE 9.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C - 0.60, AND 7} - 1.00
(b) y/H = *0.80
L-15^9
6S
8l
TABLE 9.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1.5, C = 0*60, AND tj = 1.00
<c) y/H = ±1 .20
Correction foctors for correcting from a wind tunnel which is
to free oir to ground effect
Chl =- 3. CC CAMMA * 1 * TA = C.flQ </H= 0. Y/H = 1 . 2 r . 7/M- r. Ff ’ ■ l.C
U.l )
-C. 1*574
-C.T42 1
C.50 32
- r ♦ P ** *4 7
' i ~
- . 1 2 7
.. „ ^ ,
(C.L)
- 0 . or:-*? I
-C . C2 r 5
-C. IPO?
“ r ♦ ! r
- 0 . L ■' 7 2
U,C)
-C. 2565
-0.2151
-c.c ies
-r . j
-p.cr 12
. 1 2 C 9
L. 162'*
f L » D 1
-l.C53e
C.44^7
r.4769
r . " i c
r . 2 i 9 :
- 1 . C ’??
r . 4 r i f
CHU 3*00
GAMMA* 1.5
ZETA =
0.60
X/H = Oi
t Y/H*
1.20
Z/H* 0.
E FA* 1.00
1 W » L )
(U.t)
(WtO)
(U.D)
-0.4574
0.0091
-0.2166
-0.9318
-0.0421
0.0285
-0.1910
0.4509
0.4595
-0.0507
0.0185
0.4769
“0.2947
0.0212
-0.3555
0 .0575
0.0543
-0.3555
0.0212
0*2095
-0.1627
-0.0122
0.1387
“0,9893
0.2526
0*0072
0*1645
0*3935
CHl =15*00
GAMMA* 1*5
ZETA*
0.60
X/H = 0.
i Y/H*
1.20
Z/H= 0.
eta* 1.00
1 Wtl)
(UtL)
1 WtD)
( U * 0 }
-0.4296
0.0375
-0.1239
-0.7173
-0.0115
0.1364
-0.1316
0.4421
0.4016
0.0532
0.0656
0.4460
-0*2679
0.0996
-0.2944
0,1067
0.0052
-0.2944
0.0996
0.1609
-0.1617
-0.0621
0*1705
— 0*62t>l
0*2564
0*0367
0*1626
0.3534
CHI «30.00
GAMMA* 1.5
ZET A*
0.60
X/H = 0.
Y/H*
1.20
Z/h* o.
E'A* 1.00
(M»L 1
(UtL)
(WtD)
(UtO)
-0.3536
0.0306
-0.0039
-0.5081
0.0707
0.2383
-0.0636
0,3791
0.3602
0.1673
0. 1 308
0.3610
-0.1970
0.1621
-0.2116
0.1233
- 0 . 0101
-0.2116
0. 1621
0.1061
“0 • 1 565
-0*1315
0*2077
-0.6313
0*267 7
0*0762
0.1480
0*2556
CHI =45.00
GAMMA* 1.5
ZETA*
O.oO
X/H- 0.
Y/H=
1.20
Z/H = 0.
E1A* 1.00
(WiL)
( U * L )
( W t D )
(U.D)
-0.2551
-0.0439
0.0992
-0.3489
0.2674
0.2869
-0.0312
0.2766
0.3935
0.2392
0.1128
0.2525
-0.1173
0.1690
-0.1472
0.0976
0.0076
-0.1472
0.1690
0.0246
-0*1378
-0*2130
0* 2 4b*t
-0*4406
0*2647
0.1176
0* 1 161
0.1766
CHI-60.00
GAMMA* 1.5
ZETA*
0.60
X / H = o.
Y/H*
1.20
Z/H* 0.
ETA* 1.00
(W*L)
(UtL)
(WtO)
(0*0)
-0.1487
-0.1651
0.1777
-0.2136
0.2362
O.l6<t0
-0*0465
0.1631
0.4062
O.c 3o0
0.0391
0.1479
“0 . O 03 Q
0.1335
-0.1091
0.0579
0.0350
-0. 10 9 1
0.1335
-0,0217
-0*0637
-0*^yo6
0*2668
-0*2714
0*3012
0* 1312
0*0626
0*1055
CHI-75.00
GAMMA* 1.5
ZETA*
O.oO
X/H= o.
Y/H=
1.20
Z/H* 0.
ETA* 1.00
( W *L )
(UtL)
1 WtO)
(0*0)
-0.0137
-0.2580
0.2265
-0.0894
0.2495
0.2414
-0.0992
0.064O
0.3936
0.2261
-0.0560
0.0597
-0.0525
0.0930
-0.0876
0*0234
0.0500
-0.0878
0.0930
-0.0205
0*0369
-0*3510
0*3143
-0*1126
0*5020
0*1464
-0*0114
0*04l2
Chi -90.00
GAMMA* 1.5
ZETA*
0.60
X/H* 0.
Y/H =
1.20
Z/H* 0*
ETA* 1.00
(W»L)
(UtL)
(WtO)
(U.D)
0.1695
-0,2211
0.2211
-0.0000
0.2006
0.1604
-0.1604
0.0000
0.3315
0.1504
-0.1504
0.0000
-0*0566
0.0716
-0.0716
-0.0000
0.0586
-0.0/16
0.0716
0.0000
0*2262
-0*2927
0*2927
-0*0000
0*2595
0*0668
-0*0886
0*0000
82
TABLE 10
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y- 1.5, K = 0.70, AND tj = 1.00
(a) y/H = ±0.40
Correction foctors for correcting from o wind tunnel which is
closed
closed
on bottom
only
to free air
closed
on bottom
only
to ground effect
<U*LJ
< ft *L> }
U>'L>)
— 0 « o 3b -
— 0 « o b 1 J
-o • 76b6
— w •U341
— Ci*b4U4 — o*Covu
o*ooob
*“0 • 0400
u • 4 i 4 i
“U • 0 0 1. 3
*U»k+CO
0 * 1 b
0 • OuOb
u • i (14
-10 ■ lu\J&
CH I = Jit'w
'OMi'll'lM - 4 • J
u*Tw' a/i i*n= u«> ly
4. / h - W •
0 [ M - 1 • O w
um
(U *L )
( A 1 U )
( O t J 1
uiwjbv
-M.blV .
--•6iyy
-u* 0 1 3 / «*uj>»
0*431* ulOkJ
0 * — 400
- ^ * o 1 <L 0
^ • v y y 0
“0 * 0 14 0
-♦ 3d lb
-U • -+3 3*
-0 • oO Ob
j • 1 y 4 O
— 0 • (' 1 Vh
cm = i3ivw
OAi-iMA ~ 1.5
•j » 70 a/m- 0 • 'l/ii- 0*40
ol H- a • 00
i, v. i L J
t U »L /
(O tU )
“4* JCOt
0*3471 0*3 iwo
w • L. 1 *t /
"W SO I
y « O 1 / O
0 • j 0 V /
- 0 • 0 7 0 0
0 • 4 A 4 if
0 • 3 1 7 3
-0 * Wv v
-0 • 04‘+_-
0 • 0 3 0 1
** 0 • D 0 ( 4 !
Ch I
U h rt •• x • 'J
iLi,-
O*/- A/'.:- O • 'l'/[ = w*40
“ Y r t - u.
C. . A - *. • 0 O
( '* ♦ L )
(o »i )
(h»U)
1 1 J • w J
-o*y£3l
U • £ 3 4 l
— o • i a v 4
0 • -bow 1 • 1 1 1 b
o*41b3 — v*0i>5 1
-U • 3 344 w • *.4 J 1
0*3UVl 0 * 4 uO 4 . _
*~U »MjO>
U * i
— - ■ 40 4 1
0 • t ^ 0 ;
“0 • **04 i
utjjuf
0*1043
— 0 • 4b4o
— V * O V 4> O
CHI-43*00
umi v iWm - * • j
w » <' W A / ; -. - v * r" / r • - 'J • l i w
/ n = u *
t i A- 1*00
t w «L )
( U iL )
( *1 tO )
( U *0 )
— 0 * < 66*+
J * 1 4 3 1
o • - 4 7 o
ibl4
O • 5 i 1 3 ._ I*- 3 £ 4 . ....
0# 4 V 04 O.itHl
— 0*44.31 Jubtu
O * 4 U i / 0 ♦ 4 3 4 *.
“■ 0 * ^ 0 b b
0* bl yw
-o*<!yo4
0 * 1 d > 0
“ 0 ( titlu
0 • 3* ;u
0 • 0*35
-u*>ooy
“0* 1 7 -J'j
0*3£44
“i.*.3 Y 1 0
CHl=6o*00
iiAMMA- i*J
«-t.T a -
-*<v, o* I'/n- 0*40
i/n- 0.
i ( rt“ 1 • 0 0
{OtL t
i * * O )
<U*0>
— U ■ 0 0 0 4
03 yd
0* i V4i
“i- • 1 3 76
V*4(00 "u*4/*.>
— 0 • 3 w -•■ v - 0 • 0 4 i 3
0*4-74 _U *_i b i V
o*4 3 J*.
~ 0 • 1 > 0 0
0 * i 44^
Utwi i i
“ 0 * ivd 3
J • 4 J J-.
—0 » 5 j y 0
—w* £ >30
0 • j V 4 3
-0* 4.0 1 0
C H 1 = ( 3 , .j o
i , '
tts A =
0* i'l> X/ii= 0 ■ 1 / M* O*4'0
4 . t r, = 0 *
L 7 H- 1*00
(u • L )
— o • t>506
O • OO i O 1 • L £i J 1
-w* 1 1 14
0 • iv / 6
-0*3454
( U »L J
t *' » O )
< J »U )
“O • 504 &
0*3447
“vHJJi
U*2i.<4 «• i ^-4
0*1541
“ J • i 40 V
- * 0 J V 4.
-0*1401.
0* 1 34 i
- J* 0330
— 0 • 43t> 7
0 • 4 > 1 3
-0*i4£4
CH i = V O*0O
oaAi^m- 1*3
fct i rt-
0*7w A/f1= 0* Y /ri= 0*4v
t/rl= 0 *
£ i M = 1 • 0 0
ImL)
iU»L)
U* j )
[ Li ft 1 J )
“4 *Ov3 1
-ViS-i <
-■•51/17
0*-a*»-^ •
0*^>ob 0*-/-oJ
-J*3bbj -U*b^^4
w • Jw i/Li 4 * * u — 0
-U*lioO
0* 1 ibU
“0* i 150
u* 1 103
“ 0 • 1 i 3b
J* 1 i 30
0 * oOOO
“0*4y4o
— 0* ol 34
C ■ 0 1 34
-0 *000.0.
l-15^9
83
TABLE 10.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - « = 010 ■ '“ 1M
(b) y/H = ±0.80
Correction factors for correcting from a wind tunnel which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
'
to ground effect
— -r
{ WtL )
(U.L )
( W # 0 )
<U *0 J
-0.7939
-0.02 68
-0.5075
-0.7504
0.70
-0.1915
— 0 • 04Q3
-0.5599
0*3565
Y/H- O.oO
1 .0974
-0 . 3 7 0 b
-0,0309
0.3091
0 . 5 i 50
' -0.0353
-0.6366
0.0213
t.T A- i • U 0
0.3112
-0.6366
-0.0333
0 . 32 3 1
—0.2 7b9
0*0066
0.1291
-0.7716
0.3233
-0.0049
0.0767
0.335i_
CHI e 3.00 GAMMA= 1.5
( M t L )
<U.l)
< w . d )
(U.D >
-0.7939
0.U28B
-0*4596
-0*6210
it! A= O.?o
—0 .191 6
0.040 3
-0.6322
0*3973
if /h=’ uVfiU
0.9906
-0.3175
0.0309
0.5091
t/H = 0 •
-U . 31 30
0.0355
-0.6027
0.0662
tTA- 1.00
0.227b
-0 .6027
u. 0353
u. 3231
-0 « 2 7 tt.9
-0.0063
0.i45i
-0.7073
0 . 3 2 33
0.0049
0.0705
_0.il 13 .
CHl = 13.0d GAMMA* 1.3 2£TA-
( W i L I
( U ,L )
( W * D )
(UtD I
-C. 7498
0.1310
-0.3323
-0*4143
-0 .1363
0 • l9o 1
-0 . 442 b
0 « 4 3 b 9
Y/h= 0.
0.32 9 3
— j » i b 3 9
0. 1 4i 3
0.4623
4 / M = 0
“0 . 46 O 2
0 ■ i 646
-0* 3v02
0.1741
v. 1064
- j . 3 Ju2
J . 1 b46
J . 2732
-0.2636
-O.o337
0 . i 6 i 9
-0.3664
0.32 99
0.02 34
0.03/3
0 . 2 64b_
CHI =3u»uu
1,5
T/n= w .Po
^ / H = J •
(.,4= 1 •
< . L )
( U .L )
I W • D )
(UtD)
— U .6374
0.1876
-0.1568
-0.2563
o.olob
0.3163
-0.3179
0.4093
0 . / 2 b 2
—0 . 0 09 d
0.2)06
0* 3 433
-U. 3 J90
0.2623
-0. J344
O. 1990
0. 041 A
-o . 3644
0 * i-O*. 6
0 . A J 3 A
CHI =46.00
GAMM A = 1.3
w n ; o.
Y / n = o • <j w
( W tt. >
( U *L J
< W * U )
< U 1 0 1
-u.3196
u . 1642
0. < O l_l
-0. 2 uiw
O . \J 4 L 0
u • i 3 2 i
—0 *00 62
-0*1795
v/. 56 5 k,
-0*2336
U. 3 i3o
—
0 • i 2 o b
0.1721
0*2 lb 1
0.2633
-0.2366
0.1353
0.2635
0. 02 74
t i A= a • 0 0
CHI=60.0o
6AMMA= 1.5
iET A =
' 0.7u ~ ”
a/h= o.
Y/H* o. 8o
4/ H“ 0 •
0.3167
0 . 7 ob 1
-0.1122
0 .2 oil
—0 . lo9^
O.0893
O.0669
(UtL )
t W t 0 >
{ U ♦ D 1
-0.0176
0.1118
-o*n?3
0.3573
-0.2163
0.1998
0 . 2 1 <. 2
0.0439
0.1295
0. iOji
“0 .0374
CHI *75.00
GAMMA = 1.5
Zt7 A =
u.7o
,\7h- 0.
Y / H * 0.60
4/6!= 0.
t |H= i.OU
(WtL)
(UtL) *
( W * D )
(UtD)
-u • 394 0
-0.1971
0.2171
-0.0749
0.3637
0.3515
-u .2637
0 • o 9 4 2
0.7013
'■'"0.2614
-0.1213
0.0692
-O.Obbo
0.l3bb
-0 • i 3 i 2
O.0350
U* 06 44
-u . 1 3 12
0. 1363
-O. 0309
CHI «90.UO
GAMMA= 1*6
ZET A*
0 . 7 u
a/h^' d'
i /h* ’ 0.80
4/H= o.
fc.TA= 1*00
{WtL)
(UtL)
(W.D)
(UtD)
-0.2947
-0.3105
0.3105
—0 *00 Ou
0.3802
0.3541
-0.3541
O.QOGo
0.6602
0.2908
-0.290a
o.GuOO
-0.0927
0.1 u45
-0.1045
-0.0000
0.0927
-0.1045
0.1043
0.0000
- O . O i 4 v
“ O • J i. 60
-0.133“
0.2324
— 0 .3346
— 0 . ii 3b
-0*2207
0.2610
-0*2213
-0.3060
-0*3333
0*5462
-0. 10*95
- 0.2020
-0.4l5'0
0*4160
— O* 0000
0*0030
0*1597
U.*+309
0.1342
-0.04/1
0*1106
0.4/17
u.2136
-0. 1326
0*0392
0*4729
-0*2496
0.0000
84
TABLE 10. - Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 0.70, AND r) = 1.00
(c) y/H = ±1.20
s
Correc
tion foctors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
>d effect
1 ' 1
4
CHI =-3,00
GAMMm= i . b
ZETA
- 0 . 7u x/h = 0 , y/H
* 1.20 Z/H = 0.
ETA* 1.00
(W*L)
(U»L )
<W»D)
(U»D)
-0.3496
-o.oiae
-0.3760
-0.7956
-0.0916 0.4534
-0,0276 -0.1593
-0,2478 -0.0240
0.3615 0.4275
“0.3272
“0.0246
-0.4326
0.0266
0. 0209
“0.4326
-0.0246
0.2576
-0.Z224
0.0039
0.0567
— 0* 62 **2
0.2336
-0,0032
0.1646
0.3329
CHl = 3.00
GAMMA= 1,5
ZET A<
= 0.70 X/H= 0. Y/H:
= 1.20 Z/H = 0.
ETA= 1.00
(W.LJ
IU»L 1
( w *0 )
tu.oj
-0.5496
0.0168
-0.3447
-0.6808
-0.0916 0.4139
0.027a -0,1145
-0.2136 0.0240
0.3763 0.4275
-0.3272
0.0246
“0 « 4036
0.0726
-0.0123
-0.4036
0. 0246
0.23/6
-0,2224
-0.0059
0.0609
-0. / 533
0.2336
0 . 003*:
0.1920
0.3037
CHI =15.00
GAMMA- i.3
ZtTA =
0.<0 X/H= 0. Y/H=
: 1.20 Z/H = 0.
6TA= i.00
(U*L >
CW.D)
(U.DI
-0*5244
0.0659
-0.2642
-0.4695
-0.0567 0.3693
0*1322 -0.01/a
—0.1351 0.1126
0.3614 0.3945
-0.29/6
0. 1 lol
-0. 3 34e
0.1304
-0. O 3 O 2
-0. 3348
0.1161
0.2246
“0.2266
-Q.O 3 O 2
0.0/06
-0.6199
0.2411
0.0161
0.1997
0*2311
CHI =30. Qu
Gamma = 1.3
ZtT A =
0.70 A/H = 0. Y/n=
1.20 Z/H = 0*
ETA= 1.00
(WiL)
IU*L )
(W.D)
(U.D)
-0.4593
0.1254
-0.1543
-0.3209
0.0396 0,3716
0*2259 0.0906
—0,0460 0.1626
0.3306 0.J031
-0.2197
0.1916
“0 . 2 42 3
0.1463
-0. 0*+ f 6
-0.2423
0*1916
0 # 13 08
“0,2390
—0 .0662
0.0662
-0.**6t2
0.2395
0.0343
0*1964
0.1643
CHI =45.00
GAMMa 3 a . p
2tTrt =
0./0 X/H = 0. Y/H=
1*^0 Z/H = 0*
t T A= 1.00
(W*L)
<U«L)
(W»D)
(U.D )
-0.3693
0.0692
—0 . u56o
-0.2112
0.161** 0.4154
0.2600 0.1593
0,003w 0.1632
0.2366 0.1966
-0.1302
0.2042
-0.1726
0*1171
-0 . Oi 16
-0.1 /28
0.2042
0.03/3
“0.2591
“0.1130
0.1166
“0.3263
0.291 /
0*0336
0*1736
0.1213
CHI =60.00
GAMMA = 1,5
ZtTA =
0, iO X/H= 0. Y/H=
1.20 Z/H = 0.
ETA= l.oo
IW.L)
(U.L.1
1 W t D )
(U.D)
-0.3442
-0.0174
U . 6 301
-0.1312
0 • 26 /2 0.4668
0.2423 0.1791
-0.0016 0.1162
0.1369 0.1055
-0.0709
0*1632
-0*1326
0.0706
0. 026/
-0.1326
0.1632
- 0 . 0236
“0.2 7 32
“0 . 1623
0*1620
-0*2020
0.3381
0.0/ /I
0*1310
0.0661
CHI ■ 75.00
GAMMA= 1.5
Zt 7 A =
0.70 X/h = 0. Y/H =
l.fiO Z/H= 0.
ETA = i.OO
(W.L)
IU.L )
(W.DI
(U.D)
-0.3016
-0.1423
0.1163
-0.0682
0.3275 0.4964
0.1976 0.1583
-0.0553 u . 0093
0.052y 0.04x6
-0.0589
0.1172
-0.1102
0.0294
0.0554
“0.1102
0. 1172
-0. 0255
-0.2427
-0.2397
0.2265
-0.0896
0*3864
0.0804
0*0347
0*0233
CHI -90.00
GAMMA = i.b
Zt f A =
0./0 X/'H = 0. Y/h=
1.20 Z/H= 0.
eta= 1.00
(W.L)
(U.L)
(W»D)
(U.D)
-0.1976
-0,1893
0.1693
- 0.0000
0,3315 0,4631
0.1383 0.1115
-0.1383 -0.1115
0.0000 0.0000
-0.0696
0.0917
-0.0917
-0.0000
0. 0696
-0.0917
0.0917
0.0000
-0.1262
-0.2610
0.2610
-o.oooo
0.4011
0*0467
-0*0467
0*0000
6 +
L- 15^9
85
TABLE 11
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.80, AND rj= 1.00
(a) y/H = 10.40
Correction factors for correcting from a wind tunnel which Is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI =“3.00
GAMMA - 1.3
A C T A = 0.60 A / M —
0. i/n-
0.4U fc,/H- '-J •
LT* = 1 . 0 0
(W >L >
-1*1407
“0.6364
1 . 7 1 V 6
-0*9045
O • 03 JO
“ 0.2330
. .. 0*4063
(U.L)
“0.0333
-uiuoiv
-u .6 394
“0 .039L
-i. 0 / 7 7
0. 0053
“O.UOac
(W.D J
-0.9442
“i*046i
“0 . 0 3 3 3
-1.0777
-0 . 0390
0.1333
0* 0* >6
(U.D)
-0*5707
0.2663
0.6 G44
0 • 01 7 3
0.4694
“0 • 3o o2
0 * 2 4 90
CHI = 3.00
GAMMm= 1.3
aETA- o.Bo
a/ji= 0 . Y/n-
0 . 40 A/n - 0 •
L 1 rt= 1 . OU
(Will
-1.1407
“0 .6304
1.3032
— U . 9045
0* 6636
“0.4336
0.466 3
-
(U.L)
' C. 3555
' 0.0615'
-0.7760
0.0350
“1 . U1D4
“0.0033
0.0026
(**Ul
-0.8635
“1.0022
0.0335
“1.0264
0.0396
0.1445
0.0246
(U.D )
“u .4067
0.3374
0.6044
0. Ic70
0 • 4b 94
“0 . 3304
0.2296
-
CHI =15. Ou
GAMMA = 1.3
Ztf A = uT 60
a / n= 0 . r/h=
0.40 A/H = 0.
8TA- 1.00
( W » L 1
“i . o342
-0.3400
1.1612
-0 . 6 1 2 5
0*3667
“0. 4 . 4 1 J
0 • 4 7 30
(U.L)
0.4337
0 * iiio'j
-0.3014
0.4722
“U. 03 11
-0.0163
OiUli?
t W.D)
“0.6921
-0.6372
0.2360
“0.6311
0.2722
0.1350
0.0135
< J.D )
“U . 1646
0.4723
0.3233
0 . 4 7 6 7
0 . 4ubb
— 0 *4433
0. 1936
CHI =30.00
GAMMA= 1.5
££TA = 0.60 X/'r
■~7r. ynw*
'40 Z7FT= "07""
ETA = 1.00
( W » L )
-0.8391
“0.2855
0.920c>
“0.3802
0. 1690
“0.2569
0.2945
(UtL J
0.3791
0.4544
-o.icnTJ
0*4211
“0 . 5667
-0.0420
0 .' 0 3 3 3
(W.D)
-0.4112
“0. 3667
0 . 31.43
-0. 3b67
0.4211
0. I77p
-0.0001
(U.O)
-0. 0-229
0.4732
0.3530
0.31 5 £
0.2110
“0.3421
0.1340
CHI =45 .00
GAMMA- 1.5
Z E 7 A = ~C.SC "X7r
T7H=~
”0."40 " Z/h = G.
E7A= 1.00
(W.D
-0.6267
“0.0050
(J . 6 3 9 6
-0 * 336d
0. i 168
“0*2900
0.3387
(U.L)
0.3297
0*4696
—0.0740
ij . 4tl 84
-0.3767
-0.0767
0*0614
< W.D)
-0.1797
-0.3965
0.3393
“0.3787
0.4084
0.1990
-0*0196
tu.D)
—0 • 'j 1U4
0 • 3607
0.1306
U .4423
0. 0243
-0.232b
_ _G* 11 64_
CHI =6U.0u
GAMMA = 115
’ZETA = b'.Sb ’ X / r 1 = "0 .
r /h*
0 . 40 4/ h = 0 .
LT A = 1 .OU
( W » L )
“0.3193
0.2079
0.633b
“0 .166/
u * 1233
“0.5327
0*3946
( U.L )
0.1571
0 *4076 " ~
0.068 I
0 . 5001
“0*2349
“0.1430
0*1075
< W • 0 )
“0 .0229
-0.3C98
0.173V
-0.2349
0 » 30 01
0.2321
“0*0344
( U »D >
-0.0363
0.2166
0.063b
0.1339
“0 * 0 62 2
“0.1703
0*0649
CHI =75. OJ
GAMMA = 1.3
261 A = ’ O.eO
X/M- O'. Y/H =
O.Oo a / h = 0.
6 T A - 1.00
( W.L)
-u .3068
0 * 3 jOu
0.6 445
-«.!4lo
0.1371
“0*303U
0.4716
(U.L)
-0*U34^
0.3 / 4 3
u« i 869
v . 1990
“0 * 1693
“0.2330
0. 1733
(W.£>)
0.1002
—0.3113
-0.029^
“0.1898
0.1990
0*4697
“0.1220
(U.D)
-0.0360
0 *u996
u « 4 4 1 9
u . 03ub
“u » U432
“0.0686
. 0.0490
CHI >90.00
GAMMA= 1.5
2tT A= 0.60 X/l- =
0 . r / h=
0.40 4/ H= 0.
c T A = 1.00
(W.L)
-0.4908
0.3973
0.8494
“0.1413
0.1418
“0.5492
0*5391
(U.L)
-0.2269
0.5664
0.2384
C.1471
-0*1471
“0. 3740
0*2393
( W t D )
0.2269
“0.3664
-0.4382
-0.1471
0.1471
0.3740
“0*2393
(U.O)
-0.0000
0.0000
0.U4U0
_“U*Ou00
U • 0000
-0_.ooou
_0.0000
86
TABLE 11.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.80, AND rj = 1.00
(b) y/H =10.80
Correction factors for
correcting from
a wind tunnel
which is
closed
closed floor
open
closed
s
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
ChIc-3.00 G
i
AMMA= 1.5 ZET A = "0.50 X/H =
0. ~ 779=“ 0*30 7/ H * U*
—
' "ETA= i .00
(WtL 1
-0*7930
-0*3791
0.9660
-0.5960
0.2763
-0.1971
0*2169
(U.L J
-0*0388
-Oi'OTB"
-0.5064
-0*0418
-0. 7490
0*0030
-0*0020
(WtD)
-0.6577
-0.6691
-0*0399
-0.7490
-0.0418
0.0913
0*0900
CUtD)
-0.5318
0.2842
0*6051
0*0310
0.3972
“0*ol28
0*263*
CHI* 3.00 GAMMA* 1.5 ZET A = 0*80 X/H*
0. Y/h* 0
80 Z/H = 0*
£TA= 1*00
( W»LI
-0.7930
-0*3791
0,8599
“0.5960
0. 1901
-0.1971
0*2 lbV
( U » L )
0.0388
0*0438
-0.4535
0.0418
-0. 7074
-0*0030
0*0020
(WtD>
-0.6103
-0.6181
0.0399
-0.7074
0.0418
0*0971
0*0893
(U.D)
-0.4502
0*3392
0.5051
0.1073
0.3972
—0.667b
0*2316
CHl-15.00
GAMMA* 1.5
ZETA*
0*80
X/H* 0. Y/H-
0.80
4/H = 0*
£ T A = 1.00
!W*L)
-0.7423
-0*3184
0.7065
-0 . 5407
0.0701
“0 *2 018
0*2223
<U»L)
0 . 1 800
0.2060
-0.3155
0.1956
-0. 5886
-0*0156
0*0103
( W * D >
-0.4791
-0.5003
0.1853
-0.5866
0. 1956
0*1076
0*0863
(U»D)
-0.2472
0.4014
0.4499
0.2100
0*3407
-0*4571
0*1914
CHI-30.00
GAMMA* 1*5
ZET A*
0 . 80
X/H* 0. Y/H*
0.80
Z/H= 0.
tTA= 1.00
(WtL )
-0.6125
-0.1669
0.6210
-0.3961
0. Glo3
-0*4 i 64
0*2401
(UtL I
0.2797
0.3384
-0.1336
0*3154
-0.4188
-0*0355
0*0232
(W.DI
-0.2976
-0*3401
0.2914
— w .4166
0.3162
0.1212
v • 0 / d 7
(UtD 1
-0. 1074
0*3843
O.3O«0
U* 2394
0. 1947
“0.8466
0*1451
CHI -45. Ou
GAMMA* 1.5
ZtT A*
0*80
X/H-0* V/H*
0. 6u
4 / ri * 0 .
£TA* 1*00
(WtL 1
-0.4778
0*0376
0.6175
-0.2353
0.0344
-0.2424
0*2734
IU*U
0*2575
0*3659
0.0063
0.3237
-0.2867
— 0*06o*:
0*0422
(WtOI
-0.1471
-0*2233
0*2782
-0.2867
0.3237
0*1396
0*0633
lU.D)
-0*0599
0*2912
0*16/4
0 . 1683
0.0401
— 0*2462_
0*1029
CHI-60.00
GAMMA = T*5
“ZETA*
0*o0
X/H-0. Y / h=
0. oil
''Z7h*'-\ 0.
£TA= 1.00
-
—
(WtLI
-u.4082
0*1936
0.6441
-0.1311
0.0730
“0*2771
0*3247
(UtLI
0.1321
Ut iilii
0.08 76
0.2515
— 0*2677
“0*1194
0*0716
(Wtoi
-0*0377
-0.1751
0.1658
-0.2u77
0.2515
0*1701
0*0326
(utD>
_-_0«0490
0*1746
0.0677
0*1098
-_0. 04 3 7
-0.1588
0*0647
~ CHI *75.00
GAMMA* 1.5
ZET A =
o * BO
A/M ! \Ji i / H-
u. 8u
£ 1 A= 1 *sj u
- -
tWtL)
-0.3997
0*2846
0.6640
-0.1044
0. 0997
-0*2954
0*3890
(UtLI
-0*0347
0*4O0i
o.l 486
0.1 tic
“U. ibJ*
-0*2080
0* 1 069
(WtOI
0.O587
-0*1918
0. u iO 9
-0.1 bJ?
0* 1732
0*2227
-0*0279
(UtD)
-0.0328
0.0/49
0.0330
0 . 0437
-0.0385
-0*07bb
0.0312
TMr=90'.00 GAMMA= I *'5 ' " ZfcTA = u*Su A /H = 0* T7h= Gabo t/h = o* EfA-'TYOQ
<W*L)
-0.3648
0*3227
0.6600
-0.1128
u * 1 128
“0*2519
0*4355
fU.L )
-0,159?"
0.2590
‘ '0TT5T9
0.1370
-0.1320
-0.2912 —
0*12/0
(W.D)
0.1592
-0.2590
-0.1529
-0.1320
0.1320
0.2912
-0*1270
(UtO I
-0.0000
0.0000
0.0000
-0.
Q.
-0*0000
0*0000
6+^I-1
L-15^9
87
TABLE 11- Concluded
LAT eral distribution or interference factors for
(c) y/H = * 1.20
r = 1.5, K °- 80 ’ AN®
= 1.00
CH l *
Correction foctors for correcting from 0 wind tunnel which Is
closed
closed
on bottom
only
.00
l W # L )
( U .L )
(W.D)
(U.D )
GAMMA = 1*5
-0 * 55 18
-U*b243
— u • 649 c:
ZE TA= 0.
open
closed floor
only
((ground effect)
open
floor
only
to free air
X/H-- 0 *
Y/H 3
uooic
- 0*2067
— 0 • 0 2 ( 2
0 1‘tcOi:
L/r\- 0 *
-0*3436
-0*0 2(4
-0*4(37
0 * 0^00
t T A- 1.00
- 0 * 0 f u
-0.4/37
closed
closed
on bottom
only
1
to ground effect
— ■ ’
-0*2063
0*0051
0*0144
-u*o9oc
g* X9B 7
-0*0015
0*1935
0*2932
CHl c
3.00
GAMMA -
ZtT A = 0*oO
IWtL J
< UiL 5
(W.D)
(U*D )
-0.551b
0 * 0243
-w.4283
-0*3370
-U* 140V
0*0289
-u*2368
0 • 3 5 *+ o
Y / H = i * 1 0
□• tTA= 1*00
0.5464
-0*1620
0*0272
0. >.262
— 0 • 3456
0*0274
-0.4420
0 • QbbO
-0. 0982
-0. 4420
0*0274
0 • jiliio
-0*2063
-0*0031
0.0137
— O* 0230
0*1087
0*0013
0*2035
0 * 266b
CHl “13*00
GAMMA 3 1*»
2cTA= 0*80
(W.L)
IU.L )
(W.D)
( U.D )
-0.5258
0*1136
-0.3460
-0.3393
-0*1108
0.1371
-0*1305
0*5032
Y/H= i*^0 Z/H= 0*
ET A - 1*00
0.5x52
-0*0646
0*1 2b3
0*5904
-0.5146
0*1293
-0 * 5650
0*1301
-0. i2Q7
-0.3630
0.1295
0 * 26o2
- 0*2112
-0*0139
0*0130
-0*3094
0*2058
0*00 i 6
0*212 /
0*2150
CHl =30*00 GAMMA- 1*3
X/t-
{ M • L >
(U»L )
( W.D)
tu *0 >
-0*4589 -0*0x06
u.18.8 0.2520
Y/H = iiGf A/H^
t T A - x*00
0.5317
0 * 0 44 0
O* a 123
Q • 2 9 5 0
— 0 * 25 16
0*2165
- 0.2641
0*1662
— 0 • 09 o 9
-0 * to. i
0*1105
0 * 1 b 7 b
-0*22 (5
-0*0534
0*0252
-0* 5 7tl3
0*2210
0*0iO5
0*2153
0* 1351
CHi=43*0U GmMMA-
At 1 M- O.oo
(W.L) -0.3912
(UtLI 0*i712
(W.J) -0.1496
(O.D) -u * 1 2 7 1
0*1179
0*2619
U*007o
0*2295
t /n-
0*5911
0*1116
0*2 24 5
0 • i 7 3 0
2 / H — 0 *
-0*1535
0.2531
-0* 1925
0*1557
ETA- i • 0 <
- J* 0599
-0.1923
0*2531
0.0323
-0.2339
-0.065b
0*042o
— 0*2606
0*2352
0 * 0266
0*1999
0*0937
CHl "60.00
(W.L I
IU.L )
( 0 . 0 )
(U.D )
GAMMA- 1*3 2ETA-
-0.5630
u .u e 3b
-O.o725
-0.J739
X/H- U*
Y/H- 1*20 A/ H - 0*
0*2550
0 • 2 5 1 7
0*0122
0*1282
0 • 4 3 i 1
0.129 /
0*1642
0*0816
-o • o ( 1 1
0 • a 946
-0* 1350
0*0823
ETA- 1*00
0 • 0 1 i 9
-0 • 1350
0 , 1*40
-0.023 i
-0*2939
-0*iQ67
0.0603
-0* 1362
0*3041
0*05/1
0. 1632
0*0459
CH 1 "73*00
(W.L)
( U * L )
(W.D)
(UiD)
G f. MM A — 1.3
-0.3735
-0*0549
u * u 129
-0.-329
Z.C.TA 3 0*80
0*50 il
0 * 1 l HO
-0*0323
0.0467
Y / H= 1*20 A/H-
0. 302 1
0 • 1 o ( 9
0.0393
0 .0282
-O.OoOc
0* I40u
-0.1313
0*0331
tlA- i*Q0
0.0363
-0.1313
0 • i 4 0 o
-0*0300
— 0 * 3 1 2 3
-0*1 / 30
0 * 1444
— 0* OobO
0*3679
0*0339
0 * 0992 .
0*0113
GH I*90*0O GAMMA - -.3 At!* 3 U.eO
(W.L )
I U • L )
(WiD)
(UtD)
-0*3337
-0*1081
O.luBl
-O.oooo
0*3328
0ill07
-O* 1 107
0*0000
o •
Y/H= 1*20 4/H= o*
0*3096
0*0643
-0.064 3
U.OOOO
-0*0777
0*1119
-0.il 19
- 0*0000
ETA 3 1*00
0.0777
-0(1119
0* 1119
0(0000
-0*2361
- 0*2200
0*2200
- 0*0000
0*4104
- 0*0012
0*0012
0*0000
88
TABLE 12
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.00, AND 17 = 1.1
(a) y/H = ±0.40
Correction foctors for correcting from a wind tunnel which is
-i*403?
-0*u8 48
-1*4730
-0*3699
- 1*1 'ids
-u*0863
-1*5177
0*1991
-1 *2 979
-o.ob5e
-1*3617
0*0326
1 *0961
-1*3617
“0* 0638
0.7327
-1.4037
0*0648
-1*3934
-u* 1901
-1.1763
0*u865
-i • 44 1 7
. 0*3433
1*3363
-1 *2 807
0* 0o49
0*7793
“1*2979
~ 0*0636
“1 *4649
0*1923
0. 6446
-1 * 4649
0* 0636
0*7327
-1*2798
0*3916
-1*1336
0*0990
-1*0462
0*4006
-1 * 1907
0*3336
i • 1_12 t>
-1*026 3"
0*3920
0.6636
_-l .1690
0.39 71
-1*2320
0.4102
-0*9610
0.6079
-0.7571
0.2353
-0*7056
0*6281
-0*6205
0*3626
0.6293
-0 * 646 7
0*6082
0.3766
-0* 6401
0.6202
-0*6588
0*4700
0*2062
-0.8588
0.6202
0. 3253
-0*1 209
-0.0124
0*1017
-0*2347
-0.6317
0*5848
-0.4518
0*1925
-0*3334
0*6246
-0*5272
0*4255
-0.4910
0.6092
-0*5601
0*3600
-0.1407
-0.0244
0*1082
-0*1675
-0.4475
0.4034
-0.2629
0*0947
'■^r/H= o* 40
-0*0742
0T482T
-0.3614
0*2418
0*4043
-0.0286
-0*2731
“ fr* 4 530"
-0.3828
0.2012
-0*1744
-0*0495
0*1199
-0*1063
-0*4273
0*1940
-0*1417
0*0262
0*0562
“0.3582"
-0.2960
0*0953
0.1943
-0*0173
-0.4429
0.0273
“0*0273
- 0*0000
2ET A= 1.00
0*1267
0 * 3006
-0*3008
0* uOOO
0.7734
0*002 3
-0.0025
0 * JOOC
-0.2119
0*2231
-0*2251
- 0*0000
6+^T-l
L-15^9
TABLE
89
90
TABLE 12.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 1.00, AND r} = 1.00
(c) y/H = ±1.20
Correction foctors for correcting from a wind tunnel which Is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
[--3.00 Gj
i ' 1
AMMA- 1*5 ZE TA- i»00 X/H-
0. Y/H- x.cQ Z/H- 0*
1
ETA- ±*00
l W » L }
-0*5050
“0*4041
0*2343
-0*3492
-0.2042
—0*1506
0*1430
1 U »L }
-0*0302
-0*0314
-0*2712
-0*0311
-0.5202
0*0009
-0*0003
-0.5517
-0*3226
-0*0 J09
-0*520 2
-0*0311
-0*0315
0*19/6
( U*D >
-0.4727
0*3169
0*4578
0*0667
0* 3b 10
-0*3593
0*2322
■ 3*00
GAMMA- 1*3
ZETA- 1*00 X/rt = 0.
1 Y/h =
1*20 Z / M - 0*
ETA- 1*00
1 W»L }
-0.5050
-0*2041
0* 2 10b
-0*3492
-0*2963
-0*1366
0*1430
( U »L >
0*u3U2
0*0314
-0*2232
0*0311
-0 * 4b03
-0*0009
0*0003
( W.DI
-0*5148
—0 • 2 ?64
0*0309
— U *40 03
0.0311
-0*0343
0*2039
(U.OI
— U * 5603
0 * 34ob
0*43 1 O
0*1191
0 . jo i 0
-0*40 / 3
0*2276
-15.00
G AMMA- 1*3
ZtT A- 1*00 X/H-
0* Y/h =
1*40 Z/H = U*
ETA- 1*00
IW.L >
-0*4773
-0*1674
0*2023
-0.3164
-0.2861
-0*1609
0*1491
IU »L >
0*1432
0*1494
-0* 12U3
0* 14b0
-0 . 3006
-0*0040
0*0013
1 W*DJ
-0*4264
-0*1767
0*1467
-0.3006
0. 1400
-0*03 10
0*2120
(U*0I
-0*2084
0*3652
0*4179
0*1843
0.3401
-0*3920
O*lbO0
CHI >30*00
GAMMA- i*3
ZtT A- 1*00 X/H-
0. Y/H-
1*40 4/ h - 0*
ETA- 1*00
( M *L )
-0*4033
-0*0632
0*2530
-0.2200
-0*2103
-0*1/33
0*1620
1 U *L )
0*2406
0*2546
-0*0065
0*2518
-0*2624
-0*0110
0*0026
IW»OI
-0*3169
-0*0677
0*2463
-0*2824
0*2310
-0*0364
0*214/
*
1 U *D )
-G *0902
0*3236
0*3076
0*1974
0.2270
-0*2075
0*1262
CHI =45.00
(jAMMA= 1*3
ZET A-
1.00
A/H- 0 1
i Y/H-
1*20
2/H- 0*
ETA- 1*00
(W.L 1
(U *L )
iW.O)
IU*0I
-0.3267
0*2616
-0*2396
-0*0347
0*0657
0*2063
-0*0043
0*2339
0*3422
0*0576
0*4742
0* iovb
-0*1237
0*2824
-0*2126
0.1303
-0.1102
-0 . 4 1 2 o
0. 4044
O.Ouo i
-0*2030
-0*0tU i
-0*04/0
-0* i > ji
0*1893
0*004i
0*2001
0*0755
CHl >60*00
GAMMA- 1.5
ZtT A-
1*00
X/H- Ot
» Y/H-
1*20
Z/H = 0*
ETA- 1*00
{ W *L )
(UtLl
(4.01
(U»D)
-0*3029
0*2049
-0*1651
-0*0090
0*1617
0*2466
0*0050
0*1306
0.4314
0.0715
0*2218
0*0605
-0.0540
0*2434
-0.1817
0*1002
-0. 0227
-0.1817
0. 2434
-0. 0180
-0*2409
-0*0304
-0*0034
-0*1091
0*453 /
0*0032
0* 1067
0*0306
CHI >75*00
GAMMA= 1*5
ZETA-
1*00
X/H- 0.
i Y/H-
1*40
Z/H- 0*
ETA- 1*00
IW.L 1
(U»L >
(W.D)
" { U »D >
-0*3548
0*1062
-0.1222
0*0028
0*2550
0*1720
-0*0293
0*0456
0*4917
0*0467
0*1199
0*0121
-0.0501
0.1822
-0.1602
0.0450
0.0432
-0. 1682
0.1622
-0.0374
-0*3047
“0*0739
0*0461
-0*0422
0*3051
-0*0102
0*1389
0*0000
CHI-90.00
GAMMA- 1.3
ZETA-
1*00
X/H- Oi
, Y/H-
1*40
Z/H- 0.
ETA- 1.00
(W»L>
(U.L >
(W.DI
1 U *D |
-0*3926
0*0272
-0*0272
-0*0000
0*2064
0*0944
-0*0944
0*0000
0*3123
0*0025
-0*0025
0*0000
— 0 .0020
0.1503
-0*1505
-0*0000
0*0026
-0. 1505
0* 1505
0*0000
-0*3100
“0*1233
0*1233
-0*0000
0*3690
-0*0361
0*0561
" o»odoo
6^1-1
L- 15^9
91
TABLE 13
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y * 1.5, ? = 1.50, AND tj <* 1.00
(a) y/H = 10.40
Correction factors for correcting from a wind tunnel which Is
8
closed
closed
on bottom
■ only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground
effect
CHI— 3.00
i ' 1
GAMMA = 1.3 ZtTA = 1.30 a/H= 0. ’ Y'7m=~
0.40 Z/N* 0.
1TA = 1.00
( W *L )
-2.2613
-2.192V
*•8290
-2.22B3
i. 1932
-0.0332
0.0334
<U*L )
-0.1545
-O. 1546
— 2 * 6 446
-0.1546
-2.7767
0.0001
-0.0000
I W • 0 )
-2.7312
-2. 7327
— C . 1 544
-2.7767
-0.1546
J . 0453
0.0440
( U * D )
-0.1627
0 . 20 BV
1.4526
U * 1 0 3 5
1.4402
— 0 . 2 662
0.10^3
CHI- 3.00
Gamma * 1.5
Z E T A = 1,50 X/H =
o." '
i 40 Z/H s 0 .
ETA= 1. 00
( W * L ) '
-2.261 5
-2.192V
1 .4739
-2.2263
o,b315
-o,u332
iU.L)
0.1545
0.1546
-2 .492 3
0.1 346
-2.6236
-o.uoui
w. 0000
{ W • 0 >
-2.3798
-2 ,3B 13
0.1 544
—2 .6256
0.1 346
0.0439
0. 0442
(0*0)
y • 1466
0.4B16
1 .4526
0.3666
1*4402
“0. *400
0*09 49
CHI -15.00
GAMMA= 1.5
Z E T A * 1,50 X/N*
0. Y/h*
0.40 = 0.
c i A* 1 . uO
IWtl)
-2.0539
-1.9631
U .963 7
-2.0196
o , 3645
-u.0342
_0» 0363
(U.L )
0.7209
0.7216
-2,0430
u.7216
-2,1764
-0*0007
O.Oool
tW.D)
— 2 .1316
-2 , 1 34y
0 . / 2 u 3
-2.1764
0 . 72 1 o
U • 0466
0*0444
(UtD 1
0.5746
0,6430
1.2436
____ _ 0 , 7 666
1.2306
-0.1940
0*y_/&4
CHI -30.00
GAMMA- 1.3
ZtT A= 1,50 A / H =
6* Y/H=
0,40 L/ri- o ,
L T A= 1,00
( W » L 1
-1.3133
-1,4330
0.6966
-1.4754
0. 1220
-0.0379
0*0404
(U.L)
1.1349
1 , 1 36V
-1.4123
1.1563
-1.5494
-o.ooi f
0*0004
(W.D)
-1.5021
-1 .5050
1.1536
-1 , 5494
1. 1563
0.04/3
0*0444
( U * D )
0.7322
0.9337
0.7063
0.6773
0. 6941
“0.1451
0 ♦ 0364
CHI =45 ■ 00
GAMMA- 1*5
ZtT A = *.5U X / H =
0. Y/H=
0.40 2/H- 0.
t_ T A = 1.0 0
( W *L )
-0.9206
—0 . 62 66
0.7125
-0.8752
0.1 366
-0.043m
(U.L )
1.1752
1.1795
-0.9140
1.1 766
-1*0617
-0.0034
0*0006
( W »D)
-1.0035
-1.0079
1.1729
-1.0517
1.1 7 o 5
0*0463
0*0436
(U »D )
0.5653
0.7263
0.1301
0,6677
0.1333
“0*102.3
0 ttLihh
CHI =60. Ou
GAMMA= 1.3 ZtIA=
1.60 A / H —
0. Y/H*
0.40 *./h = 0 .
t TA= 1.00
1 4 » L )
-0.5469
-0.4229
0.6177
-0.46B2
0. 2622
-0.06UO
(U.L )
0*9006
0.9104
-0.6160
0.9066
-0.7539
-0.0079
0.0016
( in »D I
-0.7037
-0.7118
0.6957
-0.7539
0 . 90 Bo
0*0302
0 * 04*. 1
( U * D )
0.3349
0.4199
-0.1421
0.3961
-0. 1627
-0.063*;
0*. 021.6. _
CHI =75.00
GAMMA- 1.5 Zc.T A =
1.30 X/M=
0. Y/H* 0.40
Z/i-i- 0.
t TA= 1*00
< W *L )
-0.4776
—0 *2837
0.8682
-0.36 3 7
0. 5694
-0.0919
0.1020
(U.L)
0.5981
0.6261
-0.452V
0.62*4
-0. 3893
-0*0242
0.0036
(W»[>)
-0*5330
—0*5539
0*3840
-0.3b 95
0.6224
0*0363
0*0336
(U»D)
0.1305
0.1634
-0.1131
0.1573
-0.1387
-0*0266
0±G06i
CHI =90.00
GAMM A = 1.3
ZET A= 1.50
A/H= 0* Y/h»
0.40 i/H s 0.
t I A= 1*00
( M*L)
-0.5359
-0.2436
0.9121
-0 « 4 1 1 4
0.411m
-0.1245
0*1657
(U»L J
U.393I
0* 4632
-0. J*.i i
U .M
-0.4/*0
“0*0/69
-O.OOoo
1M*D)
-0.3931
-0.4OJ*
0.5411
-0.47*0
0.47*0
0.0/65
U.GObe
10*0)
-O.OOOL
6.0006-
0*0 00 L
-O.OUOO
0*0000
-0*0000
0*0000
92
TABLE 13.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.50, AND tj = 1.00
(b) y/H = ±0.80
Correction factors for correcting from a wind tunnel which is
closed
ctosed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground
1 T
effect
CHI *-3.00
GAMMA* 1.5
ZET A*
1.50 X 0.
Y/h*
0.60 Z/H* 0.
ETA* 1.00
(W tL >
-U.8299
-0.7417
-0.0055
-U.7856
— U • 6395
-0.0442
0.0439
(U »L )
-0*0700
-0.0700
-1.0208
-0*o7ou
-1.1706
0.0001
0*0001
( W *0 )
-1.1580
-1.0865
-0.0698
-1*1705
-0.0700
0.0125
0*0850
(U.D)
-0.1477
0.2814
0.6740
_0. 1.500
0.8572
-0.2977
0*1314 _
CHI* 3*00
GAMMA* 1.5
ZET A*
' 1.50 a/H* 0.
i T7h»
U.8l- t/M* u •
1 1 A= 1 . i/U
( W *L )
-0.8298
-0.7417
-0.0462
-0.7856
-0.6666
-0.0442
Q.*04i9_
( U » L )
G » u 7 O 0 "
0.0700 '
-0*9292
0.0700
-1 ■ 0806
-0.0001
-0.0001
( W »D )
-1.U685
-0*9947
0.0698
-1.0806
0.0700
0 .0 122
0.0659
( U *D )
-0.0002
0.3862
0.6740
0.2680
0.8572
-0.2682
0.1182
CH 1=15.00
GAMMA ■ 1.5
ZET A-
i.30
X/ri = 5^
, Tjn= 0.60
Z/h* 0 •
ETA- i.00
( w.L )
-0.7576
-0.6667
-0*04/2
-0.7120
-0. 6438
“0 . 0436
0*0453
(U*L )
0.3327
0.3326
-0.7205
0.3331 “
-0.8744
-0*0004
-0.00O3
( W *D )
-0.8625
-0 . 7 b 7 2
0.3318
-0.8744
0.3331
0.0119
0.0872
(UtO)
0.1986
0.3093
0. / 62 4
0.4148
0.7651
-0.2162
0*0946
CHl -30.00
GAMMA* i.5
‘ ZET A -
'1.50
X/H= Oi
, y/h= or&o
Z/H = 0.
ETA* 1.00
( W » L 1
—0.5634
—0 . 46^9
0.0798
-0.5130
-0.4916
-0.0304
Q.GsOi
( U *L J
0*5657
0 .5658
-0.4797
0 . 3665
-0.6355
-0.0006
-U.0007
(W.D)
-0.6235
—0 . 5476
0.5636
-0.6353
0. 3663
0*0121
0.06/9
(U.D)
0.2836
0 • 5127
0.5296
0.4440
0* 3106
“O.loijH
0*0666
CHI-45.00
GAMMA* 1.5
ZE7"A =
X/H*
, — y/h- o.eo
“Z7 H* 0.
ETA* 1.00
| W *L )
-0.3387
-0.2184
0.2836
-0.2764
“0. 2639
-0.0603
0.0600
(U »l )
0.6337
0.63*1
-0.322T" '
0.6355
-0.4784
-0*0016
-0.0014
( W »D }
-0 ■ 4653
-o.iyio
0.6294
—0 • 47 b4
0.6355
0.0131
0.06 / 4
(U.D)
0.2453
0 • 40 1 6
0.2168
0*3565
0.1951
-0*1112
0*0451
CHI *60.00
GAMMA* 1.5
ZETA* 1.50 X/h=
Q~, Y7H-
”0T60 Z/h* 0.
ETA= 1.00
( W *L I
-0.2014
-0.0414
0.4782
-0.1215
-0.0510
-0.0799
0.0601
(U*L I
0.5434
0.544?
-0.2539
0.5476
-0.4088
-0.0042
“0.0031
(WtD)
—0.3927
-0.3241
0.5339
-0.4086
0* 5476
0.0161
0.0847
(U.D)
U • 1595
0.2481
-0.0145
0.2254
-0.0405
-0.0659
0.0227
CHI-75.O0
GAMMA* 1.5
ZET A* 1.50 ' X/H*
o'. y/h=
0.80 Z/H* 0*
ETA* 1.00
{ WtL )
-0.2319
0.0097
0.6059
-0.1127
0.0973
-0.1192
0.1224
tU.L )
0.3952
0.4009
-0.2296
0.4099
-0.3/85
-0.0147
-0*0095
( W .0 )
-0.3525
-0.303 / .
0.3699
-0.3783
0.4099
0*0260
0.0748
(U.D)
0.0765
0.1041
-0*0572
0.1013
-0.0840
-0.0248
0.0029
Chi * 90.00
GAMMA* 1.5
ZETA* 1.50 X/H=
0. Y/H-
0.80 2/H- 0.
ETA* 1.00
( WtL )
(U*L)
(WtD)
(U.D)
-0.3452
0.2822
-0.2822
-0.0000
0.0045
0.2970
-0.2970
0.0000
0.6670
-0.2081
0*2081
0.0000
-0.1859
0.3387
-0.3387
-0.0000
0. 1859
-0.3387
0.3387
0.0000
-0.1593
-0.0564
0.0564
-o.uooo
0.1903
-0.0416
0.0416
0 • 0000.
L-15^9
93
TABLE 13. - Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 1-50, AND ij = 1.00
(c) y/H = *1.20
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
1
CHI =“3*00
OAMMA- 1.5
2LTA-
1.50
>;/H= 0.
Y/H- 1.20
Z/H- 0.
ETA- 1.00
rw.u
(U#L)
(W*D)
ru»D)
-0.3430
-0.0347
-0.5783
-0.1972
-0.0344
-0 i 3494
-0.1104
-0.3189
-0.0343
-0.2701
-0.0346
-0.5184
-0. 7620
-0.5184
-0.0346
-0.07/9
-0.0000
-0,0596
0.15/29
0.0002
0.1690
-0.2278
Oi 33 74
0.5415
0.1425
0.5101
-0. 5 7 03
0.1950
CHI- 3.00
GAMMA- x.S
2ETA-
1.50
/. /H = 0.
Y/H- 1.20
Z/H - 0.
ETA- 1.00
(W.L)
(U.L)
(W*D)
<U»U)
-0.3480
0.0347
-0.526V
-0. 1394
-0.1972
0.0344
-0.2930
0. 5042
-0.1099
-0.2621
0.0343
0.5415
-0.2701
0.0346
-0.4650
0*1940
-0. 7470
-0.4650
0.0346
0.5101
-0.0779
0.0000
-0.0619
-0.3334
‘ 0.0729“
-0.0002
0.1720
0*1/52
CHI -13.00
GAMMA- 1.5
ZtlA =
1 .30
A/H- 0.
Y/H- l.cQ
Z/H= 0.
ETA- 1.00
{ W * L )
{U.L)
(W.D)
(U.D)
-0.3154
0.1659
-0.4198
-0.0173
-0.1599
0.1646
-0.1792
0.3891
-0.0691
-0.1477
0.1642
0.4979
-0.2351
0.1657
-0.3552
0.2501
-0. 6806
-0.3552
, 0. 1657
0.4657
-0 . OoOi
0.0002
-0.0b4 /
— 0 • 26 74
0.0752
-0*0011
0*1760
0*1391
CHI-30.00
GAMMA- i.5
2ETA-
1.50
X/H= 0.
Y/H- i.20
Z/h = 0.
fc T A- i.OO
<W*L)
{U.L )
( W *D )
(UtO)
-0.2278
0.2883
-U .3090
0.0491
-0.0565
0.2851
—0 . 0649
0.5451
0.045 1
-0.0329
0.2841
0.5 743
-0.1 393
0.2877
-0*2432
0.2446
-0.5393
“0.2432
0.2877
0.5594
-0.0665
O.OOOo
-0.0659
-0.1955
0.0626
-0.Q02O
0 »1 762
0.0965
~~CHl =45.00
GAMMA- 1.5
ZETA-
1.50
A/H= 0.
Y/K= 1.40
Z/ H — U.
bTA- 1.00
(W»L)
(U.L >
( W » D )
(U.D)
-0.1287
0.3368
-0.2513
U.U562
0.074V
0.3304
-0.0099
0.2482
0.1982
0.0226
0.3282
0.2096
-0.0236
0.3356
-0.1871
0.1873
-0. 3023
-0.1871
0. 3356
0.1711
-0.1032
0.0012
-0.0641
-0.1511
0.0965
“0t0055
0*1772
0.0610
CHI-60.00
GAMMA- 1.5
2ETA-
1.50
A/H- 0.
Y/N* 1.20
Z/H= C.
ETA- 1.00
< W.L )
(U.L)
( W . 0 )
■ “* (U.D)
-0.0817
0. 3088
-0.2455
0.0463
0.1842
0.2 946
-0.0160
0.1432
0.3464
0. 0 1 5 1
0.2897
0.0612
0.0555
0.5064
-0.1885
0*1176
-0. 1913
-0. 108 5
0.2064
0.0165
“0.1372
0.0024
-0.0564
-0*0715
0*1267
-0.0116
0*1706
0*0254
CHI-75.00
GAMMA- 1.5
ZtT A =
1.50
A/H = 0«
, Y/H- 1.20
Z/H = 0.
ETA- 1.00
1 W.L )
{U.L I
(W.DI
IU.D)
-0.1510
0.2460
-0.2496
0.0369
0.2324
0.2103
-0.0644
0.0549
0.4522
-0.0297
0.1964
-0.0062
0.0458
0*2433
-0*2141
0.0579
-0.0598
-0.2141
0.2433
-0.0425
-0.1968
0.0027
-0.0354
-0.0210
0.1866
-0.0330
0*1498
-0*0030
CHI -90.00
GAMMA- 1.5
ZETA =
1.50
X/H = 0«
i Y/H- 1 . 2 O
Z/H- 0.
LTA- 1.00
(W.L)
(U.L)
(W.D)
(U.D)
-0.2854
0,2037
-0.2037
-0.0000
0.2344
0 . 1226
-0.1228
0.0000
0.5027
-0.0814
0.0814
0.0000
-0.0312
0.2206
-0.2206
-0.0000
0.0312
— Q • £ 2 Q b
0.2206
0.0000
“0.2342
-0.0169
0.0169
-0.0000
0.2655
-0.09/ 7
0.0977
0.0000
TABLE 14
9k
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 2.00, AND = 1.00
(a) y/H = ±0.40
s
Correction foctors for correcting from
a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
to ground effect
CHI *-3.00
—
■ 1 — —
b A Wi A * i .3 AtIA* t.ou X/H- o. y/H*
0.40 Z/H * '04
tTA* l.oo
( W » L 1
-2 • 87b7
—2 .8464
1.0405
-2.6619
0 • 42 bO
-0.014a
0.0133
1 U » L )
-0.2122
-0.2T73
-3 .642 1
-0 • 2 1 23
-3.7424
0.0000
U.OOOQ
—
{ W.O 1
-3*7121
-3.7052
-0.2122
-3.7424
-0.2123
0.0303
0.0372
—
(U.D 1
0.0293
0.3063
2.161b
0.2270
2.1765
-0.1977
0.0793
CHi*
3.00
GAMMA* I • 5 “ZT00 X/fl* 0, Y/H* 0.40 Z7R*”1T. "ETA* I, 00
I W » L )
(U.L)
< W»D }
(U.D)
-2.8767
0 . 212 Z
-3.4839
0.4292
-2.6464
0.7147
-2.6619
0*1105
“O.Ui 4C
0.0133
■0.2123“
-3.4134
— S^.2123
-3.5143
- w . 0000
-O.uuOG
-3.4770
0.2122
-3*5143
0.2123
0.0304
0.0373
0.6769
2.1618
0.6073
2.1763
-0.1761
C. 0 7 lb
CHI *15 .00
GAMMA* 1.3 ZETA = X.0'0 X/H = 0. Y/h* 0.40 A/H« U. TA— I.UU
I W * L |
{ U * L )
(M.D)
( U .0 )
-2.6195
0.9907
-2.8736
0.9666
-2 .5682
0.3185
-2 . 6042
— u • 26 7 6
0.99E6
-2.6023
0.9966
-2 . 9042
-2*6667
0.9984
-2.9042
0.9986
1 . 16B0
1.8970
1.1104
1.6916
-0 .01 32
-0.0002
0.03 Ob
-0.1439
UlUlOU
-0 • UUOO
u.03 io
0.U3 id
Chi *30.00
GAMMA- 1.5 ZET A- ~ <..00 X/H* 0* 7/h= 0.40 " Z/H* 0. ETA- i * Q Q
(W*L)
IU pL I
<M.O)
(U.D l
-1.9371
1.6404
-2.u679
1.1431
-1.9024 0.2 b44
I .6407 " -i .9964
-2.0611 1 • b 39b
1.2935 1.1444
-1.9202
1.640b
-2.0987
1 .250o
“0 . 30 32
-2.0987
1.6406
1.1384
■0.0169
•0*0004
0*0307
■0.10/7
0.0178
-u.ooor
0.03/6
0.0**2V
CHT-45.00
GAMMA= i.5 ZET A= 2.00 X/H*"15'. f/H* 0.40 Z7H* "C." ETA= 1.00
(W.L I
( U ♦ L )
(W.D)
(U.D)
-1.1614
-1.1194
0.3137
-1.1409
-0.037b
1.7352
1.7335T
-1.3815
1.7361
-1*4641
-1.4532
-1.4466
1.7337
-1.4641
1.7361
0.9221
1.0260
0.3040
0.9904
0*2968
-0.0203
-Q.0Q09
0.0310
“0.0763
0.0213
- 0.0002
0.0375
0.0 29b
*60.00
GAMMA* 1.3
ZET A= 2.00 X/H =
0. Y/H*
O.hO Z/H* U.
lTA= 1.00
( to.L 1
-0.6541
-0.5963
0.8136
-0.6261
U* 2773
-0.0260
0.0296
IU.L }
1.3910
1.3926
-1.0231
1 . 3931
-1. 1256
-0.0021
-6.0005
( W.D)
-1.0943
— i .0867
1.3673
-1.123c
1 . 3931
0.0315
0.0371
(U.D)
0.5519
0.6167
'-0.1993
0.3995
-0. c087
-0.0476
. 0*0172
CHI "73.00
GAMMA* 1*5
ZETA= 2.00 X,
X
>-
o
X
0*40 Z/H * 0.
ETA* l.Qt
<*.L )
-0.5614
-0.4649
1.0063
-0.5149
0.4863
(U.L )
0.9749
0.98Q9
-0.6228
0.9626
-0*9249
(W.O |
-0.0914
-0.8898
0.9637
-0.9249
0.9626
(U.QI
0.226 6
0.2520
-0.2016
0 . t469
-0.2145
—0 .0463 0.0499
-0.0077 -0.0018
0.0335 0.0351
-0*0202 0.0051
1*90.00
GAMMA* 1,5
Z.ETA* 2.00 X/H*
0. Y/H*
0.40 Z/H* 0.
ETA* 1.00
< W *L )
-0,6741
-0.4967
1.0994
-0.5961
0.5961
-0.0779
0.0994
(U.L)
0.7193
0.7426
—0.6664
0.7643
-0. 7643
“0*043i
-Q. 0216
< W.D)
-0.7193
-0.7426
0.6664
—0 .7643
0. 7643
0.0451
0.0218
(U.D)
-0.0000
-0.0000
0.0000
-0.0000
0.0000
- -O.*ftQQ0
0*0000
6l£ T-1
L-15^9
95
TABLE 14.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, C = 2.00, AND t,= 1-00
s
Correction factors for correcting from a wind tunnel
which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
— ■
to free air
to ground effect
CHI— 3*00 GAMMA * 1.5
I W.L J
(UiL )
(W.D)
( U * D )
-0*7007
-0.0765
-1.1689
0.0392
2*00
-0.6583
-0.0765
-1.1224
0.3653
Y/H* 0.80
-1.0760
-0.0764
1.07 90
2/H = 0.
-0.6793 _
-6.’ 0765
-1.1922
0.2631
ETA* 1.00
-1.4010
-1.1922
-0.0765
l. 0714
-0.0213
-0.0000
0.0033
-0.2240
Q.0210_
0.0001
0.0698
_0* 102 2
CHI « 3.00 GAMMA- 1.5 2t(A*
(W.L )
(U.L >
(W.O)
( U . D )
-0.7007
0.0765
-1 .0768
0.1805
2.00
-0.6583
0.0765
-1.0096
0.4741
Y/H = 0.80
-0.7551
-0.9629
0.0764
1.0790
2 / H = 0
-0.6793
0.0765
-1.0799
0.3822 .
ETA* 1.00
-1.3823
-1.0799
0.0765
1.0714
-0.0213
0.0000
0.0031
-0.2017
0.0 210
- 0.0001
0.0703
(W.L)
(U.L )
(W.D)
(U.D)
CHI =13.00
GAMMA* 1.3
AtT A*
2 . UO
X/H= 0 . Y/h* 0*80
(W.L)
— G .6242
-0 • 36GP
-0*0363
(U.L)
U.3658
0.3053
-0. 7230
(W.D)
-0 .8403
— 0 • 7 722
0.3632
(U.D)
U.3537
0*5920
0*9803
CHI =30. Gu
GAMMA* 1.3
2ttA*
c.uG
a'H= 0. Y/H* 0*80
t W.L )
-0.4164
-0*^6 79
— 0. 3994
(U.L )
0*6327
0*6319
-0.4749
(W.D)
-0*5912
-0*5224
0.0312
(U.D)
U • 40 U 5
0*3737
0.7 024
CHI =43. UU
GAMMA* 1.3 '
ZET A *
c • UO
X/H* 0. Y/H* 0. 8 0
( W*L )
-0.1693
-0*1109
-0.0626
(U.L)
0.7323
0* vsdb
-0.3387
(W.D)
-0.4552
—0 . 386o
0.7292
(U.D)
0.3225
G*443b
0.3366
CHI =6U.Gu
GmMMa* 1.3
LC. 1 M =
£ . (JO
A / M= u » I / M= U.dU
-0.0106
0.6602
-0.4340
0.2081
0.0691
0.6567
-0*3670
-0.318a"
0.6 530
0. 02*: 8
Z/H = 0 .
—0.6022
0* 3658
-0.8432
0.5185 _
-0. 3V20
0 • b 326
-0.3938
0.62 1b
i/H = u
-0.1 400
0.7322'
-0.4381
0.4072
0.0294
C • 6 o 0 0
-0.4377
0.2392
Ol
o
o
GAMMA* 1.5“'
2ETA* ‘"7100"
(W.L)
-0 *o52 0
0* 3791
(U.L)
0.5157
UT5C 64 _ "
(W.D)
-0.4560
-0*3962
(U.D 1
0.1055
0.1261_
[=90.00
GAMMA* 1.5
2ETA* 2.00 ~
(W.L)
-0.2352
-0.0052
(U.L)
0*4302
0.4C36'
1 W.D)
-0.4302
-0 • 4036
(U.D)
-0 *0000
-O.OGGu
0.4940
-0.0800
" "ZTTi* 0.
O.Ui j6
"“"O’.' 51 66
-0.4634
0.1247
XV H* 0.
0.6319
-0.349B”
0.549a
0 * 0000
-0.127a
u .4347
-0.454?
-0.0000
ETA* 1.00
-1.2639
-0.8432
0.3658
V* 9 l cl
ETA- 1.00
-0.9862
-0.393a
0.632b
0.6938
ETA* 1.00
0.1278
-0 ."4547
G . 4347
0.0000
- 0.0220
0.0000
0.0028
— 0* 162 6
-0.0244
0.0001 ’
0.0027
-0.1211
0.0217
” -0*0003
0*0710
0*07 17 _
0*0 241
-0. 0007
0*0714
0*0541
c 1 A= 1.00
-0.6312
-0.0295
0*0291
-0.4581
C .0001
-0.0014
0. 7322
0.00*9
0*0713
0.3265
-0.0847
_ C.0363
L • M= 1 IWU
-0.2919
-0.0402
0*0397
-0.4377
C.00S2
-0.0CTJ3
0 . o60u
0.0037
0*0707
0. 0098
-0*05 1_1
0*0198
-
ETA* i *uO
-0.0394
-0.0o3o
0* U 0 30
-0 . 4634
-0.0009
-0*0102
0.3166
0.0074
0* 067 2
-0.0^62
-0.0192
0*0034
“ 0*1074
-020245
0*0245
- 0*0000
0*1227
-752 049 T
0*0491
0*0000
96
TABLE 14.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND tj = 1.00
(c) y/H = ±1 .20
s
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
i i i r~ -
to grour
id effect
CHI--3.00
GAMMA- 1.5
ZETA*
2*00
X/H= 0. Y/H- 1.20
0.
t TA= 1.00
<W*L)
<U*L )
1 W*D)
IU»0l
-0.2244
-0.0353
-0.5223
-0 *u71d
-0.1429
“0.0350
-0.3254
0.3/14
-0.3464
-0*3034
-0.0350
O.y'jii
-0.1825
-0.0352
-0*4646
0 . 2 1 3 7
-1.0575
-0.4646
-Q.C35c
0.5757
-0.0419
-0.0001
-0.05 /b
-0.2855
0*0396
0*0002
0*1392
0*15/7
CHI = 3«0<J
GAMMA= i . 5
ZETA =
2*00
X/H= Q, Y/H* 1.20
Z/H = 0.
ETA= 1.00
' - _
i M f L )
IU.L)
I W *0 1
1U*0I
“0.2244
0 • w 3 5 3
-0.4331
0.U024
-0 • 142*
0*0350
— 0 • 2653
0*4009
-0.3346
-0.2415
0.0550
0.5911
“0.1625
0.0352
-0.4042
0.2592
-1.0321
-0. 4042
0. 0352
0.5757
“0.0419
0.0001
-0*0389
-0.2565
0*0396
-0*0002
0*1407
0*1417
CHI =15.00
GAMMA- i,o
ZETA-
2*00
X/H= 0. Y/H= 1.^0
Z/H = 0.
ETA= i .00
( W »L )
1 U * L )
( W *U I
(U.OI
-0.1886
0.1691
-0.3459
0.0946
-0.1046
0*1677
-0*1427
0.4140
-0.2723
-0.1204
0.1676
0.5472
-0.1454
0.1666
-0.2854
0*3009
-0.9453
-0.2854
0. 1666
0.5314
-0.0432
0.0005
-0.0605
-0.2063
0*0408
-0*0009
0*1426
0*1130
Chi =30.00
GAMMA = i.5
ZETA-
4.00
X/H= C. Y/H= 1*20
Z/h = 0.
ETA= 1.00
-
( W » L )
<U»L)
IWfOl
( U » D )
-0 .0905
0.2951
-0*2322
0.1235
0.0025
0.2918
-0.0266
0.3571
-0.1305
-0.0041
0*2915
0.4219
-0.0427
0.2939
-0.1707
0.2755
-0.7774
-0.1707
0*2939
0.404 (
-0.0478
0.0013
-0.0614
“0.1520
0*0452
-0*0020
0*1442
0*0616
CHI =43.00
GAMMA- i,o
ZtT A-
4.00
X/H= 0. Y/H= i.cQ
Z/H = 0*
ETA= 1.00
(W.L)
IU.UI
(WtOI
IU»0)
0.0278
0.3482
-0.1839
0*0956
0.1396
0.3414
0.0216
0.2522
0.0524
0.0442
0.3407
0.2508
0.0853
0.3456
-0.1226
0.1992
-0.5711
-0. 1226
0.3456
0.2308
“0.0575
0.0026
-0.0612
-0.1036
0*0543
-0*0042
0*1442
0.052V
CHI =60.00
GAMMA- 1.5
ZtT A =
4.00
X/n= 0. Y/H= 1.20
Z/rt = o*
t TA= 1,00
(W*L)
(U.Ll
(W*Q)
(U.D)
0.1034
0.3251
-0.2051
0.0589
0.2536
0.3099
-0.0043
0.1425
0.2336
0.0185
0.3082
U .0844
0.1806
0*3194
-0.1463
0.1173
-0.3667
-0.1463
0.3194
0.0602
-0*0/ / 2
0.0057
-0.0568
-0.0584
0*0 750
-0*0095
0*1420
0*0253
CHI-75.00
GAMMA- 1.5
ZET A =
4.00
X/H= 0. Y/H* 1.20
Z/H = 0.
ETA= 1.00
(WtL >
<U.L >
IW.D)
(U.D)
0.0557
0.2708
-0.2587
0.0413
0.2911
0.2283
-0.0763
0.0578
0.3740 0*1766
-0.0530 0.2564
0.2226 -0.2092
-0.0087 0.0580
-0. 1989
-0.2092
0.2564
“0.0343
-0.1208
0.0145
-0.Q495
-0.0167
0*1145
-0*0260
0*1330
-0*0002
CHI-90.00
GAMMA- 1.5
ZET A =
4.00 X/H = o. Y/H= 1*20
Z/H* 0.
ETA= 1.00
—
~ ( WiL >
(U.L 1
IW*0J
”'IU*D>
-0.1159
0.2671
-0.26/1
-0.0000
0*2608
0.1501
—0 • 1 3 0 1
0*0000
0.4563 0.0706
-0.1239 0.2505
0.1239 -0.2505
0.0000 -0.0000
-0.0706
-0.2505
0. 2505
0.0000
-0.1664
0*0166
-0*0166.
-0*0000
0*1902
-0*1005
0*1005
0*0000
L-15^9
7S
97
TABLE 15
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR r - 1.5, C - < 00 > A*® 1 * 100
s
Correction factors for correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
on bottom
only
to free air
— — » “
to ground effect
( W ♦ L )
(U»L)
(W*D I
I U *0 I
-2.7193
-0.3061
-4,7555
0*9642
*♦♦00
-2*71 53
-0.3061
-4 . 7480
1*0930
" V / ri— 0*40
-4.7176
-0.3061
4.2062
-2.7 1.73
-0*3061
-4.7687
1*0526
t FA- *.U0
-6 . 604 1
-4 • 7 6 6 7
-0.3061
4*2655
-0*0020
0 • OOGU
0.0132
—0.09 b 3
0*0021
0 • GUUU
0*0407
... 0 *O 4 _G 5 ...
CH1* 3*00 GAMMA- 1*5
(M*L I
( U*L I
IW*D I
{U»D I
-2.7193
0*3061
-4*3063
1*4402
4*00
-2.7153
0*3061
-4*2988
1.5653
-4 *95 45
-4*2 68 6
0*3061
4 • 2 66 2
Y>H=”0*40 4/H-
-2.7173
0.3061
-4*3195
1.5288
c.1 A= 1*00
-5 # 3 4 9 0
-4* 3193
0 • 3u6 1
4.2855
- 0.0020
-0.0000
u.Ol 52
— U • U 6 tib
0 . UU4 1
— u • uooo
W*02O /
0 *0 36?
CHI -15.00
GAMMA- 1*&"’ ZtTA =
4.00 X / H
0. Y/H* 0*40
2 /h- i
[Will
IU.LI
IW»DI
|U*DI
-2.4107
1.4632
-3.3594
2.0G15
-2.4065
1.4032
-3.3519
2.1025
—4 *_490 3
-3 • 3 4 1 6
1.4634
3 • 6 9 i 3
-2 *4066
1.4633
-3 * 372 b
2.0731
-a • j3j6
-3 • 374b
1 * <+633
3. 8900
-0 *004U
- 0*0000
0*0132
-O.07 16
0_* 004 1_ .
-o. oooO
0*020 7
0*0294
CHI = 30*00"'" 5AMMA= 1*9’' ItTA-
{ W *L I
TUiLl
IWiD)
IU.DI
-1.5702
■ 2.53Q’4
-2.3622
2.0325
TOO ’
-1.5656
' 7 .530 A’
-2.3546
2.1063
Y/h= 0.40 4/H=
-3.3893
“ '-TiTSAl
2.5303
2. 7 762
-1.5679
'2.5 305 '
-2.3754
2.0863
cT A- 1.00
-3. 9450
-2.3784
2. 5303
2. (’734
-0.0023
-O.OOOG
0.0132
-O.03 jo
-0* OOuO
0_* 0 4 0 7
0* 04 2 O'
-cHr-As.aa gamma- i*?
(W»L)
iu.L)
(W»0 )
t U * D )
-0*5628
2,9286
-1.8190
1.5905
Y 2H- O. 4o
-1.8115
1 . 6446
-1.7 811
2.9285
1.3069
-0.5600
""'2.92 8 6 "
-1.8322
1.6269
L i A i . 0 0
-2.3247
-1.6322
2.9266
1 . 3059
— 0 • 0026
-0.0000
0.0132
-0.0384
0 *002 9
-0*0001
0*0206
0* 01 56
"CHI -60*00 GAMMA'* - ! .T ZETA-
(W»L)
(U*L 1
(W»D )
(U.D )
0. 1136
— 2.639T
-1*7376
1*0122
5T7Ti = "OV
0*1216
“ZT6396
-1.7301
1*0466
' Y/H- 0.40
' -0.6279
-1.6997“
2 • 6T9I
0.0405
0.1175
— ZV639r '
-1.7509
1.0366
fc T A- 1.00
-1.1677
-1.7509
2 .6398
0.0392
— U , wO J V
-O.OOul
0.0132
-U.0445
g.UUnu
-0*0004
0.0407
0.0096
-75.00
GAMMA- 1.5
ZETA= 4.GC - X7ir^
“TTh- "0*40
| M *L )
0.0470
0*0617
0.3749
0.0342
IU.LI
7,0660
-1*6 02 5"
2 . 0664
( W »DJ
-1.8403
-1*8j2'3'
2 .0635
-1 « o 33o
(U.DI
0.4874
o.5o47
— 0*3825
0.4967
t T A= 1 . O0
-0.13 i b
-i ■ 63 36
2 • UobH
-0* 3847
-0*00 i 4
— 0 .01/04
0.01 3 J
-0.0113
0*0075
-0* yUU 9
U * 0 4 O V
0 * 0040
CHI -90.00
' GAMMA= 1.5
Z&T A = "4*00
X/H= 0*' ' "Y/H- 0*40
Z/h= 0,
t T A * 1*00
<W»L)
{U*LI
(W.O)
( U *0 1
-0,5333
1.8035
-1*8035
-0 *o000
-0*4643
1 • 8001
-1*8001
-0*0000
1.0332
-l'.76BV" '
1. 7684
0 • O00U
-0.5113
'1*8167
—1*0107
— 0 • OOOU
0*5113
-1 . 8 187
1.616/
0 .OOOU
-0.0221
-0.0132
0*0132
-U.UOOb
0*0470
-0*0186
0*0106
0*0000
98
TABLE 15.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1.5, C * 4.00, AND tj * 1.00
8
Correc
tion factors for correcting from a wind tunnel which Is 1
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
1 t
to grour
»d effect
I— 3.0u GAMMA* 1,5 ZE7A* 4,00 X7Ri“0, Y/h»
<WtL> -0.2416 -0,2354 -2,2066
W»D -0,0790 -0,ff79B -0,6231
-0*0069 -0,0453 -0,0790
L U *°> U • 5408 0,7075 1 * 3 b 9 6
Z/H * G .
ETA* 1.00
■0.2 305
-2.0314
-0,0031
0,0031
■U , 0790
-0.0034 '
-0,0000
0,0000
‘0,0034
“0.0790
-0,0015
0*0300
0,6539
1,3066
-0,1131
0,0535
CHl * 3,00
(4*L)
tu*l »
IW'Di
(U,D)
GAMMA* 1,5
—0 ,241b
0 ,u 79 u
-0, 7 394
0,6371
-0,233*
7J,O790
-0,6997
0, 7671
“2,_A_3U5
6 775
0,0790
1,3696
“O,2305_
0,0790
-0.7370
0,7309
ETA* 1,00
-2, 7691
- 0*7376
0,0790
1.3666
-0,0 031
0,0000
-0,0015
-0*1018
- 0,0000
Q,0J81_
0*0462 •
'CHI*15,00 GAMMA- 1,5
Z E T A = 5V5RT X7rl*~ '57
( W * L I
t U * L )
<4,01
(will
< W.L )
(O.LJ
I4,UJ
<U*0 I
— u ,1534
0,3706
-0,4591
0,7143
GAMMA* 1,3
0,0931
u,6594
-0,1954
0,6321
-0. 1470
0.3765 '
-0.4193
0*8354
ZETA* 4,oo
~T/h* 0*05" Z/h*
-0.3970“
0*3 703
1,2912
-0,1502
0.3706
-0,4573
0,7966
0,6591
-0,1555
0,7229
-0.1331
0,6591
... 1.0099
0 ,0967
0,6593
-0.1930
0,6936
-2.5633
-0,4575
0,3/06
1,2902
ETA* 1.00
-2.1713
-0,1930
0. 6393
1,0067
-0.0032
0 .0000
—0,0016
“ 0.0022
- 0»QQ3o
0,0001
-0.001 7
“0*0617
.0032
• 0001
• 0302
• 0389
0* 0035
- 0,0001
0*0303
0, 02 9Q
CHI *45,00
I 4 * L I
HJ.Lt
(4,0)
IU.DI
GAMMA* 1.5
0,4110
0, 7734
-0,0949
0,4337
4,00 X/M* 0,
0.4197
0.7729
-0.0549
0,4901
Y/h
- 1,1039
-0.0326
0,7727
0.6218
Z/M- 0
0,4154
0 , 7 732
-0.0933
0.4776
“ 1 ,6906
-0.0933
0.7732
0. 6203
-0,0044
0.0002
-0,0017
-0*0439
0,0043
-0,0003
0,0304
0,0205
CHI *60,00
I W.L I
< O »L I
( 4,0 )
(U»D }
GAMMA* 1,5 ZtTA* 4,00
0,6 74U
0 • 707 5
- 0,1776
0,2281
0. 6662
0,7064
-0,1376
0,2664
Y/H- Q,fl4 t l/H •
CHI *76.00
GAMMA* 1,5
ZtfA* 4.00
<4«L)
0,7167
0,7390
<U.L>
0.5496
0,5456"
( 4 1 D t
-0.3860
-0,3470
(U,0t
0,1030
0,1197
CHI *90, UC
GAMMA* i,5
ZETA* 4,00
( 4 t L )
0.4373
0 • d U6h
(U.L)
0.5671
0,3336
(W.ot
“0.5671
-w. 3330
IU* Ul
-u.oouu
o.oooo
-0.6317
^0.1153
0,7 060 '
0,2287
-0.235Q_
-6.3245
0,5441
— 0,035 0
0,7071
-0,1760
0,2559
Z/h* o
0,7260
0*5404
-0.3051
0,1151
Y/H* 0,80 Z/H*
O.oolv
— 0, 5 1 U *4
0.4/U2
0,366 f
“0 • 3bo /
-0 • uuuo
-1,2093
-6.1760
0.7071
0,2267
-0.006 1
0.0004
-0.0016
■0*0277
-0,00 07
0*0383
0*0125
ETA- 1,00
-0,0033
“0.0113
0.0111
-0.3031
0.0013
-0.0020
0. 5404
-0.0015
0.0302
-0.0303
-0*0121
0.0046
ETA* 1.00
-
“0,4 702
-0,0329
6.0362
-U. 30b 7
-0,0016
-0.0350
0 , 568 /
0,0016
0.0350
0 , 0000
-o.oqoo
6?QPQ0
6^T- r I
L-15^9
99
TABLE 15.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND tj- 100
(c) y/H ■ *1.20 _
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
i
CHl— 3.00
GAMMA * 1.5
ZET A = 4.00 X/H* 0. Y/H* 1.20 Z/ H= 0.
ETA = 1.00
rw*Li
(U»L)
(W»OI
(U»D)
•o.Wi
-0.0349
-0.3291
0.2439
-0.0335 -0.6455 -0.0402
-0*0346 -O.^Obl -0.0349
-Q.ilbb -Q.Q 34o -0.2931
Q.6482 0 • 3 y 2**
’-1.3931
-0.2931
-0. 0349
0.6439
-0.0069
-0.0000
—0.0360
-0.1485
0*0066
0.0000
0.0/65
' 0*0662
ZET A= *4.00 X/H* 0. Y/H* 1.20 Z/H* 0.
ETA* 1.00
CHI* 3.00
GAMMA* 1.5
-1.3693
-0.2254
0.0349
-0.0069
0,0000
-0.0362
0*0066
Tw*u
’ Tu#u
-0.0471
0.0349
-0.2615
-0.0335 -0.6304 -0*0402
0.0348 -0.1381 0.0349
-0.1486 0.0348 -0.2254
0.4971 0.6482 0.4196
-0.0000
0*0767
<w»bi
-0.1336
0.0776
1 U »0 1
0.2159
CHI *15.00
GAMMA* 1.5
ZETA* 4.00 X/H* 0. Y/h= 1.20 Z/H* 0.
ETA- 1.00
-1.2849
-0.0966
0. 1669
0.6028
0*0068
( W»L )
( U »L )
(W»0)
(U.O)
-0.0061
0.1671
-0. 1330
0.3172
0.0079 -0.5612 0.0011
0.1666 -0*0090 0.1669
-0.0193 0.1668 -0.0966
0.4875 0.6052 0.4250
0.0001
-0*0365
-0.1078
-0*6602
0*0770
0*0625
—
CHI *30.00
GAMMA- 1.5
ZETA* 4.00 X/H* 0. Y/H* 1.20 Z/H* 0.
ETA- 1.00
—
tW.UT
0.1097
C.1253 -0.4110 0.1177
0.2895 0.1109 0.2899
0.1004 0.2895 0.0231
0.4020 0.A825 0.3555
-1 , 1187
-0.0080
4*W79l.
0.0231
0. 2899
0.0003
-9«6064
<U»L )
0.2903
-0,0136
0.2750
0*6771
{ W.D )
(U.D)
”” 0.4798
-Q.0806
6j0494 __
.... —
”
CHI-45.00
GAMMA- A.b
ZETA* A « 00 X/H* 0. Y/H* 1*20 Z/H* 0.
ETA* 1.00
- — cwfLr
ru.D
' (W.DJ
(U.D)
0.2826 -0.2190 "" 0.2733
0.336a 0.1530 0.3373
0.1444 0.3364 0.0670
-0.9126
-0.0097
0.0663
0.2636
0.0670
0.0007
-oVofroi
0.33 81
0.0302
0.1795
0.3373
-0.4368
0.2686 0.3140 0.2363
0. 3108
-0.0568
. . -
vf ,
- -
CHI *60.00
GAMMA* 1.5
ZET A= A, 00 X/H* 0* Y/H* 1.20 Z/H* 0*
ETA* 1 .00
1
<W»L>
<U#L)
I W.D)
(U.D)
0.4040
0.3023
-0.0 130
0.080?
0.4305 -0.0267 0.4175
Q*29ba 0.1117 0.3006
-0.7069
0.0237
-0.0135
0.0017
ftimi
-9.6022
0.1011 0.2982 0.0237
0.3006
-0.0367
0.1344 0*1435 6.1113
0. 1392
-0.0350
0.01*2
" '
■ ■
—
..
- ■ — •
CHI *75.00
GAMMA* 1.5
ZETA= 4.00 X/H* 0. Y/H* 1.20 I/H* 0.
ETA* 1.00
fw.in —
iu.LT
(W.D)
ovw*
0.2157
-0.1265
0.508A 0.1283 0i6S52
0.2017 -0.0030 0.2096
—0.0136 0.2010 —0.0904
-0.5373
-0.6904
0.2096
-0.0243
6*0232
0.9061
-0.0671
-0.0361 _
0 ,0446 0.0175 -“0,0390 V.
0.0108
-0.0135_
0.6036
TUTD1
0 . 0T5 5
—
....
“CfiI-90. OCT
GAMMA* 1.5
ZETA* 4,00 X/H* 0. Y/H* 1.20 Z/H* 0.
ETA* 1.00
“ -- -
-
rv.cT
■ CU.L)
'(W.D)
IT. 1744
0.2465
-0.2465
0.4617 0.2379 0.3979
0.1473 -0.1363 0.2173
-0.1473 0.1363 “6.2173
“0.3979
“0.2173
-0.0635
6.0292
“6.0760
0.2173
“0.0292
0.0700
0.0000 0.0000 -0.0000
0.0000
-0.0000
0.6666
rtr.b)
-0.0000
100
TABLE 16
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K - 10.00, AND tj = 1.00
(a) y/H
= ±0.40
8
Correction factors for
correcting from a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
>d effect
—
—
1
UMi«“3.00 GAFWA" 1*3 iSTA- 10.00 X/H*
0* Y/H* 0
40 Z/H* 0*
ETa- i.oo
(W.L1
-T.W '
“0.5738
-11.5959
-U.5739
-12.1321
“0.0001
0*0001
--
(U.L )
“0.3148
-3.0036
-0.3148
-3*0242
-0.0000
-0.0000
(W.O)
-3 • 6 1*1
-3.0137
-0.3148
“3.0242
“0.3148
0.0031
0.0085
ftl.D)
3.0978
3.1534
5.7256
3.1371
5.7238
“0.0393
0.0163
CHI • 3T0^ GAMMA* 1 • 5 ZET A—^ Q.QQ X/H = £>7 Y / n* u . 40 2/M = 0. L.TA = 1*00
*0*5739 -1 1.9169
0*3140 '-2.42 40
“2.4240 0 • 3148
3.4226 5*7256
r
CHI *14.00
GAMMA* 1,5
2ETA-
10.00
X/H* 0. Y/H* 0.40
Z/H- 0.
ETA* 1.00
'<**!_)
-0.2095
-0.2093
-10.3719
-0.2094
-11.1193
<U*L 1
1.5075
1.5075
-1.2574
1.5075
-1.2778
{ W * 0 )
-1.2728
-1.2693
1.5075
-1.2778
1.3073
(U.D )
3.5197
3.5602
5.3359
5 . 3339
• ' v •
} " CHI *30*00
GAMMa = 1.5
ZETA =
10*00
X/H* 0. Y/H- 0.40
Z/h = 0.
6 T A= 1.00
IW.t)
0.6169
0.8171
-9.0369
0*8169
-9. 3804
IU»L >
2.6210
2*6210
-0.1887
2.6210
-0,2091
<W»D)
-0.2041
-0.2006
2.6210
-o*2oyi
2.6210
IU.0)
2.9902
3.0206
4.2216
—3*0117
4. 2216
— — — j-
CHI *45*00
GAMMA 3 1.5
“Teta*
ToVou
X/h* o. Y/H*"o740"
Z/H = 0.
ETA- i.OO
li.L )
2.1700
2.1704
-7.1430
2.1702
-7.6831
iU.L)
3.0600
3.0600
0.2066
3.0600
0, 1863
(WfDI
0.1914
0.1949
3.0600
0.1863
3.0600
(U.D I
2.0087
2.0305
2.6873
2.0241
2.6872
CHI-60.00
gamma- 1,5
ZETA = 10.00
X/H ■ 0. Y/H* 0,40
Z/H- 0.
ETA* 1.00
<W»U
3.3747
3,3752
-5.2478
3.3749
-5 . 7849
<u.u
277579
2,7579
-0.1663
2.7579
-0. 1868
(M.01
-0,1817
-0.1783
2*7576
-0.1868
2.7579
(U.D )
1.0101
1.0242
1.1251
1.0201
1 . 1250
i CHI-75,00
GAMMA* 1.5
ZET A* 10,00
X/h- o. Y/H* 0,40
A/H* 0.
ETA= 1.00
f -*W.L>
3.8007
3.8017
-3.6590
3.8012
-4.1933
ru »l \
2. 0260
2,0259
-i. 1325" ' "
'2.0260
-1 , 1529
T¥»Dt
-1.1479
“1 • 1444
2 7023 8
-1.1529
2.02o0
■' . IU.DI'
0.3918
0.3986
-0*0112
0.3967
-0.0114
Crfl*9u.uoL
- -
GAMMA- 1,5
ZLTA 3 1Q.OO
■X/h* u. y/h- o,40
"ETA* TToo
7¥TlT
wn
2,8692
-2*3340
2.6648
-2.8648
TUTLT
Z , 1301
2,1 269
-2.1149
2.1353
-2.1353"
, rsroi
-27TJ01
-2.1269
2.1149
-2.1353
2 • 1353
-0,00 00
-0.0000
O.uouO
-0 • OGOG
0. GoOO
1 W»L ) 4jT, $740 “0*5736 “11*3639
Hit!
0.3148
0.3146
“2.4036
Jplfr
-2.4190
-2.4155
U.3148
3*3872
3*4373
5.725b
“0 .OQOl 0.0001
0*0000 ~ 0.0000
0.0030 0.0085
“0 .0334 0.0147
■0*0001
0.0000
0.0051
■0.0236
0 >0001
“ 0.0000
0.0053
0.0119
“O.ftflOl _ 0.0002
“0.0000 -0.0000
0*00^1 0.0033
“0.0213 0.0 0 69
-0.0002
0.0002
“0.0000
-0*0000
0.0051
0.0085
“0.0154
0.0064
“U *0003
0.0003
-0,0000
“0.0000
0.0031
0.0085
“0.0100
Q.Q041
“0.0003
0.0005
-o.oooO
-0.0001
0.0031
0.0083
“0.0048
0.0020
“0 .0037 0*0044
“0.0032 “0.0004
0*0032 0.0084
0.0 000 070000
L-15^9
101
TABLE 16.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1-5. K 10 - 00 ’ AND ^
(b) y/H=i0.80
Correction factors for correcting from a wind tunnel which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground
effect
—
— r ' r
CH S = -3*04
< WlL >
(U.L)
tW»0)
IU*D)
- 0.0200
-0*o7Bl
-0.4429
1.0611
iU.J'J
-0*0i96
-Q * U7ttl
-C * 4264
1*128*
. i/n-
-2*603 2
-0*41 7 6
-Jtu/ei
1 ,4 /VO
-0 • 01 5b
- 0- • 0 7 o 1
4420
ETA- i.OQ
-3. 2030
-0*4420
-0*0761
1.4797
-U • 0002
-0 * uOoo
-0 « 00 1 4
-0.04^4
U • COO t
0*0000
O* 0 1 bo
CHI = 3.00' GAMMA ='“175“
<u*L )
(W»D)
(U.D)
-0*0200
O.oTSI
-0*2679
1*1036
: TO • uO X /h -
-0*0196
"" O.GTST
-0.2713
1. 1643
-0 *2o2 3
0.0761
0*0761
-0*2669
1*1447
iTm- i « 0 0
- * < xbbo
-0.2669
0.0761
1.4797
- 0 .0002
0*0000
- 0.0010
-0 * C409
- 0*0000
0*0166
0*0196
CHI=13»44 GAMMA 3 1*5
l w * L )
(u.LJ
(M.O I
10*01
0.0751
0.3737
0*0059
1*0825
0 .0 V 3 *
4**7 J7
0 • 0 0 6 9
i .1136
4 • 44 iV
4 ■ _ 7 57
n joio
-O . uOd.
U • 0000
-4*00x0
-0*0331
0 • U 4 4 t
— 4 • 4 W 4 4
4*4134
0*4130
=30.00
GAMMA= 1*5
ZET A= 10.00 X/i
2 7 , Y/m= 4.04
U«L>
0.3453
0*3456
*4 7o 7
(U.D
0.6478"
0*6478
4. J 4* *
{ W *0 )
4.2760
0*2946
0 • 6 4 7 o
IU*D )
4 . bob*
0*9251
1*1097
0 * **»3 3
u » o4 7 b
4*2 7 ? 4
0 . 4 4<J 2
“4*0 400
U*L i3o
Chi =45.00 '
(w.L)
tU*L)
(WfOl
( 0 * 0 )
0.7122
0 * 749 6
0*377 4
0*5843
0.7490
0 *3940
0*6106
Y/rl =
-1*6 506
i. / n - 4
0. J i23
0.7 4 vo
0**784
t T A = x • JO
-2.4*40
0. 7496
0 . i 346
-O . 400 *
u .OOOo
— o *00 io
-0 • 4 1 7b
4. 004*
-4.0444
4*0130
4 ♦ 0 0 0 5
(W*L )
icrvu
(M»0)
(U.D)
1* 0716
“ 0.6547
0 . 27? 5
0*2752
0 .6346
0.2941
0.2922
0 • 4 3H 6
0.3376
Z7TT= 0
2*072.*
4*6347
4*2 783
0*2867
. O U 6 4
4*2/03
0.6347
0**374
-4 * VduH
0 • 4044
-0 . 00 iO
-0*0113
CH I =73.00
GAMMA 3 1.5
2L[M= 14.44
X7n- 0. 7/ri- 4*64
(Mil)
1.3064
1*5060
-0 » O V42
( 0 * L )
4.4052
0*4048
0 • 4 3 1 6
(w*0)
0.0063
0*0229
0 • 04 7 1
( u to )
0*0672
0*0752
0*4752
CHI =90.04 ’
GAMMA 3 1.5
~ZETA = 10.00
X/H= 0* Y/n= 0 • b4
{ n i L >
1*2335
1*2452
“0 *6 60 V
(U«L >
0 * 341 4
0*5252
-0* 3 164
(W.D)
-0.3414
-0*3252
0*3164
(U*0)
-0*0000
-0*0000
4*4000 —
. • *4 7 2
r*403i
; *oo 7*
J • 0 7 27
• 2*yi
• *440
4.06 7 *
0 • ** 4 3 1
0*0 7 H *
• 2* V i
-u . J“Hju
4 « * *» 4 6
4 . 4 4 4 4
-4.004d
0*0001
“4 *00 io
-0*0033
-O *4430
u . OOOo
-4 .044 0
4*4400
4 • 444 b
-4*0042
4* 4130
0*4426
u* 0061
-0*0139
4*4139
4*0044
102
TABLE 16.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 10.00, AND tj = 1 .00
(c) y/H = ±1.20
Correction factors for correcting from a wind tunnel which Is
closed
on bottom
only
6^T-1
L-15^9
103
TABLE 17
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 0.70, AND TJ = 0.75
(a) y/H = -1.50
8
Correction foctors for correcting from a wind tunnel which Is
closed
close d
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
1 1 r
CHI = - 3.00
( W f L )
(u,r 1
(W.D)
(U,C1
G A^P A = 1.5
Yet*- 0.70 x/h*
0. Y/H—
1.50 Z/H = 0.
ETA= 0.75
-0.3202
-0.0156
-0.0879
-0.0201
-0.2039
0.3285
-0.1137
-0.0174
-0.2249
-0.0186
-0.3176
-0.0952
-0.3176
-0.0186
-0.0953
0.0030
0.0739
0. 1370
-0.OO15
0.1131
-0.6379*
0.2566
0.3122
0.0317
0.2137
— 0 . 6695
0.2250
CHI* 3.00
(H,L )
IU.L)
IW,D>
( U » D )
CH 1= 1 5. 00
( W , L I
IU.L >
tw,r>
iu,p)
CH I * 30. OC
( M , L )
IU.L)
1W.D)
IU,D>
_CHI»*»5.00
JJUU-
tU. L )
OUD1.
IU.D)
CHI =60. 00
IM.L )
IU.L)
I VI. D)
tU.D)
CHI* 75. OC
( M . L )
IU.L)
(W.C)
CU.C)
chi = 90. 00
(U.L )
IU.L)
tW.D)
IU.D)
GAHHA* 1.5
ZETA*
0 .7 0 X/H- 0.
Y/H=-l
.50 Z/H* 0.
ETA* 0.75
-0.3202
0.0156
— 0. 0879
0.0201
0.3033
0.0810
0.0174
-0.2249
0.0186
-0.2952
-0.1089
-0.2952
0.0106
-0.0953
-0.0030
0.0792
0 . 1 370
0.0015
0.1155
-0.5449
0.2693 _
0.3122
0.0638
0.2137
-0.6086
0. 2055
GAMMA* 1.5
ZETA*
0.70 X/H* 0.
Y/H=-l
.50 Z/H= 0.
ET A* 0.75
-673014
0.0725
-n * 1
-0.0644
0.0961
-0.1245
0.2771
■0.0119
0.0820
-0.2046
0.0881
-0. 2412
-0. 1154
-0.2412
0.0881
-0.0968
-0.0156
0.0886
0. 1401
0.0080
0. 1 16B
-0, 3918”
0.2726
0. 2884
0. 1048
0.1891
-0.4965
G AMM A = 1.5
ZFTA =
0.70 X/H= 0.
Y/H*- 1
1 .50 Z/H* 0.
ETA* 0.75
-ri. 25 I f
0.1134
- 0. 0756
-0.2564
0.0007*
0. 1657
0.2834
0.0638
n .1343
-0. 1498
0. 1483
-0. 1757
-0.0094
-0.1757
0.1483
-0. 1013
-0.0349
0.1001
0. 1505
0.0174
0.1 133
0.2379
0.2230
0.1147
0.1220
-0.3710
0.1232
G A MM A = 1.5
ZETA*
0.70 X /H = 0 *
Y/H*- 1
1.50 Z/H= 0.
ETA* 0.75. _
—
- -
-0.1926
0.1004
0. 00 32
0. 3148
-0-0659
-0.0424
-0. 1069
O. 1690
0.1930
0,1109
n_ 1 367
6. 1632
-0. 1297
-0. 1297
Q. 1632
-0,0628
0.1141
0,0297
-0.01 56—
-0.1652
0.1739
0.14)9
0,0923
0.0415
-0.2575
0*0016
GAMMA* 1.5
ZETA*
0.70 X/H* 0.
Y/H*-
1.50 Z/H= 0.
ETA* 0.75
-0.1426
0.0 3 17
07l53T ”
0.1814
0.3466
0.1246
..lUflflT.9 —
0.0739
-0.0431
0.1373
-.0 . LQ.6 1
0.0575
0.0035
-0. 1061
0.1373
-0.0144
-0, 1056
-0. 1056
0. 1340
0.1962
Q.Q441
0.0279
-0.0963
-0* 02-68.. ....
0. 1017
-0.1538
0.0442
GAM-A* 1.5
ZETA*
0.70 X/H* 0.
Y/H=-
1.50 Z/H= 0.
ETA* 0.75
-
-n. 10 6 7
-0.0604
0.1077
0.1490
-0.056T- _
0.0398
C. 353 Y
0.1104
-0.0378
0. 1006
-O. 0937
0.0344
-0.0937
O. 1006
-0.0709
-0, 1610
0.1595.
0,2255
0.0404
0.0370 _
0.0658
-0.0301
Q.«_Q£93
0.0287
0.0250
-0.0212
-0,0632
0.0140
GAMMA~ 1.5
ZETA*
0.70 X/H - 0.
Y/H=-
1.50 Z/H* 0,
ET** 0.75
-0.0300
-0.0906
0.0906
-0.0000
0.1809
0.1033
0.3375 ’
0.0756
-O. Q756
-0.0521
0.0812-
-0.0812
0.0521
-0,0812
0.0220
-0.1718
0.1716
0,2330
0,0221
-0.0221
0.0000
0,0000
-0.0000
0.0000
-0.O0QQ
0. 0000
104
TABLE 17.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 0.70, AND tj = 0.75
(b) y/H = -1.125
Correction factors for correcting from o wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
i i t —i — —
to grour
id effect
CHI— 3.00 GA88A* 1,5 ZETA* 0.70 X/H* 0.
y/h— i.i 2 z/h- o.
ETA = 0.75
IW*L) -0.4935 -0.1709
ttl.L) -0.0224 -0.0295
(W.C) -0*344.1 -0.4 1 60
IU.C1 -0.6387 0.2308
0-7047 -0.3532 0.0627
-0.2465 -0.0264 -0.4668
-G.Q213 -0 . 4668 -0.0264
0.3960 C. 0275 0.2695
-0.1354
0.0041
0. 1226
-0.6662
0. 1873
-0.0030
Q.QS08
0.2532
CHI- 3.00 GAM8 A* 1.5 ZETA* 0.70 X/H* 0.
Y/H— 1.12 Z/H- 0.
ETA* 0,75
f M.L 1
(U.L)
(H.D1
<U,D)
-0,4935
0.0224
-_Q*3Q52
-0.1709
0.0295
-0-3927
0.6426
-0.2050
0.0233
-0,3502
_ 0.0264
-n.Axes
0.0222
-0,4385
Q.Q264
-0.5327
o. 3<m
0,3960
0,0750
0.2695
-0.1354
-0.004J
Q. 1333
-0,6077
0, 1073
0.0030
0-04 5fl_
0.2338
1-15.00
5-AHHA^ 1,5
2 ETA- 0.70 X/H*
0. T/H— 1,12
Z/H- 0.
ETA- 0-75
IH.U
auu.
IHxDl
-0,4632
0. 1034
-0.1348
0.140Q
- - -0.3264
0.5545
-0,1082
0.1031
-0.3259
0, 1244
-0. 3625
-0,0270
-0.3625
0. 1244
-0,1373
-0,0210
0. IS 1 3
0, 1?1Q
0,0157
1U.DJ
..... -0.3628
0*3346
0.3617
0, 1378
0.2340
-0.50Q6
0.1968
CHI-30.00 GAHHA* 1.5 ZETA* 0.70 X/H* Q, Y/H— 1.12 Z/H- 0. ETA* 0,75
14, L)
11), L 1
IWiD}
1U,0)
-0.3P32 -0.0373 0.5063
0-1570 0.2337 0,0109
- 0. 091 3 — nn*2Za&. 0*1676
-0.2264 0.3094 Q,?7?2
-0.2402 -0.0337
0.2040 -0.26_18
- 0-2618 G,2Q4_Q_
<1*1554 0.1403
-0.1430
-0.0470
0.1705..
-0.3618
0 . 202 ?
0.0347
0. 02311
0. 1540
_CH1«45.00
GAWA* 1*5
ZE T A= Q,7Q_ X/H* 0,
Y/J-L—
1*12
. Z/H* 0.
ETA- 0.75
1K.U
1U.L1
.. - IM.01
- 0.292*
0. 1305
0.0052
0.0800
0.2764
-0.1796
0.5014
0.1004
0.1496
-
-0. 1428
0.2154
-0. 1847
-0.0023
-0.1847
0, ? 154
-0. 1497
-0.0848
0.2228
0,O6l1_
1U.01
-0. 15D7
0,238I__
0,1682
0.1240
0.0360
-0.2746
0*1 1*2
CHI -60-00
GAH*»A= 1.5
ZETA- 0,70 X/H* 0.
Y/H=—
1 . 12
Z/H* 0.
ETA* 0,75
1 W, L 1
tU,L)
-O.2260
0.0291
0.0745.
0.1698
0.5051
-0.07C5
0.0356
-0.1475
0.2483
0.2699
- -0.1 6J3
0.1526
0.0604
0. 1724
-0*1396
-0.1396
0.1724
-0. 1433
0.214 1
0.0975
IU,D!
-0.1000
0.1501
0.0930
0.0743
-0.0262
-0. 1743
0.0758
CHI*7S« 00
GA"KA= 1.5
ZETA- 0.70 X/H* 0 •
Y/H— 1
1,12
Z/H* 0.
ETA= 0.75
I W f L )
(U.L)
IW.Dl
(U.C)
-0. 1721
-0.101 1
C. 1302
0.2036
0.2540
-0.1868
C.4097
0. 1760
-0.0598
-0.0644
0. 1214
-0*1143.
0.0609
-0. 1143
0. 1214
-0,1077
-0.2225
0.2445
0.268Q
0.1327
-0.072S
-0.0491
0.0680
0.0463
0.0305
-0.0265
-0.0796
0.0375
CHI-90,00
( W»L )
(Uf L 1
G AHM A = J.5
ZETA= 0.70 X/H* 0.
Y/H— 1
.12
Z/H- 0.
ETA* 0.75
-0.0798
-0.1692
ft. 1692
0.1P1T
0.2331
-0.2331
0.4392
0.1765
•0.1765
-0.0741
0.0942
-0.0942
0.0741
-0.0942
0.0942
-0.0058
-0.2635
0.263S
0,2552
0.1389
-fl*U89
0. 0000
( U , D )
-0. 0000
0.0000
0.0000
-0.0000
0.0000
-0.0000
StjCT-l
L-15^9
105
TABLE 17.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.70, AND r? = 0.75
(c) y/H = -0.75
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
! only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00
GAmma = 1.5
ZETA* 0.70 X/H=
0, Y /H=-0* 75
Z/H* 0,
Ef A* 0.75
(W.U
-0.799P
- 0 . 22 r 0
1.2472
-0.5414
0.35P4
-0.2583
tU.Li
-C.01C7
-0.0421
-0.4198
-O.Q360
-0.6648
0.0062
1W.C1
-P.5079
-0.6502
-0.0313
-0.664e
-0.0368
0.1570
[u.n
-C.6e96
0.3296
0.5076
0.0202
0.3313
-0.7098
0.3m
-0.0053
0. 0146
0. 3095
CHI- 3.00
gamma* 1.5
ZETA- 0.70 X/H* 0.
Y/H--Q, 75
Z/H- 0.
ETA* 0,75
(W»L 1
-0.7998
mT.2220
1 . 1258
-0.5414
P.2666
-0.2583
1 U.L 1
0.0307
-0.3666
0.036P
*0.630 1
-0.0062
14,0)
-0.4566
-0.6267
6.0313
-0.630 1
0.0360
0.1735
IU. 0 J
-0.5628
0.3767
0.5076
0.0900
0.3313
-0.6509
0 . 3131 *
0.0053
0.0031*
0.2686
Chl>li,QD_
GAMMA * 1.5
ZETA* 0.70
X/H- 0.
Y/H*— 0.75
Z/H* 0.
ETA* 0.75
(M,U
-0.7521
-0. 1703
0.9391
-0.4897
0.1311
-0.2624
0.3193
(U,L>
0.1394
0.1984
-0.2290
0. 1713
-0.5230
-0.0319
0,0272
( W , D )
-0.3211
-0.5402
0.1429
-0.5230
0.1713
0.2018
-0.0172
(U,0)
-0.3634
0.4294
0.4593
0 . 1800
0.2ei3
-0.5434
0.2493
CHI-30.00
GAMMA* 1.5
ZETA* 0.70
X/H* 0.„
Y/H*-0. 75
Z/H* 0.
ETA* 0.75
1 W,L 1
-0.6304
-0.0177
0.8076
-0.3557
0.0541
-0.2748
0.3380
IU,W
0 . 2008
0.3319
-0.0448
0.27ie
-0. 3692
-0.0710
0.0601
(W,0)
-0. 1363
-0.4122
0.2097
-0.3692
0.2718
0.2329
-0.0429
01 , 0 )
-0.21C7
0.4103
0.3369
0.2060
0. 1547
-0.4247
0.2043
>45-00.
GAM«A= 1.5.
ZETA* 0.70 X/H*_
0 ,. . Y/H—0.75
Z/H* 0 •
ETA* 0.75
(W,L )
-0.5023
0.1590
0.7608
- 0.2100
0.0501
IU,L 1
0- 1458
0.379 1
0. 1050
0.2730
- 0.2462
( W , D )
0.C1P9
-0. 3213
0. 1603
-0.2468
0.2730
(U , 0 )
-0. 1573
0. 3226
0.2095
0 . 160 1
0.0250
-0.2923
-0. 1272
0.2657
-0.3174
0.3690
0. 1Q61
-0.0745
0. 1624
CHI*60.00 GAMMA* 1,5 ZCTA* 0. 70 X/H= 0. Y/H*-0.75 Z/H = 0. flA= C.75
<U,L)
-0.4206
0.2905
0. 7466
-0.1172
0.0716
-0,3034
0.4077
(U, L 1
-0.0055
C.3791
0.2070
0.2075
-0. 1735
-0.2130
0.1716
— tlUDl
0,1344
-0.2953
0.01 29
-0. 1735
0.2075
0.3079
-0. 1218
IU.D1
-0.1231
C.211C
0. 12 93
0.0914
-''.0391
-0.2145
0. 1 196
;ahha» 1.5
ZETA= Q.7.H. X/H*
0. Y/H=-0.75
Z/H= 0.
LTA* C.75
tW.L)
-0.3671
0.3470
0.7246
-0.09 14
0. 0079
-0.2757
0. 4385
HULL
-0 ■ 19 05
0.3000
0.2776
0. 1407
-0.1335
-0.3312
0.2473
1 M ■ 0 ]
0.2318
-0.3315
-0. 1573
-0. 1335
C. 1407
0. 3653
-0.1980
(U.O)
-0.0731
0. 10 39
0.0736
0.0356
-0.0315
-0. 1 087
0.0682
CHI*9Q. 00 GAMMA* 1.5 ZE TA* 0.70 X/H* 0. Y/H*-0.75 L/ H*J).
ET A= Q . 75
<W.L) -0.2773 0.3354
IU.L1. _ -0.3173 0.4101
(W,D) 0.3176 -0.4101
tU#D) -n.0000 0.C000
0.6704
-0.0953
0.0953
- 0 . 1 R 20
0.4307
0.3-315
_ 0.1059
-0.1059
-0.4237
Q. 3043
-0.3315
-0.1059
0.1059
0.4237
-0,3043
0.0000
- 0.0000
0.0000
- 0.0000
0.0000
106
TABLE 17.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = AND T)= 0.75
(d) y/H = '0.375
Correction foctors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free, air
to ground effect
CHI-90.00 GAP*-A= 1.5 2 ET4* 0,70 X/H= 0, _ Y/H--^7 If H* 0,
t W,L ) -C.6246 0.6596 1.0325 -0.1111
(U.LI -C.5133 0. 610 1 0 -520 5 ,0.*.11W
(K,C) 0.5133 -0.6101 -0.5205 -0. 1 H0
UJ t D> -0.00C0 0.0000 0.0000 -0.0000
L-15^9
107
CHI — 3.00
(M.U
(U.U
(W.DI
f U. D >
TABLE 17.- Continued
lateral distribution of interference factors FOR r = 1.5, c = 0.70, AND V - 0.75
(e) y/H « 0
8
Correction factors for correcting from o wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
— i — 1 1
to ground effect
i **"
GAM«A* 1.5 ZEIA^ QaXQ X/H* Q,
Y/H* 0.
-1.3020
-0,04 16
-0.7092
-0.R477
-0.2003
-0.06Q6
-0.9107
0.4344
2. 1274
-0.6592
-0*4434
0.6772
It H* 0
-0.5150
-Q*Q518
-0.9533
0.0070
ETA- 0,75
0.9192
-0,9533
-0.05 18
0.4070
-0.5670
0,010.3
0. 1641
-0.B548
0.6148
-Q.QOftfi
0.0426
0.4274
CHI- 3.00 GAMMA- 1.5
(W,L)
IU.U
( VI . D )
IU.C1
-1.3820
0,0414
-0.7233
-0.6846
-0.2003
-0.8838
0.5062
1.8992
-0.5892
0.0434
0.6772
-0.8150
o.osifi
-0.9107
0. 1047
. ETA* 0 ,75
0. Z236
-0,9107
0.0518
0.4070
-0. 5670
-0,0103
0. 1874
-0.7893
0.6148
0.0008..
0.0268
0.4016
CHI- 15.00 GAMMAm 1.5 7ETA-_ 0,70 X/K-0*
( W » l >
(U V L)
<W,0)
(U.0)
Y/H* 0.
-1.3053
0,1843
-0.5240
-0.4296
-0.101 1
0,2831
-0.7577
0.5920
1.5335
-0,3813
0.1938
0.6074
Z/H- 0.
-O. 7280
0.2376
-0.7536
0.2396
ETA- Q,75..
0.4102
-0.7536
0.2376
0.3352
-0.5774
-0,0531
0.2296
-0.6692
0.6269
Q.Q455
-0. 004 1
0.3524
CHI-30. 00 GAMMA* 1.5 ZETA-
(W,U
(U.L1
(W,0>
(U.O)
-1.1216
0.2423
-0.2313
-0.2616
0.70
0.1540
0.4609
-0.5S99
0.5691
1.2716
- 0* 09 1 9
0.2631
0.4418
l /H= 0.
-0.51 18
0. 3606
-0.5126
0.2736
0.1901
-0.5126
0.3606
0.1650
-0.6098
-0,1183
0.2813
-0.5352
0.66S8
- 0.0474
0.2955
(M # U
(U,t)
(W,D)
<U.C)
GAMMA- 1.5
-0.9551
0.1305
0.0225
- 0.2099
0.70
0.4404
0t5V71
-0.4272
0.4462
1.1049
0.1491
0.1668
0.2860
It H* 0
-0. 2924
0.34Q9
-0. 3208
0.2039
XT A* 0,75. ...
0. 1187
-Q*1ZQB
0.3409
0.0100 _
- 0,6626
- 0 .2104
0.3434
- QafLUfi -
0,732?
0.1762
-0.1544
Q.2424„
CHI-60.00 GAMMA-* 1*5 ZETA* - Q.TO- X/H- 0.
(W,L)
(U.U
(w.oi
( U »D 1
-0.0055
0.6649
Q-5297
-0.4092
0.297?
1.1905
0.3192
-0.0476
0.1946
-0. 1608
G. 24Jt0
-0.2098
0. 1100
_ETA*_ 0*I5_
0 . 112 ?
-IK 2098
0.2440
- 0.0536
-0,1247
- 0.3487
0,4 324
- 0,2957
0.0257
_JU284?_
-0, !9?J
0.1871
CHI-75. 00 GAMMA- 1.5 ZETA- 0.70
(H,L )
(U.U
(W.01
(U.O)
- 0.8812
-0.3P15
0.4127
-0.1244
0.8102
0.5830
-0.5040
0. 1S61
1.2262
0 , 4573 —
-0.3118
0.1217
ZAH- Q.
- 0 . 1201
0. 1600-
-0.1527
0.0407
ETA? X- 75 —
0.1165
- Q . 1 521
0. 1600
-0.0366
-0.7611
- 0,5415
0.5655
-0.1651
0,9303
0-4210
-0.3513
0,115^
CHI-90.00 GAMMA- 1.5 ZETA- 0.70 X/H* 0.
<W,U
(U.U
(W.O)
(U.O)
-0.8635
-0.6256
0.6756
-0.0000
0.9022
0.6966
-0.6966
0.0000
Y/H*
1.2620
0.6106
-0.6106
0.0000
ZVH? Q.
- 0. 1 170
0.1170
- 0. 1170
0.0000
ETA- 0.75
0 . 1 170
-Q.IL70
0.1170
-0.0000
- 0.7465
-0.7426
0.7426
-0.0000
1.0192
0.5796
-O.5T90
0.0000
108
Correction foctors for correcting from a wind tunnel which is
closed
on bottom
only
to free air
closed
on bottom
to ground effect
GA HMA« _1.5 —ZEIA*
-1.26Q6
-0.0268
-0.71107
-C.911I
-0.1739 1.7183 -0.7295
-0-0 552 -D.542L1 - 0.0 47?
-0.7436 -0.041 J -0,8637
0.4637 0.6600 0*01 17
CHI= 3.00
-1.2606
0.036A
-0.6829
-0.7507
-0,1719
0.G552
-0.7101
0.5223
1.5360
-0.474 L
0.0411
0.6600
-0.7295
0.0472
-0.^234
0. 100 1
... E I A= C.75
0.5710
- 0.8234
0.0472
0.3844
-0.531 1
-_0.Q1.QA_.
0* 1405
-0.8508
0.5556
Q*Q0fi0
0. 1133
0.4222
-1. 1951
0. 1 6Ji_
-0.5085
-0.4947
-0.6542
_ 0* ?1 72
-0.6824
0-2213
_Y/H=. o - 37 2/H= O.
-1.0365
0.2154
-0.2505
-0. 3100
-Q,8897
0.1128
-0.0205
-0.2331
O. 13P6
0-42?.fi_
-0.4054
0.5463
1.0580
^.- 0.030 1
0.2634
0.4409
-0.4649
0.3341
-0.4696
0.2533
-0. 2466 _
0.3215
-0.2996
0.1476
_- Q. 4696
0.3341
0. 1628
._Q*J)9G5
-0.2996
0 .3215
0.0149
-0.621}
-0.2087
0.2791
-0.4243
-0.8243
_-C. 1046_
0. 1691
-0.1879
-0. 1486
Q.2J45
-0. 1998
0. 1049
CHl-7_5 i QQ G 1.5
(W*U — 0.PO44
tuaj -0*2547
(M«D1 0.3536
lUf D ) -0.1172
- 0.1122
0. 1548
-O. 1475
0.0394
0.1086
-0. 1475
0 . 1 548
-0.0352
-0.7421
-0.5486
0.5466
- 0.0000
- 0.1111
0. 1140
-0. 1140
-0.0000
L-15^9
109
TABLE 17.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5. C » 0TO ' ” = °' 75
(g) y/H = 0.75
8
i
Correction foctors for correcting from o wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
—i r “
to ground effect
CHI*-3.00
GAMMA* 1.5
ZE T A*
0.70 X/H ■« 0. Y/i»= 0.75
Z/H= 0.
ETA* 0,75 .
(W.L)
(U»L )
(W»D)
(U,D>
- 1.0094
-0.0253
-0.6239
- 1.0246
-0.1111 C.9081
-0.C441 -0.3038
-0.4162 -0.C367
0.5255 0.6333
-0.5414
-0.0368
-0.6648
0.0202
0.3584
-0.6648,
-0.0368
0.3313
-0.4600
0.0115
0.0409
-1.0448
0.4303
-0.00T3
0.2406
0.5053
CHI- 3.00
GAMMA- 1.5
ZETA*
0.70 X/H- 0. Y/H- Q.75
Z/H= O.
ETA* 0,75
(W.L)
(U.l 1
IW.D)
IU,D)
- 1.0094
0.0253
-0.5858
-0.8747
-0.1111 0.8161
0,044 1 -0,2374.
-0.3689 0.0367
0.5569 0.6333
-0.5414
C , 0 3 6 8
-0.6301
0.CP60
0.2666
-0 » 6 3Q 1
C.0360
0.3313
-0.4680
-Q. 01.1 5
0.0443
-0.9627
0.4303
0.0073
0.2612
0.4689
CH|- 15,00
GAMMA* t. 5
ZETA*
OjJO X/H» 0, Y/H* 0,75
1 / H* 0.
ETA= 0.75
(W.L)
(U.L)
(W.C)
(U.D)
-0.9674
0. 1123
-0.4670
-0.6239
-C.ouoe 0.6907
0.2084 ... -0.C231
-0.2485 0.1700
0.5726 0.5014
-0.4897
O. 1713
-0.5230
0. 1800
0.1311
-0,5230
0.1713
0.2813
-C.4775
-0.0590
0.0560
-0.8039
0.4408
0.0171
0.2745
0.3926
CHI*30. 00
G AMM A = 1.5
ZETA*
0,7£_ X/H* 0. Y/H* 0,75
Z/H* 0.
ETA- 0.75
—
(W.L )
IU.U
t W.D )
(U.D)
-0.8642
0.1448
-0.2830
-0.4116
—
0.1191 0.6435
0.3495 0.1028
-0.1022 0.2647
0.5022 0.4457
-0.3557
0.2718
-0.3692
0.2060
0.0541
-0.3692
0.2718"
0.1547
-0.5085
-0.1270
0.0854
-0.6176
0.4748
q,Q777__-
0.2670
0.2962
CHl*45.00
GAMMA* 1.5
ZETA*
0.70 X/H* 0- Y/H* 0.75
Z/H* 0.
ET A = 0.75
(W.L)
IU*L1
(W.D )
(U.D)
-0.T677
Q. ns 9 4
0.3246 0.6847
£,3965 _ Q*230J
-0.2100
0*2730
0.0501
-0.2468
-0.5577
_ -0.2136 _
0.1406
-0. 4456
0.5346
J). 1234
0.2270
0,2041
-0. 1062
-0.2055
-0,0198 0.2467
0,3643 Q.2900
-0.2468
0. 1601
0 .2730
0.0258
n v/11- n V/H* 0.7^ Z/H* 0.
_£JA=__Q.15
CHI-60. 00
IW.L)
GAMMA* 1*5 —
-0.7253
7 F T A =
0.5009 0.7598
-0.1172
O.OTJ6
-0. 1735
-0,6081
-0. 324I_
~M i e i
0- 1600
(U.L)
(W.D)
(U.D)
-0.11 72_-
0.0596
-0.1961
-0.0297 0.1306
0.2129 0. 1662
-0, 1735
0,0914
0,2QT5
-0.039L
0,2331 _
-0,2876
0. 1438
0,1215
FT A* If. 75
•
CHI*75,Q0_
(W.L)
GAMMA* Jl*5_
-0.6953
ZETA*
0.6122 _. 0*8191
-0*09 14
0. 1407
0.0870
-0.1335
-0.6019
—0. 446L_
0,7036
0.1895
(U*L1—
(W.D)
(U.D)
- Q . 3Q54 .
0.2333
-0. 1040
-0.1262 -o.om
0.0804 0.0732
-0*1135
0*0156
0,1401
-0,0315
0,3668
-0*1396
0,0073
0.Q528
—
—
...
chi-9Q*oq
n 7n v/u* n. v/H* 0.75 Z/H* Q*
_£IA^ Da 75
-
GAMMA?. 1 . j
. 7L.1A?
wm i
-0.4875
-0,5100.
0.7421
0-1T4S
(W.L)
. 1U.L1
IW.O)
IU.P)
-0.5828
-0.4042
0.4042
-0.0000
0.6468 0.8267
-0.0953
0. 1059
0.0953
-0. 1059
-0.2804 -0.2451
0.0000 0.0000
-0.1059
-0.0000
0.1059
0.0000
0.5100
-0.0000
-0. 1745
0,0000
- 0.2792
- 0* 0210
-0. 123£._
-0.021^
Gi_127e_
-0.1734.
- 0.2020
-0.0215
-Q.34Q?
0.0666
-0*3406
-0.340?
0.0793
- 0.0001
0.1136
0.1596
-0.2792
0.0210
- 0.2915
-0.2929
- 0.2020
0.0215
-0,3103
0.1008
-0.3460
-0.3103
0.0215
0.2919
-0.0764
-0.0005
0.0187
-0.3937
CHI- 15.00 GA^A= 1,5 2ETA=" 1.00 X/H= 0.
-0.0995
0.1029
0. 126J
-0.0676
...
0.3028
-0. 1811
0.1026
-0.3179
-0.2447
r 0. 2078
0.1707
-0. 1 533
-0.0912
-0.0326
0.1776
-0.0547
0.2254
- 0.1220
0. 1768
-0. 1743
0. 1437
-0.2461
-0.1743
0_. 1768
0. 1850
0.0535
0.2047
-0.0171
0. 1643
-0.0515
0. 2035
_-0. 1341
0.1132
-0.1528
-0. 134 1
0.20 3 5_
0.0839
-0. 1281
0.1573
-0.0896
-0.0219
0. 1291
0. 1830
-0.0168
0.0952
-0. 0043
0. 1819
_-0. 1247
0.0722
-0.0640
-0. 1247
0. 1819
-0.0014
-0. 1602
0.0857
-0.0701
- 0.00 22 '
-0.0074
0.1410
-0. 1276
0.0343
-0.1874
0.0272
-0.0272
-0.0000
0.3907
0.0026
-0.0026
0.0000
-0.0428
0. 1222
- 0. 1222
- 0 .
0.0426
- 0 . 1222
0. 1222
0.
6 ^ 1-1
L-15^9
111
TABLE 18.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.00, AND 7] = 0.75
(b) y/H = -1.125
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
r 1 ' 1 1
CHI— 3 *00 GAMMA* 1.5 ZE TA-
Y/H=-1 .12 If H* 0.
—
CM. LI
IU.L1
■ u n \
-0.4692
-0.0337
-0.5192
- 0 . jffi
— 0. 5164
0.3225
-0.4165
-0.0337
-0.4004
-0.0343
-0.5804
- 0 .;
-0.'
-o.<
—
l w « V 1
IU.D1
-0.3410
0,7187
0.4427
0.0659
0.1
-0.0688
0.0006
0.0792
-0.0003
0-0638
0.1448
CHI “ 3.00 GAMMA* 1.5 ZETA» 1-00 1 /H » Y/H— 1.12 Z/H* 0. ETA* 0.75
t W| U -0.4692 -0.3212 0.2 862
( U « L ) 0.0337 Q*J346 -Q«370J
I W » D ) -0.4748 -1.4736 0.0337
(U a 01 - <1.2432 0.25S4 0.4427
-0.4004 -0.2648
0.0343 -5.5311
-0.5377 0.0343
0.1245 {L.4Q.74
-0.0668 0.0 T92
-5. Q504l Q. 5503
0.0629 0.0641
-0,3676 0«JL3ifi_
CHI- 15. 00
GAMMA* 1.5
jC T|, t Qft
X/H* 0. Y/H*- 1 . 12
Z/H* Q. ......
XIA? _ 4,75. _
£t,IX i«UU —
IW.L )
1U.ll
ik.Di
CU.D )
-0.4344
0. 1597
-fl.2821
Q, 1 646
0.2617
-0.2643
-0. 3636
0. 1630
-0.2647
-0.4373
-0,0707
-0,0034
0,0815
0.0016
0. 1 598
-0.4373
0. 1630
0 . 0657
flm Q6%0
-0.0996
0.3042
0*79,92
0. 1983
0.3623
-0.2979
0.1058
—
CHI-30.00
GAMMA* 1.5
ZETA* 1.00
X/H* 0. T Y/H— 1,12
Z/H* 0.
ETA= 0.75
-
— • •—
(W.L)
CU.L )
LM.D)
CU.OI
-0. 3418
0.2680
-0, 175J
0.2795
0.2959 „
0,1411.
0.2AB3
-0.2645
0*2759.
-0.3184
-0.2028
-0.3184
Q.2759__
-0,0773
-0,0079
0,0690
0,0894 _
0.003IL
-0.0080
0.2926
0.2764
0*2147 _
0.2380
-0,2227
O.OIIf
CH 1*45. 00 GAMMA* 1.5 ZF.TA = 1.00 X/H* Q*_ Y/H?“i*12 Z/H* 0. ETA^ 0.75
1W,U
<U,LJ
< W ■ D )
1 U t D 1
-n.230 1
-0.0429
Q , 37 J 9
-0,1481
-0.1037
0.2911
0.3138
0,3068
-0.2376
-0, 1A44.
-0.1776
0.2917
-0.2376 -.
0.3068
0.0164
0.2253
0tl2H
0. 1728
0.0861
-0,0900
-0*0157
0.0732
-0.1564
0,1 wz
0.0010
0-0400
0*0524
*60.00
GAMMA* 1,5
ZETA* 1,00
X/H- 0. Y/H— 1.12
Z/H- 0,
ETA* 0,75
(H,L )
1U,L 1
IM.01
( U # D )
-0.1818
0.2290
_ n 1 itr
0.0636
0,2746
-0.1461
0.4474
-0.0196--
0.2298
-0,0702
0.2613
-0. 1986
-0-0086
-0.1906
0.2613
-0. 1 116
-0,0323
0.Q8Q8
0, !3»I
0.0133
V » 1 1 1 0 —
0.0128
0. 1376
0.0237
0,1085
-0.0234
-0,0957
— 0,02*1. _
CHI = 75.00 GAMMA* 1.5 ZETA-. 1.00 X/H» 0. 12 2/H?.. Q. .. ElAr_fii75
IW,L )
CU.LJ
(MtCI
(U,C>
-0.201<L
0. 1204
-o. Qg'n
0.0069
tf-1183 0.4947
0.21 58 - 0. QQ 34 .
-0. 1474 0. 1206
0.0573 -0.0016
-0,0632 _ 0 .0563
0.1934 - 0,1795
-0. 1795 0 . 1936
0.0480 -0.0403
-0 .1378 O. 1615
-0.0732 4*4222
0.0983 Q.Q321.
-0.0411 0.0093
C HI-9D.00 GA MMA* 1.5 ZETA* l.QQ X/H* Q. _ — Y/H»~U1 2 Z/H* 0. £IA? 0.L5
IH.L 1
tU.L )
IM.CX
MJ.D 1
-0.2247 0.1393
0.0273. 0.17 I3_
-JL. 02X3 -0- 1733
-0.0000 0..Q0ML
oISQ95 -0 .0942 0. 0942
0.0025 0, 1581 — - 0.1581
-0.0025 -0. 15ai flJiil
0.0 000 ^4*0004 . 0.0000
-0.1305
- 0.1309
P. 1308
-0.00QCL
0*2335
0 . 4152 __
0-Q131
112
TABLE 18. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1-00, AND t) = 0.75
(c) y/H = -0.75
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
GA^*a= I.S Z£ TA - 1.00 X/M= C.
Y/H=-0. 75 l /H= 0.
491 -0.77C8
306 -0,0567
559 -1.0050
P63 0.0544
0,1960
-0.0567
0.5677
-0.8613
0.0559
-n.PSPC
-n.2PEn
-0.6032
5 *_ 05 . 72 ...
-0.9065
0.2916
0.736?
-C. 7670
0.0559
0.6069
-0.77T8
0. 8567
-0.9455
0. 1566
0.0956
0.0390
0.1349
-0.7930
0.2619
—0.6907
-0.0044
7LIA- 1.0Q X/H-
-0.6099
— . 0.2691
-0.7451
0.4027
0.5R58
--Q.597Z.
0.2620
0.53 14
-0.70F2
P.?664
-0. 7R25
0.2926
-0.0179
-0.7B25_
0.2664
0.4914
-0.614 1
0.4247
— 0 .4672
0. 1074
-0. 1G39
Q*.4685„.
-0.3638
0.3215
0.5246
-0.3 735
0.4248
0.3342
-0. 5215
JL..4350 .
-0.5636
0.3310
Y/H=-0, 73 ZZR5 _(L
548 -0.3103
O.Q? 0.4561
359 -0,3946
191 Q.2633
-0.0467
-0.5636
0.4350
0.2911
0.1078
0. 0064
0.0349
0.0827
-0.3C51
0.3206
-0. 1P47
0.0561
0^3209
- 0.003 7
0,3623
- 0,0572
GA**A?_ US ZETA =
-C. 3053
0.1606
-0. 1090
0.0175
0.6425
0. 1603
-0.0109
-0 .2392
0, 0638_
0.2136
-0,0557
-0.3247
010273
-0. 0273
-9.000*
-0,1577
_ 0 1 1 96Q_
-0. 1960
- 0.0000
0.1577
- 0.1960 .
0.1960
0.0000
-0.Q SP1
O.Q OOP
L-15^9
8S
113
TABLE 18.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 1.00, AND 7] = 0.75
(d) y/H = -0.375
Correction factors for correcting from a wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CH I=- 3. 00
GAMMA* 1.5
7ETA* 1.C0 X/H=
C. Y/H=-C.i7
ll H = O.
ET A = 0.75
1M, LI
-1.4430
-1.2156
1.8873
-1.3353
1 . 1728
-O. 1078
HJ , L )
-0.0869
-0.0886
—1.4082
-0.9879
-1.60U
0.0010
iw.n
-1.5109
- 1.5592
-0.0P69
-1.6011
-0.0879
0.0902
IU,CI
-C. 3904
0.1967
0.7C99
0.0309
0.7*31
-0. *214
0. 119?
-0.0007
0.0*19
0.1657
. CHI- 3.00
GAHMA= 1.5
ZE T A = 1.00 X/H*
n. Y/H--0. 37
7/H* 0.
ETA- 0.75
(H,L )
-1.4430
-1.2156
1.6006
-1.3353
0.9055
-0. 1078
|U,U
0.0869
0.0806
- 1.3254
0.0879
-1.5232
-o.oolo
IW.OI
-1.4301
-1.4822
0.CC69
-1.5232
0.0079
0.0931
IU,CI
-0.1867
0.3*52
0.7099
0. 1947
0.7431
-0.381*
0.1197
0.0007
0 . 0*10
0.1505
CHI-15.00
GAMMA* 1.5
ZfTA* 1.00 X/H* c.
y/Hs-0.37
If H= 0.
ETA* 0.75
1 W » L 1
( U , L 1
( W . 0 )
IU,01
-1.3124
0.4009
-1.1657
0.1079
-1.0785
0.4097
-1.2246
0.5413
1.1532
-1.0583
0.4010
0.6710
-1.2017
0.4062
-1.2636
0.4184
0.4927
-1.26 36
0.4062
0.6233
-0.1108
-0.0053
0.0979
-0,3104
0. 1231
0.0035
0.0391
0. 1229
CHI*3Q- 00
GAMMA*. 1*5 ZETA* 1.00
X/H*
Y/H*-D«J37 Z/H = 0. . ETA* Q^75_ ..
1W.L J
-0,9826
-0.7269
0.8507
-0.8617
0.2248
-0.1209
(U.L)
(W, 0)
0.6201
0. 6406
-0.6668
0.6325
-0.8786
-0.012*
-0.7752
-0.8427
0.6204
-0.8786
0.6325
0.103*
(U.01
0.2452
0.5720
0. 3780
0.4793
0.3268
-0.23*2
0. 13*8
0.0081
0.0359
0.0926
CHI-45.00
GAM** A* 1.5
ZETA* 1.00 X/H*
C. Y/H
IW.L1
-0.6432
-0. 3445
0.7618
1U.L1
0.594 1
0.6343
-0.35*3
IH,0 1
-0.4604
-0.5399
0.5947
UJ,01
0. 1988
0.43 17
0.0962
37 Z/H* 0. ETA?. 0.75
-0.5025 0.1628 -0.1*07 0. 1579
0*6137 -0.5705 -0.02*6 0.0157
-0.5705 0.6107 0.1100 0.0305
0.3661 0.0393 -0.1673 0.0656
CH I *60. OQ
G AMM A = 1.5
ZETA* 1.00 X/H*
0. Y/H*-Q ■ 37
Z/H* 0.
ETA* 0.75
IW,U
-0.4536
-0.0799
0.7639
-0.2792
0. 18 39
-0.1744
tllfU
0.4083
0.4036
-0. 1682
0.4582
-0,3879
-0.0499
<W,DJ
-0.2663
-0. 3689
0.4091
-0.3879
0.4582
0.1216
1U.01
0.0972
0.2447
-0.0307
0.2038
-0.09 31
-0.1066
0.1993
0.0303
0.0190
0.0*08
CH 1*75.00 GAM*a= 1.5
ZETA* 1.00 X/H= C.
Y/H*-0. 37 1/ H* 0.
ETA* 0.75
IM.L)
<U,L )
i w ■ r i
( U , C 1
-P.43 14
0.0528
0. 7761
-0.2133
0.2060
-0.2181
0.2661
0. 1960
0, 3622
-0.0672
0.3055
-0.2907
-0,1095
0.0567
-0. 142P
-0.3010
0. 1962
-0.2907
0. 3055
0.1479
-0.0103
0.0260
0.0963
-0.0179
0.0775
-0.0691
-0.0508
0.0188
CH 1*90.00
C AMM A = 1.5
ZETA* 1.00 X/H*
0. Y/H
{ W , L 1
-0.4465
0.1267
0.7799
(U,L 1
0.C273
0.3040
0.0025
t W #E )
-0.0273
-0.3048
-0.0025
IU»C )
-0.0000
0.0000
0.0000
If H= 0. ETA ? 0.75
-0.2150 0.2150 -0.2316 0.3*16
0.2267 -0.2267 -0.1993 Q.Q761
-0,2267 0.2267 0.1993 -0.0781
- 0.0000 0.0000 - 0.0000 0.0000
11 *
TABLE 18.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5 r £ = 1.00, AND rj = 0.75
(e) y/H = 0
Correction factors for
correcting from
a wind tunnel
which is
closed
closed floor
open
ciosed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to groui
id effect
i
—
CHI — 3.00
GAMMA- 1.5
ZETA- 1.00
X/H= 0
. Y/H* 0.
Z/H- 0.
ETA- 0.75
(W,L)
HUl)
IWtOl
fU.01
-1.6023
-0.10*6
-1.07*0
-0. **69
-1.5181
-0. 1065
-1.8699
0.2119
2.6091
-1.7253
-0. 10*7
0.0885
-1.6633
-0. 1058
-1.9455
0.01*3
1.8760
-1.9*55
-0. 1050
0.8305
-0. 1390
0.0012
0.0715
-0.4612
0. 1*52
-0.0007
0.0756
0.1976
CHI* 3.00
GAMMA- 1.5
ZETA-
1.00
X/H* 0
. Y/H- 0.
Z/H- 0.
ETA- 0.75
(M.U
tu.u
( W,D)
IU,D>
-1.8023
0.10*6
-1.78*9
-0.2039
-1.5181
0.1065
-1.7826
0.3929
2. 1896
-1.6322
0. 1047
0.8865
-1.6633
0 . 10S8
-1.8585
0.2136
1.4767
-1.8585
0. 1058
0.8305
-0.1390
-0.0012
0.0736
-0.4176
0. 1*52
0.0007
0.0759
0.1792
ch^is.oo
CAMKA-_ 1.5
ZETA-
1.00
X/H- 0
. Y/H- 0.
Z/H- 0.
ETA- 0.75
IM V U
t U*L )
(W,0)
(U*D)
-1.6285
0.*790
- 1 . *60*
0.1505
-1.3363
0.488*
-1.4623
0.6343
1.5155
-1.302S
0.4796
0.7434
-1.4857
0.48*9
-1.5379
0.4890
0.8371
-1.5379
0.4649
0.6841
-0.1*29
-0.0059
0.0775
-0. 3385
0.1*9*
0.0035
0.0756
0. 1*53
CHI-30,00
GAMMA* 1.5
ZETA*
1.00
X/H* 0
. Y/H- 0.
Z/H- 0.
ETA* 0.75
(W'L)
iu,i)
1N.0)
(U,0)
- 1.200*
0.7221
-0.9630
0.30**
-0.6010
0.7440
-0.9730
0.666 1
1.0323
-0.8034
0.7235
0.3999
-1.04*5
0.7359
-1.0*60
0.558*
0. 3879
-1.0*60
0.7359
0.3360
-0.1559
-0.0138
0.0830
-0.25*0
0.163*
0.0081
0.0730
0. 1077
CH|-«*00
GAMMA- 1.5
ZETA-
1.00
X/H* 0
y/h- o.
Z/H- 0.
ETA- 0.75
>
..UliLl
IW*D)
fU»0)
-0.7782
0.6687
-0.5635
0.2365
-0.4057
0.7113
-0.5883
0.4898
0.8613
-0.4004
0.6710
0.0894
-0.5968
0.6957
-0.6548
0.4160
0.2*22
-0.6548
0.6957
0.0205
-0.1813
-0.0270
0.0912
-0.1795
0. 191 1
0.0156
0.0665
0.0737
CHI-60.00
GAMMA- 1.5
ZETA-
1.00
X/H* 0. V/H- 0.
Z/H- 0.
ETA- 0.75
(W.L)
IU.LJ
CM, 01
!U V 0)
-0.5527
0.**5*
-0.3210
0.1121
-0.0879
0.5292
-0.3773
0.2675
0.8332
-0.1814
0.4487
-0.0363
-0.3283
0.4996
-0.4283
0.2245
0.2303
-0.4283
0.4996
-0. 1094
-0.22*5
-0.05*3
0.1073
-0. 1 12*
0.2*03
0.0296
0.0510
0.0*30
CH 1-75. 00
GAMMA* 1.5
ZETA*
1.00
X/H- 0.
Y/H- 0.
Z/H- 0.
ETA- 0.75
01*1.1
(Ut t )
111,01
1U,0>
-0.5261
0.2096
-0.1682
0.0302
0.0730
0.3795
-0.2989
0.1010
0.0353
-0.0675
0.2121
-0.0180
-0.2452
0.3265
-0.3117
0.0831
0.2378
-0.3117
0.3265
-0.07*6
-0.2809
-0.1170
0. 1*35
-0.0529
0.3182
0.0529
0.0128
0.0178
CHI-90.00
GAMMA- 1.5
ZETA-
1.00
X/H- 0.
Y/H- 0.
Z/H- 0. ETA- 0.75
(N,L)
IU.LJ
IU.D)
«U,01
-0.5*2*
0.0273
-0.0273
-0.0000
0.1653
0.3080
-0.3080
0.0000
0.8367
0.0024
-0.002*
0.0000
-0.2387
0.2387
-0.2387
0.0000
0.2387
-0.2387
0.2387
-0.0000
-0.3036
-0.211*
0.211*
- 0.0000
0.40*1
0.0693
-0.0693
0.0000
6 ^ 1 -'!
L-15^9
115
TABLE 18. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR ? = 1.5, C = 100, AND tj = 0.75
(f) y/H = 0.375
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
r- 1
to ground effect
CHI — 3.00
GAFHA* 1.5
ZET A* 1.00
X/H* 0. I/H*.i«37.
Z/H= 0.
ETA* 0.75
( W « L )
-1.5187
-0.0866
-1.5845
-0.5021
-1.1581
-0.0885
-1.4487
0.2876
1.8627
-1 . 3345
-1.3353
-0.0879
1.1728
-1.6011
-0.1634
0.0013
0. 1772
-0.0006
(W,0>
(U, D 1
-0.0871
0.8244
-1.6011
0.0309
-0.0879
0.7431
0.0166
-0.5331
0.1524
0.2567
__CHI-_.3-0P
GAHHA* 1.5
ZETA* 1.00
X/H= 0. V/H* 0.37
Z/H* O.
ETA* 0.75
-1.3353
0.0879
0.9055
-1.5232
-0. 1634
-0.0013
n 1 770
I M* L )
(U.LJ
(W.Dl
-1.5187
0.0866
— 1 . 1581
0.0885
1.5780
-1.2481
0* If u
0.0006
-1.5074
-1.3670
0.0R71
-1.5232
0.0879
0.0158
-0.4824
0.1562
0.2323
(U.D)
-0.2878
0.4270
0. 82 44
0. 1947
0.7431
—
—
CHI* 15* 00 G AWHA* 1.5 ZETA* 1.00 X/H* 0. Y/H- 0.37 Z/H= 0.
ETA- 0.75
14. LI
-1.39Q1
-1.0195
1 . 1360-
-1.2017
0.4927
(1. 5997
-0.9764
0.4062
-1-2636
i**m_
IU»0J_
- 1-2476
-1.1028
0,4023
-1.2636
0,4062
Q.Q2I9
0. 6 048
0,7057
0.4184
0.6233
-0.1865
-0.0066
0.0160
-0.3905_
0. 1821
0.0032
0. 1608
0. 1865
CHI -30.00 GAHHA- 1.5 IEIAj 1.QQ, X/H- Q. Y/H* 0.31 ZZTi.=__Q_. — LI A- 0.70
f 4 ■ L )
-1,0672
-0,6627
0,8410
-0,3617
(UtL 1
0.6174
0.6398
-fi.5836
■ 0,6325
(4.0)
rP,J3fi5
-OJjeo
0.6230
-0.8786
(U.Ol
0, 1902
0*_6 1 32
0.4130
.0,4793
0,221.8 -0.2055 0. 1989
-0.B786 -0.0 1 5 1 * JML0I1
0*6325 0.0201 0.1606
0.3268 -0.2892 0.1338
CHI*45.Q0 GW!»A*_J,5 .... ILIA? 1.00 JL/h- (L.
_Y/H=_Q._3T Ui 1- 0.
ETA= _D.75„
<N,L)
(UtL 1
IW.Ol
(U,D)
1M.U
iua>
1H.01
<U,D)
-0.7408
(L5S9JL
-0.5393
0.1672
-0 .27Q7
Q.J607
-0.27S4
-0.4182
0.4516
0.5791
0.1302
-0,5025
■0.6161-
-0.S705
0.3661
0.1628
-0. 5705
0.6187
0.0393
-0.2383
-0.0290
0,0311
-0,1989
GAHHA- 1.5 ZETA = 1.00- _X7H= 0,
_1/H= 0.37 l /_Hr 0.
ETA= Oa7_5._
-0.5725
0.4023
-0.3320
0.0652
0.0098
0*4806
-0.2587
0.2466
0.7729
-0.1025
0.4152
-0.0035
-0.2792
0.4582
-0. 3879
0.2038
CHI-75,.00 G_AHHA»1.5 ZETA* 1,00 X/H- 0.
Y/H= 0.37 Z/H=_ 0.
(W*L>
IU,L 1
I W * D 1
(U.D)
-0.5767
0.1906
-0.1617
0.0250
0. 1626
0,3368
-0.2141
0.0097
0.791*9
-0.0283
0.2013
-0.0077
-0.2133
. 0, 3055__
-0.2907
0.0775
0.1839
-0. 3879 .
0.458?
-0.0931
_E.TA*_.0W5_
0.2060
-0,2?O7_
0.3055
-0.0691
-0,2933
-0.0560
0.0558
-0. 1107
-0.3634
^0,1.1 4 7. _
0.1090
-0.0525
0.2318
0.0132
0. 1522
0.0855
0.2891
0.0224
0.1292
0.0428
0.3760
0.031 4
0. 0766
0.0122
CHI-90.00
<W,L)
IU.L1
<H,D>
_ < U . P J
GAMHA* 1.5 ZETA= 1.00
-0.6038
0.0273
-0.0273
-0.0000
0.2488
0.2492
-0.2492
0.0000
0.8029
0.0024
-0.0024
0.0000
_Z/H* 0
-0.2150
0.2267
-0.2267
-0, OOQQ__
ETA*_0.75
0.2150
-0,2267
0.2267
JQ,QQ01L
-0.3889
-Q_. |9?4 .
0. 1994
rO. 0000
0.4637
0.0225
-0.0225
0.0000
ll6
TABLE 18.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 1.00, AND rj * 0.75
(g) y/H = 0.75
Correction factors for
correcting from o wind tunnel which is
closed
closed floor
open
closed
B
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to grour
id effect
CHI — 3.00 GAM
MA*. 1.5 ZE T A =
l.QQ X/H* 0
1 1
. Y/H= Q, 75 _ Z/H* o .
LT A= 0.75
( H , L 1
- 1.0508
-0.5357
0.7616
-0.7780
0.1960
-0.2720
0.2431
U/.U
-0.0547
-0.0578 ...
-Q.M23
-0,0567
- 1*0050
0020
-0.0011
1 W, C 1
-1. 1034
-0.71 IQ
-0.0570
-1.0050
-0.0567
-0.0984
0.2940
!U,D >
-0.6236
0.4364
0.7120
0.0544
0.5677
-C.6780
0. 3820
CHI* _3. OQ GAMMA* 1,5 ZETA-
l.QQ X/H* 0
. . Y/H* 0.75 Z/H* 0.
ETA* C . 75
(W,L)
-1.0508
-0.5357
0.6590
-0.7788
0. 1019
-0.2720
0.2431
(UfJ-i
0.0547
0,0578
-0.5726
0.0567
-0.9455
-0.0020
0. 001 1
1 W,D1
-1.0524
-0.6390
0.0570
-0.9455
0.0567
-0.1C68
0. 3065
IU.DI
-0.4577
0^5027
0.7120
0,1566
0.5677
-C.6143
0^3461
- _OAHJ
1ft- 1.5 Z£IA=
1.00 X/H* 0
Y/H* 0.75
Z/H* 0.
ETA* 0,75
( W.L 1
-0.9875
-0.4584
0.5286
-0.7082
-0.0178
-0.2793
0.2498
_
-XLULJ
0.2561
0.2719
-C. 38 90
0.2664
-0.7025
-0.0103
6.0055
(¥.01
-0.8994
-0.4596
0.2679
-0. 7825
0.2664
-0. 1 169
0.3229
-0.2027
0.5684
0.6366
0.2926
0.4914
-0.4954
0.2757
JEm?3QtPP KS 2ETA 3 1.00 X/H = 0, Y/H* 0.7 5 Z / H * 0. ETA* 0.75
(W*U -0.8251 -0.2494 0.4961 -0.5215 -0.0467 -0.3039 0.2T21
. J-Uj-L 1 Q.4 124 0.4465 -0. 1606 0,4350 -0.5 636 -0.0226 Q*PUL5_
IHiQ) ”0-68j31_ -0.2 3 56 0.4372 -0.5636 0.4350 -0.1165 ~ 0.3280
1U.DJ -Q.029! __ 0.5228 0.4378 0.3310 0.291 1 -0.3602 0. 1918
£H 1*45,00 QAHHA* 1,5 ZETA* 1.00 X/H* 0 . Y /H* 0 . 75 Z/H* 0. ETA* 0.75
(W.L)
-0.6611
0.0045
0.5588
-0. 3103
0.0094
-0.3508
0.3149
tU.L)
.. .0-4.162 . ..
0.4737
-0.0010
0.4561
-0.3946
-0.0399
0.0176
( HjJD 1
-0.4929
-0.0807
6.4554
-0.3946
0.4561
-6.0983
0.3139
(U,D)
0.0251
0.3770
0.215 1
0.2633
0.0710
-0.2382
0. 1137
CH1»6Q.0Q GAMMA* 1.5 ZETA* I.OO" X/H* 0. Y/H* 0.75 Z/H* 0.
CK«L> -0.5983 6 .2146" 0.^475’ -0.1715
IUaU 0.2959 0.3820 0.0645 0.362 3
. IH .PI -0.3478 -0. 0227 0.3455 -0.2950
CU.PI 0.0246 0.2033 0.0677 0. 1567
ETA* 6.75
0.0831 -0.4268
-6.2950 -0.0664
0.3623 -0.0528
-0.0572 -0.1321
0.3861
Q.P1 96
0.2723
0.0466
GAMMA* 1,5
ZETA* 1.Q0 X/H*
0. Y/H*
0.75 Z/H* 0.
ETA* 0.75
—
(W.L)
-0.6575
0.3455
0.7132
-0.1395
0- 1323
-0.5180
o
in
K
*
O
(U.L1
0.1414
0,2349
0,0535
0.2536
-0.2392
-0.1123
0.0012
IH.D)
-0.2033
-0.0503
0. 1795
-0.2392
0.2536
0.0359
0.1888
IU f D)
0.01 17
0.0680
6.0140
0.0638
-0.0557
-0.0521
0.0041
CH I *90, 00 GAMMA* 1 ,5 ZETA* 1.00 X/H* CL ~ Y/H* 0.7 5
(W.U -0.7029 0.4108 0 .73 64
(U.L) 0.0272 0.1382 0.0024
1H.D1 -0.0272 -0^1382 -0.0024
IU*D 1 -0.0000 0.0000 0.0000
Z/H- 0. ETA* 0.75
-0- V577 0.1577 -0. 5452 0. 5685
0.1960 -0.1960 -0.1687 -0.0578
-0. I960 0,1960 0.1687 Q.057JL _
-Q.QQQQ 0.0000 -0.0000 0.0000
6^i-i
L-15^9
117
TABLE 19
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 2.00, AND i] = 0.75
(a) y/H = -1.50
Correction foctors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free oir
to ground effect
— 3.00
G A W P A = 1.5
7 E T A = 2.00 X/H =
0, Y/H*-!
1.50 Z /H* 0.
ETA= 0.75
1 w, L 1
-0.0940
-0.0609
-0.2393
-0.0T75
-C.7P20
-0.0173
(U,l)
-0.0225
-0.0224
-0. 1647
-0.0225
-0.2619
-0.0000
( vi v n )
-0.2697
-0.1882
nQ. 0224
-0.2619
-0 ,0225
-O.QO70
(U,01
-0.0435
0.2661
0.3964
0. 1749
0. 3902
-0.2184
0.0167
0.0001
0.0738
0.0912
CHI= 3.00 G AP M A = 1.5 /ETA= 2.00 X/H® 0. Y/H=-1.50 Z/H= 0. ETA= 0.75
(W,L1
-0.0948
-0.0609
-0.2307
-0.0775
-0.7643
-6.0173
0.0167
(U,L 1
0.0225
0.0224
-0.1231
0.0225
-0.2210
0.0000
-0.0001
( W,D 1
-''.2291
-0. lAfcB. _ ...
0.0224
-0.2210
- Q*_&225
-0,0080
Q,Q7<L3
( U f D J
0.0036
0.2823
0.3964
0.2003
0.3902
-0.1967
0.0820
CHI= 15.00
GAPPA* 1.5
ZET A= 2.00 X/H =
0. Y/H
( H, L >
-0.0706
-6.0355
-0.1002
1 U , L )
0. 1079
0.1075
-0.0431
1W.0)
-0. 15fl.4_.
-0.0670
0. 1073
(U,D)
0.0604
0.2847
0. 3605
7 /H = 0. ETA= 0.75
-0.0527 -0.7058 -0.0179 0.0172
0.1078 -0.1420 0.0001 -0.0003
-0.14.2fl 0,1078 _ -0.0084 0.0750
0.2189 0.3621 -0.1585 0.0657
CH[=30.0D
GAPPA= 1.5 ZE TA =
2.00
I W, L I
~6”.6t)32
0.0357
(U, L 1
0. 10PO
0.1870
t w. p > ...
-0.0151
tu,ni
0.0745
0.2407
Y/Ha-1.50 Z/H= 0. E T A= 0.75
-0.09 39 0.0166 -0.594 4
0.0723 0.1878 -0.0673
0.1067 -0 .0673 0.1878
0.2P8P 0.1925 0.2818
-0.0198
0.0002
-0,0006
-0. 1180
0.0191
-0.0008
0,0755
0.0481
CH I = 45. 00 GAPPA* 1.5
ZETA = 2.00 X/M= C.
Y/H— 1.50 Z/H= 0. ET A = 0.75
(W,l> 0.0814
(U,l) 0.2210
tw,D -0,0469
(U,C) 0.0512
0.1205 C.0274
0.2109 0.0614
0.C372 C.2101
0.1662 0.1793
0.1054 -0.4578
0.2205 -0.0384
-0.0384 0.2205
0. 1 338 0.1710
-0.0239
0.0005
-IL0055
-0. 0825
0.0231
-0.0016
0.0756.
0.0324
=60.00
GAMP A= 1.5 ZE T A =
2.00 X/H= C
Y/H*— '
1.50 Z/H= C.
EIA- 0.15
(W|l)
0. 1448
0.2090
0.1493
0.1774
-0.3212
-0.0326
0.0316
(U.L)
0.2034
0.1986
0.0300
0.2024
-0.0606
0.0010
-0.0038
( W , D )
-0.0604
0.0145
0. 1969
-0.0606
0,2024
„ _tQ*Q0IS
0.0750
( u, r >
0.0234
0.0904
0.0697
0.0732
0.0591
-0.0497
0.0173
[ = 75.00
GAPP A = 1.5
7 f T A =
2.00
X/H= 0
. Y/H=-
1.50
Z/H= 0.
ETA= 0.75
( W,L )
0. 1332
0.2309
0.2473
0.1865
-0.2063
-0.0534
0.0523
(U.L)
C. 1607
0. 1468
-0.0196
0.1508
-0. 1164
0.0019
-0.0120
( d, C )
-0.1213
-0.0443
0.1410
-0. 1164
0. 1588
-0.0040
0.0722
<U,C)
0.0156
C . C 363
-0.0005
0.0340
-0.0137
-0.0183
0.0023
=90.00
GAPP A= 1.5
ZC T A =
2. CO
X/H* 0.
■ _ y/h=-i
1.50
7 / H= 0.
ETA= 0.75
t W,L 1
0.025?
0.2126
0.3114
Cull 30
-0. 1130
— 0. 0878~
11.0996
1 U , L )
0. 1536
0. 1056
-0.0782
0. 1630
-0. 1630
-0.0093
-0.0574
IW.tU
-r. 1536
-0.1056
0.0782
^0.1630
0. 1630
0,0093
Q*Q5I5l
(U,0)
-0.0000
0.0000
0.0000
-0.0000
0.0000
-0.000D
0.0000
118
TABLE 19.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5 f C = 2-00, AND r\ = 0.75
<b) y/H = -1.125
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
ciosed
on bottom
open
only
floor
ciosed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00
GAHHA* 1,5
ZETA* 2.00
X/H= 0. Y/H*- 1
.12
Z/H* 0.
ETA* 0.75
I Uf L )
-0.2419
-0.2175
-0.5924
-0.2300
-1.1363
-0.0120
0.0125
|U,l)
-0.0400
-0.0400
-0.4574
-0.0400
-0.5450
0.0000
O.OOQO
-0.5259
-0.5007
-0.C399
-0,5450
-0.0400
0,01.9!
0.0443
(U,D)
0.0285
0.2979
C.6452
0.2240
0 . 6408
-0. 1955
0.0738
CHI- 3.00 _
GAHHA- 1.5_
ZETA* 2.00
X/H* 0. Y/H--1
.12
Z/H* 0.
ETA* 0.75
tUtLL
-0.2419
-0.2175
-0.574 1
-0.2300
-1.1092
-0.012Q
0.0125
(U.L 1
0,04fifi
0.0400
—0.3098
0.0400
-0.4779
-0.0000
-0.0000
{ w. n )
-0.4587
-0.4333
0.0399
-Q.4779
0.0400
0.0191
. ft. 0445
IU.0I
0 f 1 0 1.6
0.3441
0.6452
0.2776
0.6408
-0. 1761
0.0665
CHI* 1 5. 00
GAMMA* 1.5
TjEJA* 2.00
X/M* C. Y/H=-l
t.12
Z/H* 0.
ETA* 0.75
(Wall
-0.2006
-0.1754
-0.4941
-0. 1883
-1.0138
-0.0124
0.0129
( U a L 1
0.1915
0.1914
-0.2559
0. 1916
-0.3447
-0.0001
-0.0001
IH.D1
-0.3255
-0.2999
0.1912
-0. 3447
0.1916
0.0 192.
0.0448
(U f D 1
0.1869
0.3025
0.5948
0.3290
0.5902
-0.1422
0.0535
CHI-30.00
GAHHA- 1.5
ZETA* 2.00
X/H* 0. Y/H— 1
1 . 12
Z/H* 0.
ETA* 0.75
(H»L1
-0.0871
-0.0591
-0.3236
-0.0734
-0.0272
-0.0137
0.0143
IU.t )
0.3336
0.3335
-0. 1256
0. 3338
-0.2149
-0.0002
-0.0003
<W.D)
-0. 1956
-0.1699
0.3729
-0.2149
0.333e
0.0193
P.Q45D
(Uf 0)
0.1991
0. 3450
C.45 10
0.3055
0.4459
-0.1064
0.0396
CHI* 45.00
GAHHA-K5
ZETA- 2.00
X/H* 0. Y/H—]
1.12
Z/H* 0.
ETA* 0.75
Tw.l 1
0.0522
~~ 0.0862
TO. Yoe 0 “
0.0688
-0.5975
-0.0166
0.0174
(U,l >
0.3919
0.3910
-0.0690
0.3924
-0.1586
-0.0005
-0.0005
( u t D1
-0. 1392
-0. 1136
0.3904
-0.1586
0.3924
. 0.0194
0*0450
(Ufbt
0.1486
0.2510
0.2545
0.22 38
6.2485
-0.0752
0.0272
CHI-60. 00^^
GAHHA- 1.5
Z.EJA* . 2.00
1.12
Z/H- 0.
ETA* 0.75
-
i u.u _7L
0.1494
OJ.96 1_
0.1053
0, 1722 ...
-C. 3709
-0,0228
0.0239
(UaL)
0. 3A 12
0.3612
-0.0911
0.3624
-0.1Q06_
-0.00 12__
-0. 0013
ty.p 1
-0.1608
-0. 1.359
0.3579
0.3624
IM11SS
__ 0.0447
lU.OI
0,Q875_
0. 1498
0,0653
0.1342
0.Q574
-0.0467
0.0156
ZETA* 2.00
~K/H» 0. Y/H*-
1.12
Z/H* 0.
ETA- 0.75
( WfL )
0. 1262
0.2046
0.2753 . .. .
0.1641
-0,1 BTJ
. -0.0379
0.04Q5.
(Utl. )
0.2866
0.2869
-SLJL54 3
0.2913
-0.2429
-0.0047
-0.0043
(W.D1
-0.2214
-0.1999
0.2758
-0.2429 ..
Q a 291 3
0*0215
0.0430
UI*0L
0.0475
0.0708
-0.0313
0.0668
-Ot 0422
-0,0193
0.0040
GAHHA* 1,5
ZETA- 2.00
X/H- 0. Y/H*-
1.12
Z/H- 0.
FTA» 0.75
\
-0.0140
0* 1320
0.3919
0.0494
-0.0494
-0.0634
0.0825
(U»L 1
0.2490
0.2^i8IZ
-0.1971
Q.2SOO_
-0.2800
-0.0310
-O.D32fi^
-n.?490
-0.2480
0.1971
-0.2RQQ __
Q.2BQQ
0. 03 1 Q
0.0320
cu.m
-0.0000
0.0000
0.0000
-(KQ fiftO
o.oooo
-0.0000
0.0000
6 ^ 1-1
L-15^9
119
TABLE 19.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1*5, C 2.00, AND tj
(c) y/H = -0.75
8
Correction factors for correcting from o wind tunnel which is
— — —
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
. > '
i
2JIQ.
XZR* Q, Y/h*-0.75
ETA= 0,75
chi— j.oo
GAHP&- 1.5
ZE TA-
1 1 H - 0 « .
IW.Ll
(till)
( U t D )
CU.D)
-0.8229
-0.0*59 ....
-1.3320
0.0771
—
-0.7986
-(Ltcaii
-1.3312
Q. 331 I
-0.8231
1,2 73.7 _
-0.0858
1. 1720
-0.P1 12
-0,0359..
-1. 36 34
0.2665
-1.3944
- 1 • 36 14_ _.
-0.0859
1.1676
-0.0116
G.Q000
0.0314
-0.1894
0.0126
O.QOQQ .
0.0322
0.0707
Cm--3~0tL
(H*L 1
y/H- n .
FTA= 0 . 75_._
-C. 8229
-0.7986
-0.8218
-0.8112
-1.3839
-0.0116
0.0126
n. nn59
-1 . 150R
.£1.2259
. ...-JL.24 IQ.
-Q.QQQQ
-0, QOQQ
1W.D1
(Ut D)
- 1.2095
0 .212*1
-1*20.87
0.4667
0.0858
1 . 1720
-1.2410
0.4030
0.0B59
1.1676
0.0316
-0.1706
0.0323
0.0637
■ “
_.£I A- Q.Z5 . . ...
rui.ic nn
IFTI*
2.00
xvhx n. y/H=-Q.75_
11W3 0.
-0.7243
0.41Q2
-1.2715
-0.97Q8. ...
-0.0120
-Q.Q0.O2.
0.0130
..tO.QQQO
IH.L1 ...
-0. 736*1
0.* 100
-0.7 LI 3
0-4102
-0. 7254 _ .
. . -0.B879
IK ( D1
-0.9470
-0.9463
0.4098
-0.9788
0,4102
0.0318
0.0324
0.0513
LU.D1
Q.424S_
0.6140
1.0609
0,5627
1.0564
-0. I 379
CAMf 1.5 -
2FTA* 2. QQ _
1 i H* 0.
£TA= C..75
(H.U
... _iU.L>
t W.C 1
(U,D)
-0.5015
-0.4737
0.7073
-0.4555
-0.6056
-0.4821
_Q,T073
-0.9846
-0,69.7 1
-0.0134
-0.0004
0.0145
-O.QQflQ—
-0.6651
0.4716
-0.6646
0.6131
C. 7064
0.7433
-0.6971 .....
0.574?
0.7C73
0.74 34
0.0320
-0. 1033
0.0325
0.0382
CHL*45.QO
7F TA*
2.00
X/H* 0. Y/H—Q.75_
Z/H*~Q.
_LIA-_C.Z5
-0.0162
-D.Q_Q.Q9
0.0176
-O.QOOl
1H.L1
1U.U
1 H i 0 1
1U.C1
-0.2223
Q.,8L3J_
-0. 1885
0.8140
-0.0966
-0.4446
-0.2061
0.8141
-0.61 12
. -0.5364...
-0.5041_
0.3795
--
-0.5039
0.4794
0.8121
0.34 15
-0.5364
0.4529
0.8141
0.3356
0.0322
-0.0734
0.0324
0.0265
CHI -60-00
_ GA 1,5
ZETA*
2.00
X/H= 0, Y /H=-0. 75
Z /H= 0a ..
ETA- 0,15
( W,L 1
(U . L 1
(H,D)
(U,D)
-0.0394
0.7252
-0.4663
0.2430
0.0069
0,7272
-0.4668
0.3047
0.24U9
-0.4070.
-0.0173
0.727*1
-0.2562
-0.4989
-0.0222
0.0242
-Q.Q002
0.7227
C.002 1
-O. 49R9
0.2890
0.7274
-0.0058
0.0326
-0.0460
0.0321
0.0157
CH 1*75- 00
(M.U
III . L 1
1H.0I
lU.0 1 .
C AMM A= 1.5
-0.0666
0.5564
-0.4762
C. 1 172
ZE TA =
?.ca ....
0.0116
0.5632
-0.4797
0.1420
X/H* Q, Y/H=-0.75
It H* 0,_
ETA* fl,15 ... _ _
Q.4913
-0.0296
O.OQ33
-O.Q371
0.0411
-0.4188
0.54PO
-0.0969
0.5642
-0.5103
0.1370
-0.5103
0.5642
-0. 1Q80
-0.0078
0.0341
-0.0199
-0.0009
0.0306
0,0049
CH 1-90. 00
( H , L 1
i |i _ t )
6AWF. A* 1.5.
-0.2333
0.4458
-0,4458
-0.0000
ZE TA*
2.00
X/H 3 0. Y/H=-0.75
Z/H= 0.
ETA* 0,7.5
- ...
■ ■
-0.0868
0.4692
0.64 16
-0.4006
-0.1711
0.4889
0.1711
-0,4889
-0.0621
-0.Q431
0.0844
-0.0197 .
. LUjU..
IHiDl
(U.P)
-0.4692
0.0000
0.4006
-0.0000
-0.4889
-0.
0.4809
0.
0.0431
-0.0000
0-0197
0.0000
120
TABLE 19.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5* ? = 2.00, AND i) = 0.75
(d) y/H = -0.375
Correction factors for correcting from a wind tunnel which is
closed
on bottom
to free air
closed
on bottom
only
to ground effect
-1.1298
-0.2268
-3.9888
0.0209
-3.0999
-0.2268
-3.9841
0.2965
1.3979
-3.9203
-0.2 268
2.2759
- 3.1152
-0.2269
-4. 0201
0.2177
0.7841
-4.0201
-0.2269
2.2706
-3. 1298
0.2268
-3.7507
0.4493
-3.0999
0.2268
-3.7460
0.6975
1.0113
-3.6618
0.2268
2.2759
-3. 1152
0.2 269
-3.7821
0.6266
_£TA_*_ 0.75
0.4077
-3.7821
0.2269
2.2706
-2.8170
1 . 0654_
-3.0936
1.2276
-0.0150
-OtOQQ I
0.0316
-0.1432
-0.0167
-0.0004
0.0318
-0. 1072
- 1.2200
1.6243
-1.5422
1.0824
-1.2413
La_ 82 jtA
-1.5785
1.0530
0.0377
-1 . 579 5
1.8244
0.2839
- 0.0202
----Q..Q009
0.0320
-0.0760
-1.1 474
0.5 793
2.0Q. _ X/Hf 0*
-0.6567
1.4490
-1.1441
0.6439
0.8686
-1 . 0777
1.4438
-0.2193
Y/H=-0,37. Z /H- 0 .
-0.6860
1*4494 _
-1. 1800
0.6267
0.0358
0.0172
CHI-75. 00 CAMHA= 1.5 ZETA« 2.00 X/H= 0. Y/H=-0.37 Z/H= 0.
[JULL_ ---0.6039 -0.5085 1.0511 -0.5580
1 . 0 066 1.C131 .... , . -Q..E55Q 1.0146
t Q. 9 222 -0.9228 0.9958 -0.9566
(U.Di 0.2352 0.2605 -0.2099 0.2554
U0146
-0 .2228
0.0345 ...
- 0.0202
O. 033*
0.0Q5I
CHI*9Q. 00. GAHMA-1.5 ZETA= 2 .Q 0 V/ H»-n.X 7
-0.7077
0.7380
-0.7380
- 0.0000
-0.7839
-D.QQQO
L-15^9
121
TABLE 19. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND rj = 0.75
(e) y/H = 0
Correction factors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CH J*-3. 00 GAHYA* 1.5 ZF T A* 2. CO X/H* 0.
7/H* 0. ETA* C.75
(W.L )
-6.6748
-6,6316
8. 175G
-6.6532
l U # L )
-0.4230
-0.4232
-7.6624
-C. 4232
( w»r )
-7.7675
-7.7229
-C.4229
-7. 7822
(U»C)
-C. 1653
0.1595
3. 3304
0.0572
7.5039
-7.7822
-C - 42 32
. 322 1
-0.0216
0.0001
0.0147
-0.2224
0.0216
-o.oaoo
0.0593
0. 1023
CHI* 3.00 CAMYA*
ZETA* 2. CO X/H= 0. Y/H = 0. If H= 0.
ET ' =
0.75
(H, L )
-6 .6748
-6.6316
6.5669
-6.6532
r .9069
-0.C216
(U.L)
0.4230
0.4232
-7. 3134
C.4232
-7.4340
-0.0001
IW,C)
-7.4193
-7.3743
C. 4229
-7.4340
C.4232
C.0146
(U.D)
C.654 1
0.946C
3.3304
0.8546
7 . 322 1
-0.2005
0.0216
0.0000
0.0597
0. 0922
CHI* 1 5 • 00
GAMMA* 1.5
ZETA* 2.00 X/H*
0. Y/H- C.
Z /It* 0.
ET A * 0.75
1 W » L )
(U.L1
(H.Dl
(U.D)
-5.9649
1.9396
-6. 1 371
1.7959
-5.9203
1.9394
-6.0914
2.0286
3.9880
-6.0298
1.9790
2. 7444
-5.9426
1.9396
-6.1516
1 . 9559
3 . 34 25
-6.1516
1 .9396
2.7366
-0.0223
-0.0001
0.0145
-0. 1599
0.0223
- 0.0002
0.0602
0.0727
C H I* 30- OC GAMMA* 1,5
ZETA* ?. CO X/H = Om.
Y/H* 0.
Z/H*
0.
e r a =
C.75
( W,L 1
1 U i L )
(W,D1
( U , D )
-4.2026
2.9435
-4. 1696
2.1144
-4. 1531
2.9431
-4.1235
2.2872
2.1695
-4.0 MS
2.9421
1.3559
-4. 1778
2.94 36
-4. 1^41
2.2337
1.5518
-4.1841
2. 94 36
1.3473
-C.0248
-C.000 1
0.0145
-0. 1 193
0.0248
-0.0005
0.0605
0.0535
CH J*45. 00
GAMMA* 1.5
ZETA* 2.00 X/H* 0.
Y/H* 0.
U M* 0.
E T A = C.75
(W,L)
(U.L)
( W.D)
(U.D)
-2.4173
2.7826
-2.6043
1.5004
-2.3574
2.7819
-2.5585
1.70C5
1.5676
- 2 . 4 9 6 c
2.7797
0.0921
-2. 3873
2. 7*29
-2.6190
1 . 664 1
C .9690
-2 . 6 190
2. 7829
0.0819
-0.0300
-0.0003
0.0147
-C. 0837
0.0300
- 0.0010
0.0605
0.0364
CHI_*60. 00
GAMMA*
1.5
ZETA* 2.00
X/H* 0. Y/H* 0.
If H* 0.
ETA* 0.75
(W»L 1
(U.L)
(W.D)
(U.C)
-1.3539
1.9978
-1.6974
0.8470
-1.2721
1.9963
-1.6532
0.9182
1 .5C2 2
-1.5902
1.9913
-0.4246
-1.7130
1.9986
-1.7130
0.S980
0.92 1 3
-1.7130
1.9986
-0.4377
-0.0408
-0.0008
0.0156
-0.0510
0.040?
-0.0022
0.0598
0.0202
CHI-75.QC
GAMMA*
1.5
ZETA* 2.00
X/H* 0. Y/H* C.
Z/H= n.
ETA* 0.75
(H.M
iU.LJ
tw»o 1
IU»C )
-1.0474
1.3022
- 1.2276
0.3126
-0.9120
1.2991
-1.1904
0.3369
1.5139
-1. 1259
1 . 2°24
-0.2819
-0. ?'>06
1.3062
-1.2467
0. 7325
0.95 M
-1 . 24G7
1 . 3062
-0.2986
-0.0668
-0.0040
0.0191
-0.0199
0.0678
-0.0070
0.0563
0-0043
CHI-90, 00
GAMMA* 1.5
ZETA* 2.00 X/H*
C. Y/H= C.
If H* 0.
ETA: 0.75
(W.L)
(U.L)
(W.D)
CU.D)
-1.0652
0.9186
-0.9186
-0.0000
-0.9272
0.9170
-0.91 70
a. oooo
1.4920
-0.8432
C.^4 32
-G.CO00
-0.9549
0.954?
-0.9549
0.0000
0.9549
-0.9549
0.9549
-n.oooo
-0. 1 102
-0.0363
0.0363
-0.0000
0.1277
-0.037?
0.0379
0.0000
122
TABLE 19.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 2.00, AND T) = 0.75
({] y/H - 0.375
CH I=-3. 00 GAH8A* 1-5 Z£TA- 2-00 X/H* 0. Y/H*
CH.L) -3.1539 -3.C7R2 1.5456
(U.L) -C- 2269 -0.2267 -3.8589 _
( y f 0 ) -4.050? -3.9064 -0.2267
t U , 0 1 -0.0534 0. 3659 2.2846
0.37 Z/H- 0, . ETA* 0.75
-3.1152 0.7841 -0.03C7 0.0371
-0. 2269 -4.02C1 -0.0001 0.0001
-4.0201 -0.2269 -0.0301 0.1137
0.2177 2.2706 -0.2711 0.1482
CHI* 3.00 G AH8 A = 1.5 ZETA = 2. CO X/H* 0. Y/H* 0,
<y f L) -3.1539 -3.0782 1.1547
0.2269 0. 2267 -3.6195
(U,0) -3.8130 -3.6673 0.2267
IU,D) 0.3026 0.7599 2.2P46
2/H= 0. E T A = 0.75
-3.1152 0.4077 -0.0387 0.0371
0.226? -3.7821 D.O00J -0.0001
-3.7821 0.2269 -0.0309 0.1148
0.6266 2.2706 -0.2440 0.1333.
CHJ- 15.00 GAHHA* 1.5 ZETA* 2.00 X/H* 0. Y/H*
IW,L) -2.8727 -2.7946 C.6504
(g t Lj 1.0658 1.0648 -2.9652
( U f D 1 -3.1619 - 3. Cl 35 1.0645
( U, D ) 0.9744 1.2770 1.9797
CHI * 30. 00 GAH8A* 1.5 ZETA = 2.00 X/H* 0. Y/H* Q
( y , L 1 -2.1302 -2.0436 0.5073
tg.U 1.7408 1.7305 -2.0881 . ....
( y v 0 1 -2.2F70 -2.1369 1.7377
(U,D) 1.1791 1.4014 1.1800
0.37 Z/H* 0. ETA* 0.75
-2.8328
-0.0711
-0.0399
0.0383
1.0654
-3. 1299
0.0003
-0. Q006
-3. 1299
1.0654
-0.0320
0. 1 164
1. 1706
1.9654
-0. 1962
0. 1065
Z/H- 0.
ETA* 0.75
-2.0860
-0. 1870
-0.0442
0.0424
1.7400
-2.2543
0.0008
-0.0015
-2.2543
1.7400
-0.0326
0. 1 174
1 . 3241
1.1644
-0.1450
0.0773
CH 1*45.00 GAHHA* 1.5 ZETA* 2.00 X/H*
ty,L» -1.2945 -1.19C2
iy*L> 1.8260 1.8213
( y r D ) -1.6109 -1.4610
(U,D) 0.9534 1.1039
0.7078 -1.2413 0.0377 __ -0. 0532 0.0511
-1.4120 I.R244 -i .5785 Q,Q Q15_ -0*0031
1.8196 -1.5785 1.B244 -0.0324 0.11?%
0.3021 1.0530 0.2639 _ -0.0996 0.0509
CHL*60.00 GA8HA*
IN.U -C. 7570 -0,6171 0.9793
IU.L) 1.4527 1.4423 -1.0149
IM t 01 -1.210i -1,0643 .. 1.4383
(U-»DJ_ 0.5694 0.6522 -0.2063
-0.6860
1.4494
-1. 18Q0
0.6267
0.3325.
-1.1800
1.4494
-0.2287
-0,0304 Q»U56
-0.0574 0.0255
6^T-1
L-15^9
123
TABLE 19. - Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, C = 2.00, AND T = 0.75
(g) y/H = 0.75
Correction factors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
•
only
to free air
to ground effect
, . « '
*
CHI*-J.OO GAiWA? 1.5 Z.ETA* 2-.CQ^ X/H* Q* - .Y/H* 0.75 U H* 0. LIA= C.75
(W.L)
(U.L)
tW.C)
(U.D)
-0.8971
-0.0361
- 1 .1*991
-0. 1162
-0,7293
-0.0856
-1. 1331
0.5215
-0.4755
-1. 1066
-0.0P55
1.2016
-0.31 12
-C.0359
-1. 3634
0. 2665
-1 . 3944
- 1.36 34
-0. 0559
I. 1676
-0.0859 0.0819
-G.00Q2 0.0003
-C.13S7 0.2304
-0,3828 0.2550
CHI* 3.00 GAMHA* 1.5
ZETA* 2.00 X/H*
Y/H= 0.75 Z/H* 0.
ETA* 0.75
(W.L)
(U.L)
( H » D 1
(U.D)
-0.3971
0.0861
-1.3797
0.0588
-0.7293
0.0356
-1.0073
0.6321
-0.4847
-0.9806
0.0855
1.2016
- 0.^112
0.0859
-1.2410
0, 4030
-1.3339
-1.2410
0. 0859
1. 1676
-0.0859
0.0002
-0.1386
-0.3443
0.0819
-0. 0003
0.2337
0.229!
CHI* 1 5. 00 GAMP A= 1.5
ZETA* 2. CO X/H* 0.
Y/H* 0.75 Z/H* 0.
ETA* 0.75
(W.L)
(U.L)
( W « D )
(U.D)
-C.8129
C .4 1 14
-1.1215
0.2873
-0.6399
0.4086
-0.7403
0.7447
-0.4069
-0.7134
0.4034
1.0912
-0.7243
0.4102
-0.9783
0.5627
-1.2715
-0.9730
0.4102
1 .C564
-o.oeps
0.0012
-0.1427
-0.2754
0.0845
-0.0016
0.2385
0. 1820
CH l* 30. 00
GAMMA* 1.5. ZfTA* 2.00 X/H* 0.
Y/H* 0.75 It H= 0.
ETA* 0.75
(W.L)
(U.D
(W.D)
(U.D)
-0.5859 -0.3949 -0.
Q.7VQ2L 0.7035 -0.
-0.3422 -0.4557 0.
0.3748 0.7045 0.
1572
-0.4881
-0.9846
4235
0.7073
-0.6971
7030
-0.6971
0.7073
79*09
0.5749
0.74 14
-0.0976
0.0C29
-0. 1451
- 0.2001
0.0932
-0.003a
0.2414
0.1296
CHI-45. 00
GAMMA* 1.5 ZETA* 2. CO X/H*
Y/H= 0.75 Z/H* 0.
e r a=
0.75
(W.L)
IU,U
(W.D)
(U,D)
-0.3229
0.8200
-0.6806
0.3207
-0.0946
0. 6062
-0.2955
0.5342
0. 102"
-0.2682
0.8052
0.3781
-0.206 1
0.3141
-0.5364
0.4529
-0.6 M2
-0.5364
0.0141
0.3356
-0.1168
0-0059
-0.1442
-0.1322
0.1)13
-0.0079
0.2408
0.0813
CH 1*60. OO
GAMHA* 1.5 ZETA* 2.00 X/H* O.
Y/H= 0.75 Z/H* 0.
ETA* C . 75
(W.L) -0.1717
(U.LL 0.7403
(W.0) -0.6364
(U.D) 0.2205
0.1298
0.7098
-0.2644
0. 32 39
0.595C
-0.2369
0.7076
0.04 29
-0.0173
0. 7274
-0.4989
0. 2890
-0.2562
- 0.4999
0.7274
-0.0058
-0.1544
0.0129
-0.1376
-0.0684
0. 1470
-0.0176
0.2344
0.0349
CH I* 75. 00 GAMMA* 1.5 ZETA* 2.0C X/H* 0. Y/ll* 0.75 It H* 0.
ETA* 0.75
(W.L) -0.26D6
(U.L) 0.5970
(W.C) -0.6253
(U.D) 0.1236
0. 1 900
0.5148
-0.298C
0. 1329
0. 7260
-0.2698
0.5075
-0.0635
-0.0296
0.5642
-0.5103
0. 1370
0.0033
-0.5)03
0.5642
-0. 1090
-0.231 1
0.0328
-0.1150
-0.0135
0.2196
-0.0494
0.2123
-0.0042
CHI-90.00 GAMMA* 1.5 ZETA* 2.00 X/H* 0, Y/H* 0.75 Z/H* Q._ ETA* C.75
(W.L )
-0.5055
0.1589
0.0312
-0. 1711
0.1711
(U.L)
C. 5404
0.3386
-0.3060
0.4889
-0.4889
(W.D)
-0.5404
-0.3386
0.3060
-0.4889
0.4089
(U.D)
-0.0000
0.0000
c.ocoo
-0.
0.
-0.3344 0.3301
0.0515 -0.1503
-0.0515 0.1503
- 0.0000 0.0000
124
TABLE 20
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.50, C = 4.00, AND i) = 0.75
(a) y/H * -1.50
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
chi— 3 . 0 c
GAMMft. 1.5
ZCTA* 4.00 X /H = 0
Y/H*-
1.50
Z/H* 0.
ETA* 0.75
(W.LJ
-0.0164.
.... . . -0*0.1.14
-0.36i2
-H.CL]1£_ __
-0.9076
-0.0026
0.0025
MJ,L 1
(W,P)
(U,D)
-0.0223
-0.1642
0.1713
-0.0223
-0. 1 182
0* 3299 _
-0. 1069
-0.022?
0 . 4 iea
-0.0223
-0. 1577
0^2815
-0.1577
-0.0223
Q .4 17?
-0.0000
-0.0065
fl.OQQfl
0.0395
0.04B1
CHI- 3.00
GAM«A= 1.5
ZFTA- 4.00 X/H= 6
. Y/H—
1.50
Z/H* 0.
ETA* 0.75
(W.U
-0,0164
-0.0114
-0.3593
-P.Q 138
_ -Qj_2945.
-0.0026
0.002S
I U * L 1
( Mf D 1
. CUtB)
0.0223
-0.1204
0.1965
0.0223
-0.0743
0.3393
-0.0630
0-0222
0.4188
0.0223
-0. 1139
0.2960
-0. 1139
0.0223
0.4179
0.0000
-0.0066
-0.0995
- 0.0000
0.0393
0.0433
CHI-15.00
GAMMA* 1.5
ZETA* 4.00 X/H— 0.
Y/H— 1
1.50
Z/H* 0.
ETA* 0.75
_JW»L>
0.0102
0.0155
-0.3171
0.0129
-0.8443
-0.0027
0.0026
I U t L 1
1W,01
i M ■ P-l
0. 1066
-0.0374
0.2 1 34
0. 1065
0.0089
0.3286
0.0203
0. 1065
0.3914
0.1065
-0.0308
0.2937
-0.0308
0.1065
0.3905
0.0000
-0.0066
-0.0804
- 0.0001
0.0396
0. 0349
CHI-30.00
GAMMA* 1.5
ZETA* 4.00 X/H* 0.
Y/H—l
1.50
Z/H* 6.
ETA* 0.75
(W.L1
0.0C59
0.0917
-0.2246
0,0889
-0.7423
-0.0030
0. 0029
(U,L)
t Hy D )
( u^p >
0. 1849
0.0396
0. 1825
6. 1847
0.0860
0.2688
0.0974
0. 1846
0.3132
0. 1848
0.0463
0.2428
0.0463
0.1848
0.3122
0.0001
-0.0067
-0.0603
- 0.0001
0.0397
0.0261
CHI-45.00
GAMMA* 1.5
ZETA* 4.00 X/H* 0.
Y/H—l
±50
Z/H* 0.
ETA* 0.75
LMJJ
Q«.l.e76„
0 . 1 9140
-0. 105 1
0. 1913
-0.6145
, 0 ; D03 ;
0.0035
IU,L)
. IW.D1
IU*.B 1
0.2145
0.0678
5*1114
0.2141
0. 1 142
0. 1 787
0. 1256
0.2140
0.2061
0.2144
0.0745
0. 1603
0.0745
0.2144
0 . 2049
0.0002 "
-0.0067
-0.0429
-0.0003
0. 0399
QiPlO*!
CHI-60.00
GAMMA* 1.5
ZETA-
4.00
X/H*
0. Y/H*-’
1.50
Z/H- 0.
ETA- 0.75
IH.U
0.2842
0.2942
0.C144
0. 2993
-0.4873
-0.0051
1 U,L 1
(H,D)
(U*P1
0. 1P93
0.0395
_0_._045.6_
0.1882
0.0860
0.0879
0.0974
0. 1880
0.0991
O. 1889
0.0462
0.0767
0.0462
0.1889
0.0964
0.0004
-0.0067
-0.0271
-0.0007
0.0398
n.ni 1 ?
CHI-75. 00
gamma- 1.5
ZETA*
4.00
X/H*
0. Y/H* - 1
1.50
Z/H- (L.
ETA* 0.75
1*«U
0.3360
.
0.3544
0. I0B6
0. 3454
-0.3851
-0.0094
0.0090
(U*L)
(W,01
(U.Dl
C. 1254
-0.0361
0.0103
0.1212
0.0101
0.0262
0.0215
0. 1205
0.0174
0. 1240
-0.0295
0.0222
-0.0295
0.1240
0.0146
0.0014
-0.0065
-0.0119
-0. 0028
0.0396
0.0041
CM 1*90. OC GAMMA* 1.5 ZETA* 4.00 X/H- 0. Y/H=-1.50 Z/H* 0.
ETA* 0.75
LH*kl. 0.2778 0.33 57 0.1727 0.3056 -Q.3CS6
0.1248 0.0838 -C.0720 0.1208 -0.1208
-0.1248 -0.0338 0.0720 -0.1208 0.1208
— UU °j -0.00 00 -0.0000 0.0000 - 0 ,0000 0,0000
-O.O 277 0.0301
0.0040 -0 .0370
-0.0040 0.0370
-0.0000 6.0000
6^ T-T
L-15^9
125
TABLE 20.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1.50, { = 4.00, AND H = 0.75
(b) y/H - -1.125
s
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
r ~~~~l
to ground effect
i
CHl*-3.00
GAMMA* 1.5
7ETA* 4.00
X/M*
O.
Y/H=-
1 . 12
Z / H* 0.
ETA* 0.75
1W,W
-0.0557
... -Q.0S24
-1.0489
-0.0541
... -1,5709
-0.0017
0,5017
IU,D
-0.0397
-0.0397
-0. 3055
-0.0397
-0.3502
0.0000
0.0000
(W,I)1
-0.3423
-0. 3263
-0.0397
-0. 3502
-0.0397
0.0079
0.0239
IU.01
0.3317
... . 3.4672
Q * 732 1
0 , 4 29 1
0*73 16
-0*0976
0.0379
CHI* 3.00
GAMMA* 1.5
ZE TA = 4.00
X/H*
6.
Y/H=-
f. 12
Z/H* 0.
ETA* 0.75
—
IW . n
-0,0557
-0.0524
-1.0254
-0.Q541
- 1 .5420
-0.0017
0,0017...
IU,L )
0.0397
C.0397
-0.2288
0.0397
-0.2736
-0.0000
-0.0000
(W,D)
-0.2657
-0.2496
0.0397
-0.2736
0.0397
0.0079
0.0239
lUjD}
0.3741
0*4961
0.7321
0.4620
0,7315
-0,0879
0.5341
CHJ=I5.00
GAMMA* 1.5
ZE T A = 4.00
X/H*
0.
Y/H--
1.12
Z/H* 0.
ETA* 0.75
1 W.L 1
-0.0091
-Q. 0056
-0.9356
-Qj 0QJ4_
-1,4450 __
—0. 0017
_ ... Q. OOlfi
1U.L1
0.1902
C. 1901
-0.0827
0. 1902
-0.1275
-0.0000
-0.0000
(W.0)
-0. 1196
-C. 1035
C. 1901
-0.1275
(1. 1902
0.0079
0.0240
(U.C 1
0.4005
0.4990
__0,.6e30.
0.4 7_L5
0,6824
-Q.Q7LQ.__
0.0275
~CH~I = 30.00 "
GAMMA* 1.5
7F TA = 4.00
X/H =
d".
Y/H* —
1 . 12
z/h= o.
E T A= 0.75
< W.L)
£* 12_24
0. 1263
-Q, 7529
-1,2538
-Q.QQL9 _
0.0020
(U,L )
0.3303
0.3303
0.0532
0. 3304
0.0083
-0.0000
-0.0001
(W,DI
0.0162
0.C323
0.3302
0.0083
O. 3304
0.0079
0.0240
1U.0J
0. 3429
0.4169
0.5429
0.3962
0.5422
-0.0534
0,0206
CH 1*45. 00
GAMMA* 1.5 ZETA*
4.00 X/H*
O. Y/H=— 1.12
Z/H* 0.
ETA* 0.75
(M.Ll
0.2971
0.3019
-0.5737
0.2995
-1.0173
-0.0023
0,0024 _
(U,L1
0.3048
0. 3847
0. 1032
0. 3848
0.0582
- 0.0000
-0.0001
(W,01
0.0661
0.0022
0.3846
0.0582
0.3848
0.0079
0.0240
(U.O)
0.2261
0.2788
0.3502
0.2642
0.3494
-0.0381
0.0146
CHI»60. 00
(W.L)
GAMMA* 1.5 ZETA*
0.4565
4.00 X/H* 0.
0.4632
Y/H*- 1 .12
-0.2941
Z/H= 0.
0.4598
ETA* 0.75
-0.7810
-0.0033
. 0,001*1
( U , L 1
0.3442
6. 3439
0.0546
0.3442
0.0096
- 0.0000
-0.0003
< W , O J
0.0175
0.0336
0.3435
0.0096
0.3442
0.0079
0.0240
(U.O)
0.1058
0.1393
C. 1544
0. 1301
0.1533
-0.0243
0.0091
CHI-75.00
GAMMA* I.'S'
ZETA*
4.00
X/H*
0.
Y/H*— 1
1 . 12
Z/H* 0.
ETA* 0.75
(W.L 1
0.5229
0.5352
-0.1045
0.5289
-0.5848
-0.0061
_ 0.0061
fU.L)
0.2445
0.2434
-0.0731
0.2445
-0. 1180
-0.0001
-0.0012
(w,oi
-0. 1 101
-C. 094 1
0.2420
-0.1180
(1.2445
0.0080
Q. 0240
(U.O)
0.0351
0.0499
0.0096
0.0462
0.0076
-0.0112
0.0037
CHI*90ToT
GAMMA* 1 . 5
ZETA*
4‘.“do
X/H^
~0.
Y/H*— 1
\'.\T
Z/H* 0.
ETA* 0.75
( Wj LI
0.4C34
0.4452
0.0474
0.4222
-0. 4222
-P.Q196--
0.0231
(Ilf L )
0.2463
0.2337
-0.2120
0.2559
-0.2559
-0.0095
-0.0222
(W.0)
-0.2463
-0.2337
0.2120
-0.2559
0,2669
Q .0095
0.0222
(UfOl
-0.0000
-0.0000
0.0000
-0.0000
0.0000
-0.0000
0.0000
126
TABLE 20. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.50, £ =4.00, AND T? = 0.75
(c) y/H = -0.75
CHI — 3.00 GAMMA* 1.5 ZETA* 4.00 X/H= 0. Y/H = -0.75 Z/H= 0. E T A = 0.75
U.LX -0*3117 ... -0.30C5 r2.53.9J -0.31QL -3.1202 -0.0015 0.001ft
1 0» L ) -0,0900 -0.0900 -1.0024 -0.0900 -1.0477 0.0000 0.0000
(H.01 -1.0335 -1.0299 -0.0900 -1.0477 -0.0900 0.0142 0.0178
_UU&L_ D.6Q57 _ ... 0.735ft__. UlftUt 0.6993 1.5609 -0.0940 0.0358
CHI* 3.00 GAMMA* 1.5 ZCTA = 4.00 X/H* 0. ~V/H— 0.75 ’ " 1 / H* 0. ETA* 0.75
.HULL -0.3L1I -0. 3085 -2*5ii6 -0.310] _ -3.0573 -0.0015 0.001ft
(UtL 1 0.0900 0.0900 -0.8387 0.0900 -0.8841 -0.0000 -0.0000
tW*D) -0.8699 -0.8663 0.0900 -0.8B41 0.0900 0.0142 0.0178
- -LVUDJ 0*7163 0,8333. 1.5614 0.8010 1.5609 -0.084.7 0.0322.
CM 1= 15.00 GAMMA* 1.5 ZETA* 4.00 X/H* 0. " Y/H=-0.75 Z/H* 0. CTA= 0.75
IMjL 1 -0. 2124 -0.209 1 -2. 2978 -0.21 08 -2.8232 -0.0016 0,0017
«U,l) 0.4312 _ 0.4312 -0.5224 0.4312 -0.5679 -0.0000 -O.OOOO"
tMiO) -0.5536 -0.5501 0.4312 -0.5679 0.4312 0.0142 0.0178
llUfi] . 0.8 073 0.9018 1.4491 0^8758 1.4485 -0.0685 O.OgftO
CHI*30.00 GAMMA* 1.5 7E T A= 4.00 X/H* 0. Y/H=-0.75 1 / H= 0. ETA* 0.75
— LW*LL 0.0645 __0.06 82 -1.8 609 0.0663 -2.3777 -0.0018 0.0019
(U,L> 0.7512 0.7512 -0.2236 6.7513 -0.2691 -0.0000 -0.0000
1W,D1 —6*2549 -0.2513 0.7512 -0.2691 0.7513 0.0142 0.0178
HU PI 0,7187 0.78 96 1. 1278 0.7701 1.1272 -0.0514 0.0195
CHI *45. 00 GAMMA* 1.5 . ZETA* 4.00 X/H* 0. ' Y/H--0.75 " " Z/H* 0. “ " ETA=0.75
___ 1 N,.LJ 0.4192 0.4 237 -1.3218 0.4214 -1.8312 -0.0022 0.0023
1U,L) 0.8020 0-8820 -0. 1080 ' 0.8P21 -0.1536 -0.0001 -0.0001
<W,D1 -0.1394 -0.1358 0.8818 -0.1536 0.8821 0.0143 0.0178
CUjDI 0.4983 0.5490 0.6847 0.53 51 _ 0.6840 -0.0368 0.0139
CH 1*60. 00 GAMMA* T. 5 ZETA* 4.00 X/H*0. Y/H * r 0.75 Z/H* "o. " ETA=0.75
1W,L) 0. 706 5 0.7128 -6.7821 0.7096 “1.2848 -0.0031 _ 0,0033
1U*t» 0.8095 0.8095 -0.196ft 0.809ft -6.2423 -6.6oof~ -0.0001
CW»D) “0.2280 “0.2244_ 0.8090 -0.2423 0.8096 0,0141 _ 0.0178
tU*D> 0.2692 0.3015 0.2376 0.2927 0.2365 -0.0236 ’ 0.0087
6 ^ 1-1
TABLE 20. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.50, 5 = 4.00, AND i) = 0.75
(d) y/H = -0.375
127
8
Correction factors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
, 1 1 »
CHI— 3,00
CHI* 3. 00
lUfLI
IM,D)
_ tUiPl--
f H,l )
tU»L)
1W,D)
lUtOL
IH»L \
( U»L )
I W, D >
IU,D >
IW,L)
( U » L I
(w,r)
(U,0)
GAHHAv 1,5
ZETA= 4.00
X/H*
0.
Y/H*-0.37
Z/H= 0.
-3-2468
-3.2428
-4.9994
-3,2440
-0.3435
-0.3435
-5.4031
-0.3435
-5-4400
-5.4337
-0. 3435
-5.4537
0.9682
1. 1062
4.6712
1.0662
GAMH A*' 1.5
ZET A* 4.00
X/H -
0 .
Y/H*-0. 37
Z/H* 0.
- 3.2468
-3.2428
-4.9624
-3.2448
0.3435
6.3435
-4.91 35
0. 3435
-4.9504
-4.944 1
0.3435
-4.9641
1.5239
1.6482
4.67L2
1
G AM4 A - 1.5
7E TA= 4.00
X/H-
0 .
Y/H=— 0. 37
Z/H* 0.
-2.8993
-2.8952
-4.5218
-2.8973
1.6408
1.6406
-3.P644
1.6406
-3.9014
-3.8950
1.6408
-3.9151
2.1794
2.2797
4,2261
2.2506
•
G A8M A = 1.5
ZETA* 4.00
X/H*
0.
Y/H--0 .37
Z/H* 0.
-1^9547
-1.9502
' — '
-3.3839
-L*9525_ .
2.8293
2.0293
-2.7375
2.8293
-2.7745
-2. 7632
2.8292
-2. 7883
2.2461
2.3214
2.9742
2.2996
ETA* 0.7 5
-5.5778
-5.4537
-0.3435
4.6706
-5.535.6_
-4.9641
0.3435
4 . 6 706
CHI = 45.00 GAHMA* 1.5 ZET A *
Y/H—C.37 Z/M* 0.
-Q . 82.7.1 .
3.2562
-2.1317
1.7734
-2.0946
3.2559
1.3431
-0.9244
3.2562
-2. 1455
1.E1J6
ETA* 0.75
-5. 0858
-3.9151
1.6408
4.2255
ET A= 0.75
-3,9383
-2.7883
2,8293
2.9734
ETA- 0.75
-2.4448
-2. 1455
3.2562
L.3422 _
-0.0019
0.0000
0.0137
-0.0979
-0.0000
0.0137
-0.0882
- 0.0020
- 0.0000
0.0137
-0.0712
- 0.0022
-0.0000
0.0137
-0.0535
0.0020
0.0000
0.0200
0.0400
0.0020
-0.0000
0.0200
_0. 036 1
0.0021
-0.0000
0.0201
0.0291_
0.0023
-0-0000
0.0201
0.0218
CHI=60.00
GAF M A* 1.5
ZETA* 4,00
X/H= 0.
Y /H=-0. 37
Z/H= O.
ETA- 0.75
(W t U
IU,L)
!W»D)
t'J.D)
-0.0729
2.9096
- 1. 9010
1.1315
. -0,5650
2.9095
-1.9754
1,1656.
-0.4061
- 1.9447
2.9090
-[1-0217
-0.0690
2.9097
-1.9955
1 . 1559
-1.0248 _
-1.9955
2.9097
-0-5230
-0,0035
-0.0001
0.013B
-0.0244
. 0.0040
-0.0002
0.0201
0.0097
CHI = 75. 00
GAK8A* 1.5
ZETA* 4.00
X/H* 0.
Y/H*-0. 37
Z/H* 0.
ETA* 0.75
( W T L )
IU.ll
t W* D J
(U»D)
-0. 1254
2.2563
-2.0274
0.5369
-0. 1109
2.2559
-2.0212
0.5522
0,5447
-CUJ J p 3
0
-Q.oon
0.0074
-1.9^04
2.2539
-0,4297
2.256B
-2.0412
0.5482
-2.0412
2.2568
-0.431?
-0.0005
0.0139
-0,5111.
-0.0008
0.0200
1,0040 _
CHI*90.00
GAP“A= 1.5
ZETA* 4.00
X/H* 0.
Y/H=-0. 37
Z/H* 0.
ETA* 0.75
IH,L)
(U,L1
f W, D )
iu.ni
-0.7062
1.9400
- 1.9400
-0.0000
-0.6576
1 7055 -0.6845
0.6845
-5,5211 .
^ 0*0267
? I 9-377
-1.9377
0.0000
-1.9057
1.9057
-0.0000
1.9557
-1.9557
-0.
-1.9557
1.9557
0.
-0.0157
0.0157
-0.0000
-0.0180
0.0160
1,0 OM
128
TABLE 20.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.50, C = 4.00, AND 17 = 0.75
(e) y/H = 0
Correction factors for
correcting from
0 wind tunnel
which Is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
1 1
CHI— 3.00 GAMWA* 1.5 ZE TA =
- 4.00 X/H* C
). Y/H= 0.
Z/H* 0.
ET A= C . 75
... tw.u '
-26.6157
-26.6096
30.6624
-26.6127
30.0157
-0.0031
0.0030
(U f l)
-1.6925
-1.6927
-31.0671
-1.6926
-31.1287
0.0001
-0.0001
IW.D)
-31.1244
-31.0959
-1.6925
-31 . 1207
-1.6926
0.0043
0.0327
10,01
0. 1162
0.2817
1 3.2897
0.2286
13.2823
-0. 1 124
0.0531
CHI- 3.00 GAHHA- K5 _Z£ TA* 4.00 X/H= C
>. Y/H= 0.
Z/H* 0.
ETA* 0.75
ItUU
-26.6157
-26.6096
24.2677
-26*6127
23.6274
-0.0031
0 . 0030 ...
tu»ll _
_ 1.6925
1.6927
-29.6741
1.6926
-29.7359
-0.0001
0.0001
tM.aj-
-29.7316
.-24* 7 030
!,i>925
-29.7359
1.6926
0.0043
0.032B
1U,0)
3.3170
3.4663
13.2897
3.4184
13.2883
-0.1014
0.0479
CHI- 15^.00 CAffHA* 1. 5 _ ZEIA* ‘i.QQ A/H = C
U_ __ _Y/H= 0...
If H* 0.
ETA = 0.75
IU.I )
-2 3.7736
-23.7672
14.0234
-23. 7704
13.3941
-Q .0032
0.0031
iu.u
JUT 50 4
-24.5444 ’
7.7585
-24.6062
0.0000
- 0.0000
(H>0)
-24.6020
-24,5733
7.7584
-24.6062
7 . 7585
0.0042
0.0329
UJ.D 1
_ T.7H29
1,8614
10.9473 _
UH234
10.9463
-0.0005
0.0379
CHI=3Q, 00 GAHHA- 1-5 ZETA * 4 .00 X/H» 0. Y/H* 0, If H* 0. ETA= 0.75
(HaL 1
-16.7148
-16.7078
6-8247
-16.711 3
6.2070
-0.003S
0.0035
1U.L)
1 1*7744
1U7743
-16.6744
1 1.7744
-16.7364
0.0000
- 0.0001
(U.D)
- -16,7322
. . - 16, 7034
11,7742
-16.7364
11.7744
0.0042
0.0330
(UaCi
8.8743
8.9631
5.3904
8, 2 347
5.3892
-0.0604
0.0284
CHI*45.00
GAHHA* 1.5
ZETA* 4.00
X/H* 0. Y/H=
0.
Z/H* 0.
ETA* 0.75
IKiU
-9.5536
-9.5450
4.4B36
-9.5493
3. 8759
-0.0043
Q, 0043
1U»U
11.1316
1 1 * 1112
. -10,4140
11.1315
-10.4761
0.0001
-0.0002
(H.D1
-10.4719
- 10.4431
11.1310
-10.4761
11.1315
0.0042
0.0330
IU.D)
6.6J34
6.6764
0.3291
6.6564
0.3277
-0.0430
Q.Q2QQ
CHI=60. 00
GAHH A- 1.5 ...
ZE TA* 4,00
X/H- 0. Y/H*
0,
Z/H* 0.
ETA* 0.75
IN.L)
-5*256 1
-5.2461
4.2835
—
-5.2521
-0.0060
0.0060
IU t L)
7.9945
7.9937
-6.7899
7.9943
-6.8520
0.0002
-0.0006
(w,oi
-6.8478
-6.8190
7.9932
-6. 8520
7.9943
0.0042
0.0330
IU.O)
3.5648
3.6043
-1.7488
3.5920
-1.7507
-0.0272
0.0123
—
CHi- 75.00
GAMMA* 1.5
ZETA* 4.00
X/H* 0. Y/H*
”67
' Z/H= 0. '
ETA* 0.Z5
.
nuu
-3,9336
-3,9115
4.3935
ri,?226
3.8044
„ -0.Q111
0.0110
IU.U
5.2254
5.2224
-4.9248
5.2246
-4.9868
0.0007
-0,5021
1H±0>
-4.9824
-4.9540
5.2204
-4.9068
5.2246
0.0044
0.0328
iu.ci
1.3181
1.3349
-1.1910
J.,3302 .....
-1. 1943
-0.0121
0. 0047
CHI-90.00
GAMMA* 1.5
7 E T A= 4.00
X/H= 0. Y/H*
0 .
z /h*~oT
ETA* 6.75
<H,L)
-3.8523
-3.7832
4.3939
-3.8197
3.8 T9 7
-0.0326
0.0365
UUJJ
3.8124
3.7900
-3.7596
3.8197
-3.8197
-O.O073
-0.0297
. IH.P1
-3.8124
-3.7900
3.7596
-3.8197
3.8197
0.0073
0.0297
IU.01
0,0000
0.0000
-0.0000
0.0000
-0.0000
-6.0000
6. 6000
6 ^ 1-1
l-15^9
129
3S
TABLE 20.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.50, £ = 4.00, AND 7} = 0.75
(f) y/H = 0.375
Correction factors for correcting from a wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CHI — 3.00
GAH0A* 1.5
ZETA* 4.00
X/H*
0 .
Y/H=
0.57
Z/H= 0.
E T A = 0.75
( Wtl )
- 3.2509
-3.239J)
-4.3065
-3.2448
-5.5779
-0,0061
0.0059
(U,L)
-0.34 36
-0.3435
-5.3681
-0. 5435
-5.4537
- 0.0000
0.0000
l W » D 1
-5.4750
-5.3900
-0.3435
-5.4537
-0.3435
-0.0213
0.0629
tU.D)
0.9265
1,1460
4,6726
1.0662
4.6706
-0.1396
0.0798
CHI = 3.00
GAPMA* 1.5
ZE T A* 4.00
X/H =
0 ,
Y/H*
0.37
Z/H* 0.
ETA* 0.75
( W,L )
-3.2509
-3.2390
-4. 7729
-3.2448
-5.5 J56
-0.0061
0.0059
(U.D
0.3436
0.3435
-4.8784
0.3435
-4.9641
0.0000
-0.0000
( W ( 0 )
-4.9R55
-4.901C
0.3435
-4.9641
0.3435
-0.0214
0.0631
(U.D)
1.4864
1.6B4Q
4.6776
1.6121
4.6706 .
-0. 1257
0.0718
Chi* 15 . 00
GAH0A* 1.5
ZETA* 4.00
X/H*
0 .
Y/H*
C .37
Z/H* 0.
ETA* 0.75
(W.D
-2.9036
-2.0912
-4.33a2___
-2.9973
-5.0858
-O.OQ63
O.OQ6I
l U.D
1.6409
1.6407
-3.8291
1 . 6408
-3.9151
0.0001
-0.0001
( W • D >
-1.9367
-3.0510
1.6406
-3.9151
1.6408
-0.0216
0.0633
(U,0)
2.1423
2.3Q85
4.2275
2.2506
4.2255
-0. 1014
0. 0578
CHI=30. 00
GAHMA*
1.5
ZET A*
4.00
X /H— 0. Y/H=
0.37 7/H* 0.
ETA* 0.75
(W.D
(U.D
1 w.n
(U.D)
- 1,9595
2.8296
-2.8)00
2.2238
-1.9457
2.8290
-2.7247
2.3427
.-J.,2066
-2.7020
2.8289
2 s 9757
-1.9525
2.8293
-2.7083
2.2996
-3.9353
-2.7CP3
2.8793
2.9734
-0.0070
0-0002
-0.0218
-0.0758
0.0068
-0.0003
0.0635
0.0430
CHI=45. 00
GA!<m*a =
1.5
ZETA*
4.00
X/H* 0. Y/H*
0.37 Z/H= 0.
ETA* 0.75
(H.D
fU.L )
(W.D)
(U.D)
-0.8329
3.2568
-2. 1673
1 . 7580
-0.8)6 1
3.2555
-2. 0818
1.8417
-1.7269
-2.0591
3.2554
1 . 3450
-0.8244
3.2562
-2.1455
1.8116
-2.4448
1455
3.2562
1.3422
-0.0086
0.0005
-0.0218
-0.0536
0.0082
-0.0007
0. 0636
0. 0301
'•01 = 60. 00
GAH0 A* 1.5
ZETA* 4. CO X/H*
0. Y/H*
0.37 Z/H= 0.
fcT A= 0.75
( W,L )
(U.D
1 W, 0 )
l U, C )
-0.0809
9.9109
-2.0173
1.1226
-0.0575
2.9090
-1.9319
1 . 17 39
-0.3199
-1.909 1
2.9076
-0.019?
-0.0690
2.9097
-1.9955
1.1559
-1.024C
- 1 .99 55
2.9097
-0.0230
-0.0119
0.00(2
-0.0210
-0.0333
0.01 15
-0.0017
0.0636
0.0180
CHI-75.00
GA0P A = 1.5
O
O
X/H* 0. Y/H=
0.37
Z/M* 0.
ET A= 0.75
( W , L )
(U.D
rw*c)
(U.D)
-O. 1390
2.261?
-7.0625
n. 5349
-0.C975
2.2506
— 1 . 9 7 F 1
0.5539
0. 7042
-1.9553
2.2490
-C.4260
-0. 11° 3
2. 2566
-2.C4 1?
C. 54 82
0.0133
-7.C4 12
9.2568
-0.4 ?I9
-0,0216
0.0044
-0.0213
-0.0133
0.0208
-0.006?
0.0631
0.0057
:hi=9o.oo
GA00A* 1.5
Z E T A * 4. 00
X/H= 0. Y/H*
0.37
Z/H= 0.
ETA* C . 75
( H.L )
(U.L)
( W. D 1
(U.D)
-0.7425
1.971C
- 1.971C
-0.0C0C
-C.624?
1.6926
- 1 • 3? "6
c.ccoc
1.3495
-1.P747
1.0747
0.0000
-0. 6P45
1.9557
-1.9557
-0.
0.6~45
-1.9557
1.9857
n.
-0,Q58(L
0.0153
-0.0153
-D.QOOQ
0,0597
-0.0571
0.0571
0.0 00Q
150
TABLE 20. - Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.50, C = 4.00, AND tj * 0.75
(g) y/H =0.75
8
Correction factors for correcting from o wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
' 1 1 ■ 1
to grour
id effect
CHI*-3.00
GAMMA = 1.5
ZETA* 4.00
X/H* 0. Y/H- 0.75
It H* 0.
ETA* 0.75
(W» L 1
-0.3260
-0.2948.
-2. 1003
-0.3101
-3,1282
-0.0159
0.0154
t U* L )
-0.0701
-0.0899
-0.9040
-0.0900
-1.0477
-0.000 1
0.0001
(M,D)
-i. ni9
-0.9166
-0.0899
-1.0477
-0.0900
-0.0842
0. 1311
III* D )
0.4735
0*84.43
Q.697S
__ . U56Q9
-0.2063
0. 1445
CHI* 3.00
GAMMA* 1.5
ZETA* 4.00
X/H* 0. Y/H= 0.75
Z/H* 0.
ETA* 0.75
(W,L)
-0. 3260
.... -0*2948
-2,0433
-0,31 0J_
-J.0573
-0.0159
0.0154
CU.L1
0.0901
0.0099
-0.7398
0.0900
-0.8841
0.0001
-0.0001
(W,D>
-0.9680
-0.7524
0.0899
-0.8841
0.0900
-0.0847
0.1317
tU»D>
0.6154
0.9310
1.5663
0.8010
1.5609
-0. 1856
0. 1299
CHI* 15.00
GAMH A = 1.5
ZETA* 4.00
X/H* 0. Y/H* 0.75
Z/H- 0.
ETA* 0.75
IW.L1
-0.2272_
-0.1.9 4 ?
-1.8337
-0.2108
-2.8232
-Q,Q164_
0.0159
(U»L)
0.4716
0.4308
-0*4227
0.4312
-0.5679
0.0004
-0.0004
1W,0I
-0.6533
-0.4354
0.4300
-0.5679
0.4312
-0.0854
0. 1325
<UiD)
0.7263
0.98 02
1*4.5.42 . ....
0,8158
1.4485
-Q* 1495
0. 1044
CHI *30. 00
GAMMA* 1.5
ZETA* 4.00
X/H* 0. Y/H* 0.75
Z/H* 0.
ETA* 0.75
(W»L )
0.0480
0.0839
-1.4142
0.0663
-2.3777
-0.0182
0.0177
LU,L>
0.75 22
0.7503
-0. 1234
0.7513
-0.2691
0.0009
-0.0010
(H.D)
-6.3551
-0.1360
0.7502
-0.2691
0.7513
-0.0860
0.1331
... ILi , D 1
_ 0*65901
Q«£473L
1,1334
0.7701
1.1272
-O. 1111
0.0772
—
CHl*45.00
GAMMA = 1.5
ZETA* 4.00
X/H* 0. Y/H* 0.75
z/h* ”o7“
ETA* 0,75
... AHmL\
0.3992
. _ 0.4429
-0.8907
Qi42J_4
-1.8312
-0.0222
0.0215
IU.ll
0. 8840
0.8799
-0.0076
0.8821
-0. 1536
0.0019
-0.0021
|M*0>
-0.2398
-0.0203
0.8799
-0.1536
0.8821
-0.0862
0.1334
IU«D)
0,45.77
0.5882
.... Qj..6.9_L4.-. ....
0.5351
0.6840
-0.0774
0. 0530
ChT*60,00
GAMMA* 1.5
ZETA* 4.00
X/H* 0. Y/H* 0.75
Z/H* 0.
ETA* 0.75
(U.L)
0.6789
C.7395
I— -Q. 3665
0.7096
-1.2848
-0.0307
0.0297
<U,L)
0.8141
0.8046
-0.C964
0.8096
-0.2423
0.0045
-0.0050
(W,C)
-0.3282
-0.1091
0.8044
-0.2423
0.8096
-0.0860
6.1331
lu.oi
0.2467
0.3229
0.2464
0.2927
0.2365
-0.0460
0.0302
CH 1*75. 00
GAMMA* 1.5
ZET A* 4760
X/H= 0. Y/H* 0.75
Z/H* O.
ETA* 0.75
I Wf L I
C . 6925
0.7982
0. 0677
0.7462
-0.8250
-0.0537
0.0520
tu.u
0.6506
0.6177
-0.3218
0.6353
-0.4658
0.0153
-0.0175
(W,D)
-0.5498
-0.3345
0.6169
-0.4658
0.6353
-0.0840
5.131?
IU,OJ
9.121?
C. 1425
_ -0_9_0407
0. 1358
-0.0549
-0,0146
Q.Q067
CHI *90. OC
GAMMA* 1.5
ZETA* 4.00 X/H*
0. Y/H*
0.75 Z/H* 0.
ETA* 0.75
(W,L>
0.3273
0.5752
0.3897
0.4520
-0.4520
-0.1247
0. 1232
tlf.L)
0.7206
C. 5359
-0.5226
0.6519
-0.6519
0.0686
-0.1161
l M, D 1
-0.720ft
-0.5359
0.5226
-0.6519
0.6519
-0.0686
0.1161
f II, D 1
-0.0000
o.ooco
0.0000
-o.oooa
C.0000
-0.0000
Q.QOOO
6i£t -i
L-15^9
131
TABLE 21
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y * 1.5, C = 0.70, AND V * 0.50
(a) y/H= -1.875
Correction foctors for
correcting from
a wind tunnel
which Is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
1 1
guilt M 0.70 X/H
—
* 0. Y/H=-1
—
.37 2/ H- 0.
ETA- 0.50
— IlMEDtifc
®W?87
-0.0567
0.1914
-0.1 394
-0.1579
-0.0394
0.0827
-0.0139
-0.0604
-0.0132
-0.2168
0.0017
-0.0007
IH.D)
-0.1580
-0. 1238
-0. 0125
-0.2168
-0.0132
0.0589
0.0930
(U.DI
-0.5626
0. 1955
0.2289
0.0329
0.168 r
-0.5955
0. 1626
CHI- 3-00
CAHHA-_„U5 ZETA- 0.70 X/H
* 0. Y/H-— 1
.07 Z/H- 0.
ETA* 0.50
(H,LI
-0. 17 8 7
-0.0567
0. 1793
-0.1394
-0. 160 1
-0.0394
0.0027
IU.U
0.0116
0.0139
-0.0364
0.0132
-0.1992
-0.0017
0.0007
(U.0>
-0.1366
-0. 1047
0.0125
-0. 1992
0.0132
0.0626
0.0945
tU,D)
-0.4847
0.2024
0.2289
0.0547
0. 168?
-0.5394
0. 1477
CHI-15.00
GAMMA- 1.5
ZETA- 0.70
X/H- 0.
Y/H--1
1.87 Z/H- 0.
ETA* 0.50
(W,L)
-0.1656
-0.0410
0.1718
-0. 1253
-0. 1502
-0.0399
0.0847
tu
0.0664
0.0121
0.0630
-0. 1597
-C. 0086
0.0035
IW.D)
-0.0909
-0.0639
0.0591
-0. 1597
0.0630
C. 0688
0.0950
LUiDL
-0.3559
0.2005
0.2123
0.0513
0.1515
-0.4371
0. 1 192
CHl-3.Qa.00__
■ ■CAMWft.
ZETA- 0.70
X/H- 0.
Y/H=- 1
1.87 Z/H- a.
ETA- 0.50
(W,L)
-0.1302
0.0026
0.1886
-0.08G9
-0. 1150
-0.0413
0.0915
IU,L )
0.08P3
0. 1154
0.0622
0. 1078
-0. 1 155
-0.0194
0.0076
( W » D )
-0.0400
-0.0208
0.0989
-0. 1155
0. 1078
0.0755
0.0947
t U* D )
-0.2380
0.1716
0.1661
0.0855
0. 1034
-0.3235
0.0061
CHI-45.00
CAMWA- 1.5
ZETA-
0.70
X/H- 0.
Y/H—'
1.87
Z/H- 0.
ETA- 0.50
(H»L )
-0.0876
0.0589
0.221 1
-0.0452
-0.0662
-0.0424
0. 1041
(U.L1
0.0865
0. 1 353
0.0898
0.1223
-0.0879
-0.0358
0.0131
1 w ,01
-0.0054
0.00 15
0.1055
-0.0879
0.1223
0.0825
0.0894
tU.Dl
-0.1526
0. 1235
0.1065
0.0683
0.0424
-0.2209
0.05S2
CHL*40.J)_Q_.
£AMEA-_1*5
ZETA-
0.70
X/H- 0.
Y/H—'
1.87
Z/H- O.
ETA- 0.50
IW.tl
-0.0537
0. 1079
0.2516
-0.0160
-0.0201
-0.0377
0.1238
lUiLl
Q.0444
0. 1261
0.0920
0. 1070
-0.0776
-0.0626
0.0191
IW.01 _
0.0139
-0.0008
0.C758
-0.0776
0.1070
0.0915
0.0768
(U.oi
-0.0835
0.0706
0.0537
0.0435
-0.0053
-0.1269
0.0272
CHI-75.00
GAMMA- 1.5
4ETA-
0.70
X/H= 0.
Y/H—!
1.87
Z/H- 0.
ETA- 0.50
CN*U
-0.0243
0.1330
0.2650
-0.0158
0.0125
-0.0085
0. 1408
(U« L 1
-Q. 0 1 92
Q* 0979
0.0733
0.0813
-0.0745
-0.1005
0.0167
m>p)
0.0276
-0.0235
0.0221
-0.0745
0.0813
0. 1021
0.0510
IU*D1
-Q.0270
0.0262
0.0188
0.0200
-0.0163
-0.0469
0.0062
CHl-9fl*lliLZ_
JfiAMMA- U5-
Teta-
0. 70
X/H- 0.
Y/H — 1
1.87
Z/H* 0.
ETA- 0.50
cw.u~
0.0309
0. 1294
0.2535
-0.0325
0.0325
0.0635
0.1620
.. tU.LI
-0.0310
0.0571
0.0390
0.0684
-0.0684
-0.1001
-0.0112
fw.oi
0.0316
-0.0571
-0.0390
-0.0694
0.0684
0.1001
0.0112
(U.DI
-0.0000
0.0000
0.0000
-0.0000
0.0000
-0.0000
0.0000
152
TABLE 21.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y ~ 1.5, £ = 0.70, AND tj = 0.50
(b) y/H = -1.50
CHl — 3.00 CAVi'fis 1.5 ZET A = 0.70 X/H- 0. Y/H — 1.50 7/H- 0. CTA = 0.50
<W*U -0.2^40 -0.1157 0.3877 -0.224? -0.0952 -0.0591 0. 1092
1 U» L J -0.0162 -0.0201 — 0 - 1 * M 7 -0.0186 -0.3176 0.0024 -0i0016
<*»D> -0.2227 -0.2555 -0.016" -0.3176 -0.01F6 0.094B 0.0621
fU*D) -0.5770 0.2269 0.2976 0."317 0.2137 -0.6007 0.1952
CH I = 3.00 GAK*A= 1.5 ZFTA- 0.70 X/H= 0. Y/H"
«W*L) -0.2 t 'U0 -0.1157 0.3 r ‘79
1U,U 0.0162 0.0201 -0. 1 C 35
(W.D) -0.1935 -0.2350 0.M6E
t U * D ) -0.4P90 0.2425 0.2976
-1.50 7 /H= 0. E T A = 0.50
-0.2249 -0.10P9 -0.0591 0.1092
0 . " 1 P6 -0.2952 -0.0024 0.0016
-0.2952 0.0186 0 . 1017 0.0602
0- , '638 0.2137 -0.5523 0.1788
CHI* 1 5.00 GAMM A= 1.5 ZETA = 0.70 X/H= 0. Y/H— 1.50 It H* 0. tTA= 0.50
*W»L1 -0.2643 -0.0930 0.3222 -0.2046 -0.1154 -C.0598 0.1116
lUtU 0.0755 C. 0962 -C.0362 0.0831 -0.2412 -0.0126 0.0081
-0.1203 -0.1850 C.0790 -0.2412 0.0831 0.1129 0.0562
<b,D) -0.3462 0.2523 0.2740 0.1043 0.1091 -0.4509 0.1476
_CH.i»30 .00 GjftWtA* 1*5 7ETA = 0.70 X/H= 0. Y/H--1.50 l/H- 0. ETA= 0.50
l w »A> ..... -0.2114 -0.0306 0.3159 -0. 149? -0.0094 -0.0616 0. 1 192
tU«L) 0«. 11.99 0. 1662 0.0393 0.1483 -0. 1757 -0.0204 0.0179
— UfsDL. _ -0,0517 -0. 1255 0.1278 -0. 1757 0.14P3 0. 1240 0.0502
tUfDl -0.2235 0.2262 0.2095 0.1147 0.1220 -0.3381 0.1115
CHt-45.00 GAMHA- 1.5* ZFTA* 0.70 X/H* 0. Y/H— 1.50 Z/H = 0. ETA= 0.50
1 H ,L 1
-0. 1404
0.0468
0. 3334
-0.0859
-0.0424
-0.0626
0.1326
iuu.i
0.1113
0. 1943
0.0907
0.1632
-0. 1297
-0.0519
0.0316
1H,01
0.0046
-0.08F6
0. 1253
-0. 1297
C. 1632
0. 1 343
0.0411
(u,oj
-0. 144 !
0. 1 703
0. 1 309
0.0923
0.0415
-0.2364
0.0780
_CHI«60. 0Q GAHHA* 1.5 ZFTA- 0.70 X/H* 0. Y/H— 1.50 Z/H= 0. ETA= 0.50
IWfL.L -0.0985 0.1031 0.3498 -0.0431 0.0035 -0.0554 0.1512
0.0476 0.1373 0. 1 125 0. 1373 -C.1061 -0.0897 0.0500
* W f D > 0.0399 -0.081 1 0.0720 -0. 1061 0. 1373 0. 1460 0.0249
!U*D> -0.0543 0.104C G.06R2 0.n575 -0.0144 -0.1423 0.0465
CHI-75.00
G AHF A * 1.5
ZETA= 0.70 X/M= 0.
Y/H— 1
.50 Z/H= 0.
ETA* 0.50
<W,U
(U.U
<W,01
( Uy D )
-0.0558
-0.0421
0.0651
-0 .0332
0.1311
0. 1638
-0.0936
0. 0430
0.3456
0.1112
-0.0090
0.C289
-0.0378
0. 1006
-0.0937
0. 0250
0.0344
-0.0937
0.1006
-0.0212
-0.0180
-C. 1427
0. 1508
-0.0582
0.1609
0.0632
-0.0049
0.0186
CHI-90.00
GAPHA* 1.5
ZE TA * 0.70 X/H*
0. Y/H—
1.50 Z/H= 0.
ET A= 0.50
tWyl)
(U,L1
IWyCJ
lUyOt
0.0165
-0.0762
0.0762
-0.0000
C. 1 1 37
0.1292
-0. 1292
0.0000
0.3115
0.0099
-0.0899
0.0000
-0.0521
0.0812
-0.0812
-0.0000
0.0521
-0.0812
0.0812
0.0000
0.0686
-0. 1574
0. 1574
-0.0000
0.1658
0.0400
-0.0480
0. OOOO
6- tifix-i
L-15^9
133
TABLE 21.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1-5, C - 0.70, AND t? 0.50
(c) y/H = -1.125
8
Correction foctors for correcting from o wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
— — — 1
to ground effect
CHl — 3.00
G AHM A = 1.5
ZE TA =
0.70
X/H* 0. Y/H*-
1.12 z/h= a.
ETA* 0.50
IM.Lt
1UJL1
(WiD)
(U.0)
-0. U935
-0.0224
-0.3441
—0.6367
-0.1709
-0.0295
-0.4160
0.2808
0.7047
-0.2465
-0.0233
0.3960
-0.3502
-0.0264
-0.4668
0.0275
0,0627
-0,4668
-0.0264
0.2695
-0.1354
0.0041
0. 1226
-0.6662
0.1873
-0.0030
0.0508
0.2532
CHI* 3,00
GAKMA= 1.5
ZETA*
0.70
X/H* Q, Y/H*-
1.J2 Z/H= 0.
£TA= 0,50
(H*L )
. .J1UU .
<W,0)
(U.DI
-0.4935
0.0224 _
-0.3052
-0.5327
-
-0.1709
0.0295
-0.3927
0.3089
0.6426
-0.205.0
0.0233
0.3960
-0.3582
Q.0264
-0.4385
0.0750
0,0222
-0,43^5
0.0264
0.2695
-0. 1354
-0.0041
C. 1333
-0.6077
0.1873
0.0030
0.0458
0.2338
cai^j.5,oc _ _
CAPPA* 1.5
ZETA*
0.70
X/H* CL „JY/H*t.
1,12 _ U H= .0,.
£LA~ 0..5.Q ..._
[W,L )
iu.j.1 .
IW,D)
(UfO )
-0.4632
0. 1034
-C.21 12
-0.3620
-0. 1340
0. 1400
-0.3264
0.3346
0.5545
-0.1082 _
0.1001
0.3617
-0.3259
0.1244
-0.0270
-0.3625
-0,1373
-0,0210
0.1910
0.0157
-0.3625
0.1378
0.1244
0-2340
0,1513
-0.5006
0.0361
0.1968
CHI*30.00
GAMP A* 1.5
ZETA*
C.70
X/H* 0. Y/H—
1,12 Z/H= 0,
ETA- 0.50
( M * L )
iu,u
1W,D)
IU» 0 >
-0.3932
0.1570
-0.0913
-0.2264
-0.0373
0.2387
-0.2308
0.3094
0.5063
0.0109
-0.2402
0.2040
-0.0337
-0.2618
-0.1430
-0.0470
0.2029
0.0347
0.1676
0.2712
-0.2618
0. 1554
0.2040
0, 1403
0. 1705
-0.381B
0.0230
0.1540
CHI-45.00
GAPP A* 1.5
ZETA*
0-70
X/H* 0, Y/H—
1-12 Z/H= 0. .
_..ETA= 0.50
0 .501 4
0. 10Q4
-0, 1428
0.215 4 .
-0.0023
-0.1^47
-O. 1497
-0.0848
0.2228
0.0611
<W,L>
tu.u
(M t D)
IU,D1
-0.2925
0.1305
0.0052
-0. 15C7
0.0800
0.2764
-0.1796
0.2331
0.1496
0. 1682
-0. 1B47
0. 1240
0.2154
0.0360
0. 1899
-0.2746
0.0051
0. 1 142
CH 1=60. 00 .
GAMP A= 1.5
ZETA*
0.70
y/m- O Y/H*— 1 . 1? Z/H= 0.
ETA* O.SQ
( W,L )
tU,LJ
1W.D1
lUiDl
-0.2260
0.0291
0.0745
-o..ioua.
0. 169S
0.2699
0.5051
0, 1526.
-0.0785
.0,1724
0.0356
-0.1396 .
-0. 1475
-0. 1433
0.2463
0.0975
-0.0238
0.0750
-0.1633
0,1501
0.0604
0.0938 ...
-0. 1396
0.0743
0.1724
-Q.0262
0.2141
-O. LZA3
G APP A= 1.5
ZETA*
0.70
X/H* 0. Y/H —
1,12 i/H 0.
ETA* 0.5IL.„
CH[=_75,Q0
( W,L )
-0. 1721
0.2036
0.2540
-0.1868
0.0680
0.4897
-0.0644
0. 1214
-0.1143
0.0305
0 . 0609
-0.1143
-0. 1077.
0.2680
Q, 1327.
(U,L) .
tW,0)
(U,0)
-C. 10 11
0.1302
-0.0491
-0.0598
0.0463
0.1214
-0.0265
_ ‘ 0.2445
-0.0796
-0.0725
0.0375
CHI =90, 00
G APP A= 1,5
ZETA*
0.70
X/H* 0, Y/H®
-1^1.2 It H® 0,
ETA* 0.50
tW,L )
IU.L)
(W,D>
tU,D)
-0.0796
-0.1692
0.1692
-0.0000
0.101 1
0.2331
-0.2331
0.0000
0.4392
0.1765
-0.1765
0.0000
-0.0741
0.0942
-0.0942
-0.0000
C.0741
-0,0942.
0,0942
C.0000
-0.0050
-0.2635
0.2635
-0.0000
0.2552
0^1389
-0.1309
0.0000
13 k
TABLE 21.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 0.70, AND tj * 0.50
(d) y/H = -0.75
a
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
to grour
id effect
- Q,7Q. _ X/M* 0,
(U.L)
PUD )
DUD }
-0.52a?
-6.750*
-0.2003
-0,J3Jl2L
-0,5.995
1,1881
_-Q^i?sa
0.3594
-0,0319
0.5222
Y/H— 0,75 I/H-..CL*
-0. 5414__
-G*0l6fl_
_EIA* _Q.5fl _
0 . 3564
-0,64_4_B_.
0,02.02
-0. 664ft
-0. 0368
0.3313
-0,2946
0*006I_
O.J412^-
_ -0.0052
- 0.7706
0,731 _ X/H* 0.
Y/H--Q.7.5 2/R-.Q*
ETA* 0.50
DUk!
-LUmU_
-0.6 3 60
_-.flAQ.3QL_
-0.61S7
- 0.2003
— . 0.0 42 J _
-0.5713
0.4034
1.0712
0.0319
-0a5_414_
0.0368
— Qjl5222
-0 .6301
. - fl,63P1
-0 .2946.
o.oeeo
0,0368
0*3113
-0,1510
- Q. 706 7
CHI * 15.00
GAMA A* 1.5 ZETA*
DUD
-0.7891
0.1364
DU PI
-0. 3454
UUD1
-0.4090
-£HI- 30,00 CMFA?_ i*5_._ZEIA*
PUL)
. -0,6702
0. 1943
DUO)
^0. 16Q2
1U,P1
-0,2515
CHI* 4 5. 00
■ GAHHA- 1.5 ZETA*
PUL)
-0.546T
IU.L1
0.1349
DUO)
-0.0013
(U,D)
-0.1783
CHI-60.00
GAHHA* 1.5 ZETA*
IU.L 1
-0.4707
1 U, L 1
-0.0214
UUC1
0.1224
tu»m
-0.1346
CHI*75.00
PULI
-0,4200
HULL
-0.2flftfl
PU0)
JJ.2325
lU.OI
-0,0780
CHI-90,00
..GAMFA- 1.5 ZETA*
PUL)
. -0.323?
UU17
-0.3322
(HmDl
_ 0. 3322
1U.0)
-0.0000
Q*JQ x/mi.
_L/-it-^fl.7S ... _Z/H« 0.
-0 . 1416
0,i 983
-0.4797
_Q*
,4498^
0.8933
-Q.2047_
_ -0^14551
-0.4697
0-1713
- 0.5230
0,1 311 _
-Q.5230_
0, 1900
0.1713
-0.2995
- Q.Q346
0.2813
Q, 1 7 7 6
-0.5691 _
0.0433
-0*70 X/H-_Q*
-Y/H— CL.L5 IZH*
ETA* -0,50
0,0114
0.31 lk_.
0.7752-
0.4221-
0.2152
- 0.3S5 7
— Q.27JA-
-0.3692,
0,2060
Q.QS41
- -0.3692-
0*2718 _ .
0,1547
. ■-0, 3 145
-0. 0775
0.2090
-0,4575
0.3692
0.05961
0.0201
0.2160
0,70 X/H*, Q«
0.1954
0.37 73-.
-0.2600
0.3262
0.7422
0 . 1252
0.1712
27 H- Q,
‘0,2100-
-Q.2I3P_
_ -0.2468
6. 1601
ETA- 0 ,50 .
0.0501
rO.2466
0.2730
0.0258
-0,3367
0*2455
-0,3385-
0,70. X/H* 0,
0-3355
0.3732
-0.2410
0.2086
_r/H— Q.T5 1/ H- 0.
ETA* 0.50
0,7435
0.2190
0,0348.
_ Q, 1339 _
0.2075
-0. 1735
P.Q716
-0.1735
_ Q.2Q75
—0.0391
-0.2289
0.2959
0.1657
-0.0675
0.70 X/H* 0.
0.4036
Q. 3732
-0.2896
0.0999
0,70
0.4026
0.3942
-0.3842
0.0000
Y/H—Q.7S Z/H* 0.
0.7372
0.2771
Q.JA07
-Q. 1335
-0.3405
a ?3jh
-0.1390
-Q.1335
0.1407
0.3660
-O. 1561
0.0734
0,0356
-0.0315
-0.1117
0.0643
X/H- 0. Y/H--Q. 75
It H* 0,
ETA* 0.50 ~
... — :
—
0.6963
-0.0953
0.0951
-Q.2284_
0.4979
0,3171
0. 1059
-0. 1059
-0-43B0
0.2784
-0.3171
-0,1059
0. I059_
-0.4380
-0.2784
0.0000
-O.0Q00
0.0000
-0.0000
0*0008
6^1-1
L-15^9
135
TABLE 21.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0 70, AND rj = 0.50
(e) y/H - -0.375
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
fl oor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI— 3.00 GAHH A- 1,5 ZETA = 0.70 X/H = 0. Y/H=-0.37 If H- Q. ETA= 0.5Q
IHiL '
-1.2606
-0.1739
1.7193
-0.7295
0.7309
-0.531 1
0.5556
1U.L 1
-0.0368
-0.0552
-0.5433
-0.0472
-0.8637
0.0104
-0. QQBQ
(W.P1
-0.74PJ
-0.7436
-0.04 1 1
-0.9637
-0.0472
0.1230
0.1201
(U«P)
-0.9111
0.4637
0.6600
0.0117
0.3644
-0.9228
0.4520
CHI* _2*flfi £AH*A_« 1^5 ZE T A = 0.70 X/H = 0* Y/H=-Q.37 Z/H= 0. .... £TA 3 fl*5fi
<W.O
-1.2606
-0.1739
1.5360
-0.7295
0.5710
-0.5311
0.5556
(U, L 1
0.0368
<M>552
. -Q.4741
0 . 04 72_
-0.fi? 34
-0,0104
0.0QBQ
<W,D>
-0.6829
-0.7101
0.041 1
-0.8234
0 . 04 72
0.1405
0.1133
fU.PI
-Q.75QI
0.5223
0.6600
0. 1001
0,3844
-0,8506
0.4222
CHl«lS*.QQ GAHHA- I«5 ZETA = Q.7Q _ X/tii. 0* YZh^-Q.37 ZZH= 0. ET A = 0.50
IWrl> -1.1951 -0.0873 1.2507 -0.6542 0.3189 _ -0,5409 0.5669
IIW.1 . .. ft«.lA35._ ... 0,2582 - 0.28.65 0*2172 -0.6824 -Q.Q538 0.0410
IWtOl -0.5085 -0.5862 0.1858 -0.6824 0.21/2 0.1739 0.0963
tU?DI -0.4947 0.5845 0.5967 0.2213 0.3199 -0.7160 0.3632
CH J = 30. 00 _
GAXWA= 1.5
_ 1E_T A.* X/H*
0. Y/H— 0.37
Z / H - 0-
ETA 3 0.5Q
OJ,L)
-7*0365
0.1386
1*0588
-0.4649
0.1476
-0.5717
0.6035
1U.L)
0.2154
... . 0,4238
-0.0301
0.3341
-0.4696
-0. 1 187
0.0897
1 W , D 1
-0.2505
-0.4054
0.2634
-0.4696
0.3341
0.2191
0.0642
(U,D)
-0.3100
0.5463
0.44 Q9
0.2533"
0.1628
-0.5633
0.2930
CHI-45.00
GAMP A= 1.5 ZETA*
0.70 X/H 3 0
. Y/H--0.37 It H» 0.
ET A= 0.50
tW.L)
-0.8897
0.3982
fTolLI -0. 2686
0.0905
-0.6211
0.6668
0.1128
_fi. 4I6_L. . _
0. 17.42 0,3215
-0.2996
-0.2087
0. 1546
(W.D)
-0.0205
-0.2886
0.1924 -0.2996
0. 3215
0.2791
0.0110
(U.D)
-0.2331
0.4183
0.2858 0.1912
0.0149
-0.4243
0.2271
CHI-60.00
GAHWA= 1.5 ZET A =
0.70 X/H- 0
. Y/H—0.37 Z/H- 0.
ETA= 0.50
-0.8243
“076060
1 .0371 -0. 14Q6
0. 1012
-0.6757
0.7545
(U.U
-P. 1046
0.4764
0.3059 0.2345.
-0.1998.
-0.339 1_. -
0.24 IB
(W.O)
0. 1691
-0.2791
0.0104 -0.199B
0.2345
0.36Q9
-0.0793
lUtDJL
-0.1879
0.2681 ..
0 . 1845 0.1049
-0.0495
-0.2928
0. 1633
CHI-75.00
GAMHA- 1.5 ZETA*
0.70 X/H- 0
... Y/H--0.3t II H= 0,
ETA= 0.50
<U,U
-0.8044”
0.7372
1.0766 -0*_1 122
0.1086
-0.6921
0.8494
lU.Ll
-0.3547
0.4958
0.3960 O.1540
-fl. 1475
-0.5095
Q. 34 10
<w,oi
0.3536
-0.3742
-0.2220 -0,1475
0.1548
0.5011
-0.2267
1U.D1
-O. 1 172
0. 1327
0.1053 0.0394
-0.0352
-0.1566
0.0934 .
~Cl7l-90.00
__ CAHma- 1*5 ZETA- 0.70 X/H- 6,
. Y/H—0.37 ZZH= 0.
ET A 1 0.50
iw,u
-0.7421
0,8021 ...
1,0952 -0.1111
0.1111
-0.6310
0.9 13 fll
— Ui*L)
. ... -0.5466
Q. 5523
.0.4852 JU.14Q
-0. L140 -
. .-0.6626
0.4383
_ IHiDL _
0.5486
-0,5523
-p.4852 -0,1140
0.1140
0.6626
-Q.43B3
JU*D>
-0.0000
o.oooo
o.oooo -0,0000
0.00CQ
-0.0000
O.QQQO
156
TABLE 21.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 0.70, AND r; = 0.50
(f) y/H = o
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CHI =-3.00 G Af -
(H,L )
tU*L)
(W,D)
tU*Dl
^A = 1.5 7CTA= 0.70 X/H- 0. Y/H= 0. Z/H- 0. ETA- 0.50
-1.5555 — 0- 1111 1.8474 -O.R150 0.9192
-0.0369 -0.0627 -0.5641 -0.0518 -0.9533
-0.8843 -0.7284 -0.0482 -0.9533 -0.0518
-1.1219 0.6005 0.7882 0.0070 0.4070
-0.7404 0.7039
0.0151 -0.010B
0.0690 0.2249
-1.1239 0.5935
CHI- 3.00
G AMH A =
1.5
ZETA =
0.70
X/H= 0. y/h=
0.
If H* 0.
ET A- 0.50
<W t ll
IU,U
<U V D)
fU»01
-1.5555
0.0368
-0.8300
-0.9405
-0. 1111
0.0627
-0.6814
0.6597
1.6440
-0.4815
0.0432
0.7882
-0.8150
0.0518
-0.9107
0.1047
0.7236
-0.9107
0.0518
0.4070
-0.7404
-0.0151.
0.0807
-1.0452
0.7039
0.0108
0.2293
0.5550
CHI-15. 00
GAMHA-
1.5
ZETA =
0.70
X/H- 0, Y/H-
0.
Z/H- 0.
ETA- 0.50
IW.L1
(U»L 1
<W,D)
1U,D)
-1.4836
0. 1602
-0.6456
-0.6445
-0.0081
0.2931
-0.5265
0.7150
1.3311
-0.2617
0.2179
0.7150
~
-0.7230
0.2376
-0.7536
0.2396
0.4102
-0.7536
0.2376
0.3352
-0.7557
-0.0774
0.1080
-0.8841
0.7196
0.0555
0.2271
0.4754
[-30.00
GAHHA- 1.5 ZETA-
0.7Q X/H-
Y/H- 0.
Z/H* 0.
ETA- 0.50
(W,L)
-1.3157
0.2596
1.1399
-0.5118
0.1901
-0.8039
0.7714
IU.L1„
Q* 1927
0.4791
0,0317
0.3606
-0.5126
-0.1679
0-1185
tW.D)
-0,^549
0.3131
0.3126
-0.5126
0. 3606
0.1577
0. 1995
IU,D)
-0.4216
0.6493
0.5372
0.2736
0.1650
-0.6952
0.3756
CHI-45.0 0 G AME A « 1.5 ZETA» 0.70 X/M»^0._ Y/H- 0
1W,L) -1.1761 0.5696 1.1274
tV.il. . 0. 05 50 0.5364~ _ _Q-2540
<W,0) -0.0823 _-0. 1870 0.2423
1U.D1 -0.3170 0.4 843 0.3563
CHI-60.00 GAPNA*_1«5 ZETA- 0.70 X/H« n. y/H- 0
<H,LJ -I.ThOI 0.8303 I 1.2068
IU.L1 -0*1252 Q« 5320 5.3820
CW,D) 0.1597 -0.1980 0.0482
IU,D) -Q.2W3 0.3014 0,2269
CHI-75,00 . -ZLTA- 0.70 X/H* Q*. __ Y/H= 0
1H.U -1. 1565 1.0108 1.3080
IU.L) -Q.4781 0.54Q0 0.4566
1 H » D ) 0.4135 -0.3406 -0.2152
1U.D1 -0.1503 0.1446 0.1215
If H- 0.
ETA= 0.50
-0.2924
0.3409
-0.3208
0.2039
o. ner
-0.3208
0.3409
0.0100
-0.8836
-0.2859
0.2385
-0.5209
0.8620
0. 1955
0. 1338
0.2804
Z/H- 0.
ET A= 0.50
-0. 1608
0.2448
-0.2098 .
0. 1100
0. 1129
-0.2096
0.2448
-0.0536
-0.9792
-0.4445
0.3696
-0.3573
0.9911
0.2872
0.0119
0.1914
Z/H- 0.
ETA- 0.50
-0. 1201
0.1600
-0.1527
0.0407
0. 1165
-0. 1527
0.1600
-0.0366
-1,0364
-0*6381
0.5662
-0.1911
1.1389
0.3800
-0.1879
0.1039
CHI-90. 00
GAMMA- 1.5
ZCTA- 0.70 X/H-
-Q* Y/H- 0*.
Z/H- 0.
ETA- 0.50
( W, L )
(U*L J
(W.Ol
( U, D 1
-1.1224
-0.6976
0.6976
- 0.0000
1.1464
0.5927
-0.5927
0.0000
1.3924
0.5386
-0.5336
0.0000
-0.1170
0.1170
-0. 1170
0.0000
0.1170
-0. 1170
0.1170
- 0.0000
-1.0054
-0.8146
0.8146
- 0.0000
1.2633
0.4758
-0.4758
0.0000
6i£i-n
L- 15^9
137
TABLE 21.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, V = 0.70, AND 17 = 0.50
(g) y/H = 0.375
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
>d effect
.. X.K1*'J*.00_ ] f 5 ZETA* 0.70 X/H*
Y/H= 0.37 U h= 0.
(W.D
IU.U
1W,D)
til. D )
-1.5767
-0.0224
-0.9013
-1.4670
-0.0585
-0.0648
-0.4769
0.8600
1.2038
-0.3827
-0.0556
0.9745
-0.7295
-0,0472
-0.8637
0. n 1 17
E I A = 0.50
0.7309
-0.8637
-0.0472
0. 3P44
-0.8472
-0.0248
-0.0376
-1.47e7
0.6710
-0.0176
0.3868
0.8483
CHI* 3.00 GAMMA* 1,5
ZETA* 0,70 X/H* 0,
Y/H= 0.37 If H= 0.
IW.L) -1.5767
<U,l) 0.0224
IW,D 1 -0.8765
IU,D) -1.2787
-0.0585
0.0648
-0.3970
0.8975
1.0715
-0.2806
0.0556
0.9745
-0.7295
0.0472
-0.8234
0 . 1001
ET A= 0.50
0.5710
-0.8234
0.0472
0. 3844
-0.8472
-0.0248
-0.0531
-1.3788
0.6710
0.0176
0.4264
0.7974
, C H I -1 5. QQ SAW Ag_. U 5 ZETA* 0.70 X/M* 0, Y/H* 0.37 i/H= 0 .
(U t L)
IU.U
-1.5250
0.0917
0.0388
.. 0.3054
-0.2031
0.9009
0.8979
-0.6542
0,2172
-0.6R24
0.2213
0.3189
-0.8708
0.6930
Uj_D|_
tU,DI
-0.7493
-0.9510
0-2575
0.8978
-0,6824
0.2172
0.3199
-0.1255
-0.0669
-1. 1723
0.0081
0.4793
0.6796
CH 1*30. 0D
GAMMA* 1.5 7PJA=
_
0.37 Z/H* 0.
ETA* 0,50
.V« Y/H-
(W.L>
-1.4102
0.0750
0.2993
0^5096
0.0215
0.7707
0.8594
0.2301
0.4038
0.6980
-0.4649
0,3341
-0.4696
0.2533
0 . 1476
-0.9454
0.7641
1W.D)
-0.5106
-0,4696
-0.2592
0.1755
lUiDl
-0.6596
0. 5341
-0.04 10
0.4911
0 . 1628
-0.9130
0.5173
*
—
CHI*45. 00
GAMMA* 1.8
Z E T A *
0.70 X/H* Y/H* 0 37
Z/H* 0.
.ETA* 0 • 5 Q
IM.L1
-1.3361
Q« 6.LS..4 _ 0.9704
-0.2686
0 Q 2 D'
(UtL]
(W ,01
-0.0846
-0.2510
0-5765 0.4048
0.1338 0.3898
0.5452 0.4656
0.3215
-0.2996
0.1912
-0.2996 "
-1*06 7.S.
-0.4061
0. B87Q
0.2550
(U,D)
-0.4719
0.3215
0. 0485
0.4334
0.0149
-0.6631
0, 3539
.
“ — -----
—
■
CMI»60.00
GAMMA* 1.8
_ZETA=
0 .X/tL* .YZH* 0.37
- Z/H*
. ET A= Qj_5Q
( W»L )
— 1 • 3588
0.9061 1 . 1434
0.5417 0.4541
-0. I486
0.2345
-0. 1998
0. 1049
0 . 10 12
1 U.L>
-0*3290
- 1.2102
1.0547
(W,DI
0.0209
0.0924 0.2348
-P.J998
-0.5635
0. 3072
(UiP)
-0.3248
—
0. 3094 0.2651
0.2345
-0.0495
0.2207
-0,4297
0,2922
0.2046
CHI«75.00 ;
GAMMA =1.5
ZETA-
0- 70 X/H* 0,.. Y/H* 0.37
Z/H* 0.
ETA* 0^50
i«,Lj
-1.4028 "
t-nilT 1.3001
0. 4604 O li 1
- 0. 1122
0.1086
-LUxUL
-0.5573
-1.2905
1.2292
(M r D)
1U,0»
0.3358
-0.1716
T V Yj . , _ y f “ * jy
-0.0905 -0.0194
0.1233 0.1101
0, 1540
-0.1475
0.0394
-0.1475- .
0.1548
-0.0352
-0.7121
0.4634
-0.2109
0.3055
0.0571
0.0839
CH1»90,00 Gi
1MMA* 1-5
ZETA* 0.70 X/H* 0.
0,37 Z/H* 0.
ETA? 0.50
Y/H*
(M.U
~?T-3358
1.2335
0.3765
-0.3765
0.0000
-o.mt
0. 1140
-0. 1 140
-0.0000
IU.L)
-0,6563
1 3?0' >
.0*3475.
-0.3475
0.0000
0.1111
-1.2247
(W,0>
lUt D1
0.6863
-0.0000
-D, U40
0,1 140
0.0000
-0.8003
0.8003
-0.0000
1.3446
Q.2625
-0.2625
0.0000
138
TABLE 22
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 1.00, AND rj - 0.50
(a) y/H = -1-B75
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 — 1
to ground effect
CHT — 3.00 G A MV A * 1.5 ZETA- 1.00 X/H- 0.
Y/H— 1.87 Z/H* 0.
I U , L ) **0.1490
( 1) » L ) -0.013?
I D ) -0. If P0
ll),DI -0.3736
-0.0567
-0.0142
-0.1242
0.1796
0.0733
-O.C?52
-0.0140
0.2364
-0. 1057
-0.0142
-0.2100
0.0622
ETA- 0.50
-0.3312
- 0.2100
-0.0142
0.2134
-0.0433
0.0003
0.0221
-0.3958
0.0490
o.oooa
0. 0958
0.1174
CHI- 3.00 G AM M A* 1.5
( W f L ) -0.1490
( U , L ) 0.0139
[ H t C 1 -0.1652
(Ut D ) -0.2739
ZETA* 1.C0 X/H- 0.
-0.0567
0.014?
-0.1005
0.1888
Y/H — 1.87 Z/H* 0.
0.0705 -0.1057
-0.0605 0.0142
0.0140 -0.1877
0.2364 0.0831
ET A= 0.50
-0.3242
-0. 1877
0.0142
0.2134
-0.0433 0.0490
-0.0003 -Q.QOOQ
0.0225 0.0871
-0.3570 Q.105T
CHI* 15.00 GAMMA- 1,5
iwTtF -0.1358
1U.LI .0*0665
IHlOI -0*1188
( U, D ) -_o. 1827
ZETA- 1.00 X/H* 0.
-0.0408
0.0682
-0.0533
0.1896
Y/H— 1.87 Z/H- 0.
0.0822 -0.0913
-0. 0114 0. 0682
0.0667 -0.1421
0.2188 0.1053
ETA- 0.50
-0.2954
-0.1421
0.0682
0. 1952
-0,0445
-0.0016
0.0233
-0.2880
0.0505
-D.OQQO
0.0888
0.Q8M1
CHI-30.00 GAMMA- 1.5 ZETA- 1.00 X/H* 0.
Y/H— 1.87 Z/H- 0.
(VJ.L! -0. 1004 0. 0078
| U, L ) 0. 1 147 0. 11?4
|W t D) -0.0714 -C .0066
( U* D » -0. 1 1 14 0.1623
0.1239 -0.0517
0.0369 0.1105
0.1150 -0.0960
0.1687 0.1020
ETA* 0.50
-0.2353
-0.0960
0. 1185
0.1435
-0.0487
-0.0038
0.0246
-0,2134
0.0555
-Q, QQfl-L — _
0.0895.
0.0604
CHI-45.00
GAMMA- 1.5
ZETA-
1.00
X/H- 0.
Y/H — 1
1*8.7
It H- 0.
ETA- 0,50.
—
(W«L»
IU,LI
IH,D)
(U,D>
-0.0606
O.1309
-0.0467
-0.0697
0.0620
0.1302
0.0146
C. 1157
0.1827
0.0595
0. 13 14
C. 1019
-0.0036
0,1385
-0.0737
0.0775
-0.1605
-0.0737
0,1385
0.0738
-0.0570
-0.0077
0.0270
-0.1472
0,0656
-0*0003
0.0883
0.0383
CHI-60. 00
GAMMA- 1.5
ZETA-
1.00
X/H* C.
Y/H —
1.87
Z/H- 0.
ETA* 0.50
( H »L 1
Wall. _
-0.04 17
0. 1108
0.1 141
0. 1256
0.2402
0.0545
0.1116
0.0407
0.0294
0. 1269
-0.0757
0.0484
-0.0879
-0.0757
0.1269
0.0098
-0.071 1
-0.0161
0.0321
0.0847
-0.0013
0.0836
t«,D>
tu.p )
-0.0436
-0.0377
0.0079
0.0659
-0.0861
0.0175
ZETA- 1.00 X/H- 0.
Y/H*— 1 .97 Z/M= 0.
CW.LL
CU.L1
IW.01
-0.0629
0.Q625
-0.0440
-0.0079
0.1438
0.0932
-0.0185
0.0247
0.2798
0,0316
0.0627
0.0080
0.0253
0.1011
-0.0383
0.0239
ETA* 0.50
-0.0315
-0.0883
0.1011
-0.0172
-0.QB 82 0.1185
-0.0 387 -Q.QOIS
0.0444 0.0699
-0.0319 0.0008 —
CHI*90.jOO GAMMA- 1.5 ZETA* 1.00 X/H- 0. Y/H--1.87 Z/H- 0
(W,L)
... 1U.U
«u,D)
1U.0)
-0.0E34
0.0272
-C.0272
-n.oooo
0.1500
0.0551
-0.0551
O.OGOQ
0.2934
C . 0026
-0.0026
-0.0000
-0.0082
0.0927
-0.0927
- 0 .
ETA- 0.50
0.0082
-0.0927
0. 0927
0.
-0.0752 0. 1592
-0.0655 -CUOH6
0.0655 0.0376
- 0.0000 0.0000
6+£l-i
L-15^9
139
TABLE 22.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.00, AND 77 = 0.50
(b) y/H = -1.50
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00 GAMMA* 1.5 ZETA* 1.00 X/H* 0.
Y/H=-l .50 Z /H= 0.
ETA*
C. 50
IM,L 1
-8.2489
-0.1464
0.1350
-0. *>023
(Ufll
-0.0210
-0.0216
-0.2030
-0.0215
(W,c)
-0.2925
-0.2759
-0.0210
-0. 7409
(U,D)
-0.3224
0.1897
0.3181
0.0666
-0.34F6
-0.3407
-0.0215
0.2917
-0.0461
0.0004
0.0463
—0.3890
0.0564
- 0.0001
0.0649
0.1230
CHI* 3.00
GAMMA* 1.5
ZETA= 1.00 X/H *
0. Y/H=-
1.50 Z/H= 0.
ETA* C.5C
( WyL )
-0.2489
-0. 1464
0.1251
-0.202?
-0. 7460
-0.0461
(U»L 1
0.0210
0.0216
-0. 1697
0.021S
-0.3103
-0.0004
t W,D)
-0.2607
-0.2449
0.0210
-0.3103
0.C715
0 . 0496
(U* D )
-0.2504
0.211P
0.3181
0.1008
0.2919
-C.3511
0.0564
0.0001
0.0654
0. 1 m
_CH1* 15*00
GAMMA* 1.5
ZETA* 1.00 X/H*
0. Y/H*-!
1.50 Z/H* 0.
ET A= 0.50
<w,u
-0.2285
-0. 1230
0.1313
-0. 1811
-0.3179
-0.0474
_ I u , L 1
0.1002
0. 10 13
-C. 1001
0.1026
-0.2447
-0.0024
(U,0)
-0.1931
-0.1739
0.1003
-0.2447
0. 1026
0.0516
<u,0)
-0. 1433
0.2300
C.2909
0. 1407
0.264 1
-0.2040
0.0561
0.0008
0.0658
0.0894
CHI-30,
GAMMA* _1_, 5
ZETA* 1.00 X/H* 0.
Y/H = -
1.50 Z/H= 0.
ETA 1 C.50
[ W.L 1
-0.1738
-0.0502
0.1797
-0. 1220
-0.2461
-0.0518
(UjL )
0, 1713
0.1786
-0.0266
0. 1760
-0. 1743
-0.0055
( M, D )
-0. 1203
-0. 1080
0. 1714
-C. 1743
0.176?
0.0540
(U*D )
-0.0680
0.2090
0.2147
0. 1437
0. 1058
-C.2117
0.0638
0.0018
0.0655
0.0653
_CHI-45.QQ
GAMMA- 1,5.
ZETA* 1.00 X/H* 0.
Y/H=-1
.50 Z/H= 0.
ET A - 0.50
(My L)
tu.u
(M.D)
(11* D )
-0. 1120
0. 1925
-0.0773
-0.0346
0.0239
0.2069
-0.0704
0.1566
0.2527
0.0148
0.1927
0.1 162
-0.0515
0.2C35
-0.1341
0.1132
-0. 152C
-0. 134 1
0.2035
0.0839
-0.0604
-0.0110
0.0568
-0.1478
0.0754
0.0034
0.0637
0.0434
CHI-60.00 GAMMA* 1.5
(W,ll -0.0795
lli t Ll 0.1588
( My D ) -0.0629
(U,0) -0.0168
ZETA* 1.00 X/H* 0.
0.0925
0.1881
-0.0660
0.0951
Y/H=-t.50 It H = 0.
C. 32 33 -0.0043
0.0232 0.1319
0.1591 -0.1247
0.0347 0.0722
ETA : - 0.50
-0.0640 -0.0752
-0.1247 -0.0230
0.1819 0.0618
-0.0014 -0.0891
0.0968
0.0063
0.0567
0.0228
_CHI»75. 00 GAMP A * 1.5 ZETA* 1.00 X/H* 0. Y/H*-1.S0 Z/H= 0.
ETA- 0.50
IW,L)
1U .L1
1W,D1
_ fUjD)
-0.0997
0.0871
-0.0539
-C.00 16
0.1266
0.1494
-0.C833
0.0396
C. 7693
0.0144
0 . C ^ 6 8
0.C036
-0.0074
0.1410
-0.1276
0.0343
0.0008
-0. 1276
0.1410
-0.0270
-0.0923
-0.0539
0.0737
-0.0359
0.1340
0.0083
0.0443
0.0054
CH [-90.00
GAMMA * 1.5
ZFTA* 1.00 X/H*
0. Y/H=-1
1.50 Z/H= 0.
E T A = 0.50
1 M. LI
- 0 . l21 2
0.1337
0.3?44
-0.0428
0.0420
-0.0784
1 U*L }
0.0272
0. 11 34
0.0026
0. 1222
-0. 1222
-0. 0950
( W* D )
-0.0272
-0. 1134
-0.C026
-0.1222
0.1222
0.0950
fU.OJ
-0.0000
0.0000
o.onoo
-0.
0 .
-0.0000
0.1764
- 0.0088
0.0088
0.0000
TABLE 22.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K * 1.00, AND f? = 0.50
(c) y/H = -1.125
140
Correction factors for correcting from a wind tunnel which Is
closed
closed floor
open
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI— 3.00
GAMP A= 1.5
7E TA = 1,00
X/H— 0. Y/H— 1.12
Z/H* 0. .
_ ETA- 0 ,50
. .
< W,L )
-0.4692
-0.3212
0.3225
-0.4004
-0.2458
-0.Q6B8
0.0792
(U.U
-0.03J37. .
-0.0346
-0,41 65
-0.0343
-0,58Q4_ ...
0.00D6
-0.0003
IW.Dl
-0.519?
-0.5166
-0.0337
-0.5804
-0,0343
0.0612
0.0638
fU.Dl
-0.3410
0.2107
0.4427
0.0659
0.4076
-0.4069
0.1448
CHI* 3,00
GAMHA= 1.5
ZETA* _i,00
X/H- 0, Y /H* -1.12
Z/H- 0.
ET A= 0.5Q
( W. L )
-0.4692
-0,3212
0.2982
-0.4004
-0.2648
-0.0688
0.0792
tU, LI
0.03LL-
0.0346
-0.3701
0.0343
-0.5377
-0. 0006
0.0003
tw f o>
-0.4743
-0.4736
0.0337
-0.5377
0.0343
0.0629
0.0641
(U,D>
-0.2432
0.2554
0.4427
0. 1245
0.4076
-0.3676
0. 1310
CHI-15,00 ..
CAW A- 1.5
-IEXA? 1.00
X/H- 0. Y/H— _1* 12
. Z/H- 0.
ETA- 0,50
(U.U
-0.4344
-0.2821
0.26 17
-C. 3636
-0.2647
-0.0707
0.0815
(U,u
0, 1597
0.1646
-0.2643
0.1630
-0.4373
-0.0034
0.0016
(W,D)
-0. 3717
-0.3733
0.1598
-0.4373
0. 1630
0.0657
0.0640
(U.01
-0.0996
0. 3042
0.3982
0. 1983
O. 3623
-0.2979
0. 1058
CHI-30. 0D GAMHA* 1.5
7ETA* JUQ0
X/H— 0. Y/H=- 1 . 12
Z/H- 0.
ETA- 0,50
(V.L1
-0.3418
0,1751
0.2959
-0.2645
-0.2028
-0.0773
0.0894
tU.L I
0.2680
0.2796
-0. 14 1 1
0.2759
-0.31P4
-0.0079
0.0037
iM«Di
-0.2494
-0.2554
0.2683
-0.3104
0.2759
0.069Q
0.063Q
U1.01
-0.0080
0.2926
0.2764
0.2147
0.2300
-0.2227
0.0779
CH1»45^00__ GAWA=_ U5_, Z£ TA*. _J«.QD X/H* 0. Y./H— 1,12- Z/H= 0, _ ETA= 0,5a
(H,L)
-0.2381
-0,042?
0.3719
-0.1481
1U.L1
0.2911. .
—Qm 3138
-0.0532
_ 0.3068
(W,D)
-0,1644
-0.1776
0.2917
-0.2376
(U f D)
0,0164
0,2253
0. 1288
0.1728
-0,1037
-o<
-0.2376
_-Di
0.3068
0
0.0861
-0,
0900 0.1052
0157 0.0070
0732 0.0600
1564 0.0526
CHI-60. 00 GAWA=..1,5 Z£IA« UQQ X/H* 0. Y/H— 1.12 It H* 0. ETA=_G,5Q
tw,u tQ* IBIS 0.0636 0.4474
1U.L1 Q.229Q _ _ „Q*2Z*A_ -0.0196
1W.01 -.0*1178 -0.1461 0.2796
(U,D) _ 0,0128 0.1376 0.0237
•0.0702 -0.00B6
0. 26 13 -0.1956.
-0.19e6 0.2613
0.1085 -0.0234
-0.1116 0. 1338
-0.0323 0.01 33
0.0808 0.0524
-0.0957 0.0291
CHI-75.00
G A WA« 1.5 ZETA -
1.00
X/H= C. Y/H— 1
1. 12
Z/H= 0.
ETA= .0,50 _ .
. .
. ....
(W.L)
-0.2010
0. 1193
0.4947
-0.0632
0.0563
-0. 1378
0.1815
(U.U
0. 1204
0.2158
-0.0054
0. 1936
-0.1795
-0.0732
0.0223
(U.01
-0.08 1 1
-0.1474
0. 1206
-0. T795
0. 1936
0.0985
0.0321
(U,D)
0.0069
0.0573
-0.0016
0.0480
-0.0403
-0.0411
0.0093
CHI-90.00
1.5 . ZETA-
JL*_QQ.
X/H* 0. Y/H— 1
1.12
Z/H* 0.
ET A* 0.50
(H,L )
-0.2247
0* 1393
0.5095
-0.0942
0.0942
-0.1305
0.2335
hud
0.0273
Q. 1733
0.0025
0. 156 1
-0.1581
-0.1308 .
0.0152
(HyD)
-0.0273
-0.1733
-0.0025
-0. 158 1
0.1531
0.1308
-0.0152
(U, D)
-0.0000
0.0000
0.0000
-0.0000
0.0000
-0.0000
0.0000
6+^i- a
L-15^9
TABLE 22.- Continued
Ikl
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.00, AND rj = 0.50
(d) y/H = -0.75
Correction factors for correcting from
o wind tunnel
which is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
1
CHI--3.00 GA*MA= 1.5 ZETA
= 1.00 X/H=
1
3. Y/Hs-0.75 Z/H= 0.
ET A= 0.50
< W,L )
-0.8916
-0.6604
0.8420
-0.7788
0. 1960
-0. 1 128
0. 1 184
IU.L)
-0.0558
-0.0572
-o.eno
-0.0567
-1.0050
0.0009
-0.0004
(W,D)
-0.9497
-0.9166
-0.0559
-1.0050
-0.0567
0.0553
0.0884
IU.D1
-0. 3967
0.2398
0.6186
0.0544
0.5677
-0.4512
0. 1854
CHI - 3.00 CAMHA= 1.5 ZETA
* 1.00 X/H*
3. Y/H=-0.75 Z/H= 0* ...
£TA= 0 ■ 5Q
(W,LI
-0.09 16
-0.6604
0. 7304
-0.7788
0, 1019
-0. 1 128
0. 1184
(Udl
0.0558
-0.7361
P.Q567
-0*9455 _
-0.0009
0.0004
CK,CI
-0.8889
-0.6561
0.0559
-0.9455
0.0567
0.0567
0.0894
IU.01
-0.2513
0.3244
0.61 86
0. 1566
0.5677
-0.4080
0.1678
CH1= 15.00 1,5 _ i£I*
1.00 X/M= JL. ... Y/H=-0.X5 Z/ii* o .
ETA= 0,50
( W»L )
-0.8242
-0.5864
0.5807
-0.7082
-0.0178
-0. 1 160
0. 121B
(U,U .
0^6J7
0.2637
. -0.5652
0. 2664
-0,7825
-0.0C47
0.0023
<W f 0)
-0.7231
-0.6922
0.2623
-0.7825
0.2664
0.0593
0.0903
111,01
-0.0381
0.4280
0.5434
0.2926
0.4914
-0.3307
0. 1354
CH 1*30. 00 GAMHA- 1.5 ZETA
1.00 X /H** 0. Y/H=-0.75 If H* 0.
ET A- C . 50
IW,JJ
-0.6461
-0.3882
0.5215
-0.5215
-0.0467
-0.1266
0. 1333
]UtU
0.4241
0,4404.
-0.3405
0.4350
-0.5636
-0.0109
0.0053
1 Wt D )
-0.5001
-0.4745
0.4254
-0.5636
0.4350
0.0634
0.0891
(U,0>
0.0B42
0.4301
0.3464
0.3310
0.2911
-0.2469
0.0990
CHI-45.00 GAMMA* 1.5 ZETA
e 1.00 X/H* 0. Y/H=-0. 75 Z/H= 0.
ETA* 0.50
IW t L)
-0.4576
-0. 1 542
0.5539
-0.3103
0.0094
-0. 1472
0. 1561
<U»U
0.4347
0.4663
-0^1694
0.4561
-0.3946
-0.0214
0.0102
IW.Ol
-0.3245
-0.3105
0.4369
-0. 3946
0.4561
0.0701
0.0841
IU,D1
0.0906
0.3292
0.1314
0.2633
0.0710
-0.1727
0.0659
CHI-60.00 GAMMA* 1.5 ZETA-* 1.00 X/H=
.. Y/H=— 0.75 Z/H= 0.
ET A= 0.50
(H.tJ
-0.3537
0.0253
0.6101
-0.1715
0.0831
-0.1822
0. 1968
iu,u
Q«319J
0. 3812
-0,0719
0. 3623
-0.2950
-0.0433
0.0189
(W f D)
-0.2114
-0.223B
0.3224
-0.2950
0.3623
0.0836
0.0712
CU.O)
0.0511
0.1925
0.0068
0. 1567
-0.0572
-0. 1056
0.0358
CHI-75.00 GAMMA* 1.S ZETA- 1.00 X/H =
. Y/H=-0.75 Z/H= 0.
ETA= 0.50
I Wf L 1
-0.3659
0.1222
0.6475
-0. 1395
0.1323
-0.2264
0.2617
tU,L)
22
£*2849
-0.0246
0.2536
-0.2392
-0.0945
0.0313
(W, D1
-0.1252
- 0.2001
0. 1617
-0.2392
0.2536
0.1139
0.0390
(U,D1
0.0169
0.0758
-0.0067
0.0638
-0.0557
-0.0469
0.0119
CHI-90.00 GAM
MA= 1.5 ZETA* 1.00 X/H*
. Y/H=-0 .75 Z/H= 0.
ET A= Q.5Q.
■ - — -
( H f L )
-0,3909
0. 1 728
0.6591
-0. 1577
0.1577
-0*2332
Q.33QS
tU.LI
0.0273
0.2252
0,0025
0, I960
-0.1960
. -0,1667
Q. 0293
tw.oi
-0,0273
-0.2252
-0.0025
-0. 1960
0.1960
0.1687
- 0.0293
tu.PI __
- 0.0000
0.0000
0.0000
- 0.0000
0.0000
-O.Q0Q0
0.0000
TABLE 22.- Continued
142
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1.5, C - 1.00, AND t) - 0.50
(e) y/H = -0.375
8
Correction foctors for
correcting from
o wind tunnel
which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
1
0. Y/H— 0
*.37 _ 0*
O-SO
| WtL 1
-I.51B7
-1.1581
1.8627
-1*I353___
1.1728
-Q.1834
0. 1772
lU.l 1
-0.0R66
-0.0885
-1.2345
zO*OSZ9
rl*6Cll
Q.QQ13 _
-0*0006
UULI
U.D1
-1.5845
-I. 4487
-0.0871
-1.601 1
-0.0879
0.01 66
0. 1524
tU.Di
-0.5021
0.2876
0,8244
O.0JQ9
O. 7431
-0*5131
0.2567
rH f~ ^ 00 “
GAMMA* 1.5
2£TA-
o
o
X/H* 0*.
y/H*-a*3i
£IA?_ 0*50
“
-0.1834
-0.0013
0.1772
0.0006
(U.L)
-1.5187
-1.1581
1.5700 -1.3353
0.9055
(U.l 1
0^0866
0.0833
-U 24 3.1 ... 0-0879
- t b23 2
U.D)
1U.D)
_ ” -1.5074
-0*2873
-1.3670.
0.4270
--
0,0871 -1,5232
<3,8244 0* 1947
0*0319—
0,7431
0.0 158
-0, 4824 __
0.1562
0.2323
CHI * 1 5. 00
GAMMA* 1.5
ZETA*
1.00
X/H« 0.
Y/H*-0,37 I/H» 0.
EIA- 0.50
0.1821
u»u
- 1.3901
-1.0195
1.1360 -1,2017 ___
0,4927
-0.1B85
0. 3997
0.4095
-0.9764 0.4062
^1*2636
-0.0066
0.0032
U.D) _
-1.2476
0*3279
-1.1028
0.6348
0,4021 -1.2636
0.7057 0-4184
0.4062
0.6233
0.0160
-0.3905
0.1608
0. 1B65
"
CH1-3Q.00 .
GAMMA* 1.5
LET A*
1.00
X/H= 0.
. Y/H*-Q.37 .. . XZd*_Q*_.
EIA= 0.50
0. 1989
0.0073
1H.L)
tU>L 1
-1.3672
n.MTU
-0.6627
0-6.398
0,8413- -0.8617
-0.5836 Q.6325.
0.2248
-0*8786 ....
-0.20S5
-a. oi5i
u.oi
tU«Di_
-0*8585
0. 1902
-0*7180
0.6132
0.6230 -0.8786
0.4133 _Q.4791_
0,6325
0.3268
0.0201
-0.2892
0.1606
0.1338
rut.k«L nn gamma* 1_5
7FTA-
1 . 0Q
X/H* 0.
Y/h*-Q.37 Z/H- 0. .
EIA* 0.5Q
"
0.2318
U.U
IU.L1
U.D)
(U.D)
_-_Q » 7.433—
Q.5897
-0,5393
0.1672
-0.2IQI
0.6319
0.7607 -3 *5025
0.1628
-0.2383
-0.2754 0.6187
-0,5705
-0.0290
0.0132
-0,4182
0*4516
—
0.5991 -0.5705
0, 1302 0.3661
0.6187
0.0393
0.0311
-0.1989
0.1522
0.0855
CHI-60. 0Q
U*L )
IU.U
U.D)
<U,0)
7FTA*
1.00
X/H= 0.
vtu ., n „ , /H . n
ET A= 0.5Q
-0,5725
0.4023
-0.3320
0.0852
0.0098
0.4806
-0.2587
0.2466
0.7729 -0.2792
-n. 1025 Q.4S82
0,4152 -0.3879
-0.0035 0.2038
0 . 1 e 39
-0.3879
0.45B2
-0.0931
-0.2933
-0.056a
0.0558
-0.1187
0.2891
0.0224
0.1292
0.0428
CHI-75.00
GAMMA* 1*5
ZETA*
1.00
X/H* Q.
Y/H?-D»37 Z/H- 0.
ETA* 0,50
U.L)
. W»U
Ua_DI
(U.D)
-0.5767
0, 1908
-0.1817
0.0250
0.1626
0.3368
-0.2141
0.0897
0.7949 -0,2131
-0*0283 . 0*1055
0.2013 -0.29Q7
-0.0077 0.0775
0.2060
-0.29QI.
0.3055
-0.0691
-0,3634
-0.1147
0,1090
-0.0525
0.3760
0.0314
0.0766
0.0122
CHI -90, 00
GAMMA* 1,5
ZETA*
1.00
X/H?. 0.
7/H*rO*37 1 /
ETA* Q«5D
_ .
U,LI
IUaU
.UU.D1-
_1U.P1
-0.6038
0.0273
-0.0273
-0.0000
0.2488
0.2492
-0.2492
0.0000
—
0.8Q29 -0.2150
0,0024 0.2267
-0.0024 -0.2267
0.0000 -0.0000
0.2150
-0.2267
0.2267
0.0000
-0.3889
-0. 1 994
0. 1994
-0.0000
0.4637
0.0225
-0.0225
0.0000
6t£ I-l
L-1549
1^3
TABLE 22.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 100, AND tj = 0.50
(f) y/H = 0
Correction factors for
correcting from
a wind funnel
which Is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI=-3.00
GAf
'MA = 1.5
—
ZETA
= 1.00 X/H = 0. Y/H= 0.
r - ■
Z/H* 0.
ETA* 0.50
—
—
( Vi • L 1
1U,L 1
<W,C)
( (Jt D 1
-1.9614
-0. 1035
-2.027r
-0.6737
-1.3933
-0.1071
-1.6644
0.4005
2.5207
-1.5716
-0.1058
0.9013
-1.6633
-0. 1053
-1.9455
0.0143
1.E760
-1.9455
-0. 1058
0.0305
-0.2981
0.0023
-0.0022
-C.6380
0.2700
-0.0013
0.2812
0.3942
CHI* 3.00
GAM“A= 1.5
ZETA
1.00 X/H=
>. Y/H* 0.
7/H* 0.
ETA* 0.50
1 H » L 1
IU f L 1
(W,0>
I U» P )
- 1 .96 14
0.1035
-1.9484
-0.4 102
-1.3933
0. 1071
-1.5655
0.5712
2.1182
-1.4607
0. 1058
0.9010
-1.6633
0. 1058
-1 .*505
0.2136
1.4767
-1.0505
0. 1053
0.0305
-0.293 1
-0.0023
-0.0899
-0.6239
0.2700
0.0013
0.2930
0.3575
CHI* 15.00
GAMP A= 1.5
ZE T A =
1.00 X/H= 0
. Y/H= 0.
Z/H* 0.
ETA* 0.50
1W.U
f U» L 1
t W t D )
IU,D)
-1.7919
0.4734
- 1.6366
-0.0142
-1.2003
0.4916
-1.2297
0.7746
1,4634
-1.1263
0.4352
0.8366
-1.4857
0.4849
-1.5379
0. 4390
0.8371
-1.5379
0.4849
0.6341
-0.3062
-0.0115
-0.0987
-0.5031
0.2774
0.0067
0.308?
0.2857
CH 1=30. CO
GAMMA* 1.5
ZETA*
1.00 X/H* 0
. Y/H* 0.
Z/H= 0.
ETA* 0.50
(W,LI
1U.L1
( N ( 0 1
(U,D)
-1.3777
0.7104
- 1. 1430
0.1911
-0.7423
0.7502
-0.734 1
0.7539
1.0070
-0.6235
0.735?
0.4913
-1.D445
0.7359
-1.0460
0.5564
0.3079
- 1.0460
0.7359
0.3368
-0.3333
-0.0255
-0.0969
-0.3673
0.3022
0.0143
0.3119
0.2005
CHI*45. 00
G AMM A= 1.5
ZETA*
1.00 X/H= 0
. Y/H= 0.
Z/H* 0.
ETA* 0.50
{ H , L )
1UyL )
1W.D)
(U,D)
-0.9017
0.6502
-0.73 19
0.1710
-0.2469
0. 71 OR
-0.3585
0.5375
0.P661
-0.2400
0.6P95
0.1731
-0.5968
0.6957
-0.6548
0.4160
0.2422
-0.6548
0.6957
0.0205
-0.3849
-0.0455
^0.0772
-0.2450
0.3499
0.0231
0.2963
0.1215
CHI=60.00
G AMM A = 1.5
ZE TA*
1.00 X/H= 0,
. Y/H= 0.
Z/H* 0.
ETA* 0.50
(H.L1
(U.ll
(W.D1
(U.D1
-0. 7973
0.4222
-C.4573
0.0056
0.1014
0.5300
-0.1762
0.2703
0.8706
-0.0450
0.4718
0.0246
-0.3203
0.4996
-0.4233
0.2245
0.2303
-0.4203
0.4996
-0.1094
-0.4690
-0.0774
-0.0291
-0.1 389
0.4296
0.0303
0.2520
0.0538
CH 1=75. 00
GAMMA* 1.5
ZETA*
1.00 X/H* 0.
. Y/H= 0.
Z/H= 0.
ETA* C . SO
IW*L»
IU.U
IW,01
(U,D)
-0.R 177
0. 1910
-0.2462
0.0250
0.2963
0. 3494
-0. 1491
0.0932
0.9010
0.0105
0.2299
0.0026
-0.245?
0. 3265
-0.3117
0.QB31
0.2373
-0.3117
0.3265
-0.0746
-0.5725
-0.1340
0.0655
-0 .0502
0.5415
0.0229
0. 1626
0. 0101
CHI*90.OO GAPM A*
ZETA* 1.00 X/H* 0. Y/H* 0. 1/ M= 0.
ET A- 0.50
(U,L1 0.0273
CW,D1 -0.0273
(U,0) -0.0000
0.4034
0.2209
-0.2209
0.0000
0.9140
0.0024
-0.0024
0.0000
-0. 2307
0.2337
-0.2387
0.0000
0.2307
-0.2327
0.2307
-0.0000
-0.6156
-0.2115
0.2115
- 0.0000
0.6421
-0.0178
0.0178
0. 0000
TABLE 22.- Concluded
Ikk
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, < = 1.00, AND rj = 0.50
(g) y/H = 0.375
Correction foctors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
— , ■ — i 1
to ground effect
CHI — 3.00
gamma- 1,5
zcta=
1.00
X /H- 0.
YZH® C. 37
Z/H= 0.
ETA= 0.50
JWfL )
IU. LI
-1.81*02
-D.Q8U
-0.R923
-0.0934
1.6124
-1.C2B7
-1.3353
-0.0879
1.1728
-1 .6C1 1
-0.0879
0.74 31
ETA- 0.50
-0.5049
G.0067
-0.2892
-1.0209
0.4429
-0.0055
0.5194
0.7072
IU.O)
_
CHI- 3.00
-1.8903
-0.9899
GAMMA= 1.5
ZF r a =
-1.0817
0.73S1
1-00
X/H* 0.
-0.0926
1.0997
Y/H= 0.37
-1.601 1
0.0309
Z/H = 0-
(W,L >
(U.L»
-1.8402
0.0811
-0.8923
0.0934
1 .3592
-0.9135
-1 . 3353
0.0879
-1.5232
0. 1747
0.9055
-1.5232
0.0679
0.7431
-0.5049
-0.0067
-C.3188
-0.9321
0.4429
0.0055
0.SS44
0.6472
C H»D>
(Ur 0)
-1.8420
-0.7375
-0.9688
0.8419
0.0926
1.0997
CHl-15.00
GA8MA- 1.5
ZETA =
1.00
X/H= 0.
Y/H= 0.37
Z/H= 0.
ET A= 0.50
(H.L)
1U.L)
IW.0I
(U.D)
-1.7211
0.3721
- 1.6210
-0.3386
-0.7459
0.4337
-0.6622
0.9409
0.9864
-0.6030
0.4299
0.9768
-1.2017
0.4062
-1.2636
0.4184
0.4927
-1.2636
0.4062
0.6233
-0.5194
-0.0342
-0.3574
-0.7570
0.4558
0.0275
0.6014
0.5225
CH1*_3A* QJQ_-
GAMMA- 1.5
ZE FA-
1.00
X/H- 0.
Y/H= 0.37
Z/H= 0.
ET A= 0.50
(W,l)
LU_*L)
(H«D»
(U.P)
-1.4293
0.5617
-1.2454
-0.0678
-0. 3631
0.6877
-0.2601
0.8451
0.7874
-0.1966
0.6787
0.6675
-0.8617
0.6325
-0. 8786
0.4793
0.2248
-0.8786
0.6325
0.3268
-0.5676
-0.0703
-0.3668
-0.5472
0.4985
0.0552
0.6185
0.3657
CHl*45*.Qa
gamma- 1.5
ZETA =
1.00
X/H= 0.
Y/H= 0.37
1/ H= 0.
ETA= 0.50
—
(W.L 1
(U*L )
IH.D)
(U,0)
- 1. 1 597
0.5085
-0.B9P3
0.0123
0.0757
0.6977
0.0153
0.5335
0.8107
0.0836
0.6802
0.3446
-0.5025
0.6187
-0.5705
0. 3661
0.1629
-0.5705
0.6187
0.0393
-0.6573
-0.1102
-0.3279
-0.3538
0.5782
Q. 079 !
0.5857
0.2174
CHI-60. OC
GAMMA= 1.5
ZE 7 A~
1.00
X/H= 0.
Y/H= 0.37
It H* 0.
ET A=* 0.50
(H.L )
(U.L )
( W » D )
CU« 01
- 1.0748
0.3115
-0.6151
0.0152
0.4224
0.5406
0. 1044
0.2956
0.9256
0. 1P06
0.5060
0.1343
-0.2792
0.4582
-0.3879
0.2038
0. ie39
-0.3879
0.4582
-0.0931
— C. 7956
-0. 1468
-0.2272
-0.1886
0.7017
0.0824
0.4922
0.0917
CHI-75.00
GAMM A= 1.5
ZETA-
1.00
X/H= 0.
Y/H= 0.37
Z/H= 0.
E T A= 0.50
(H.L)
(U.L)
I W. D )
(U.D1
-1.1654
0. 12R0
-0.3393
0.0077
0.6386
0.3350
0.0354
0.0895
1.02B3
0. 1293
0.2642
0.0343
-0.2133
0.3055
-0.2907
0.0775
0.2060
-0 . 2907
0.3055
-0.0691
-0.9520
-0. 1775
-0.0486
-0.0699
0.8519
0.0295
0.3261
0.0119
CHI-90.00
GAMMA- 1.5
ZE TA =
1.00
X/H= 0.
, Y/H= 0.37
Z/H* 0.
E F A= 0.50
(W.L)
(U.L)
(H.D)
(U,01
-1.2280
0.0272
-0.0272
-0.0000
0.7422
0.1312
-0.1312
0.0000
1.0674
0.0023
-0. 0023
0.0000
-0.2150
0.2267
-0.2267
-0.0000
0.2150
-0.2267
0.2267
0. 0000
-1.0130
-0.1995
0.1995
-0.0000
0.9571
-0.0955
0.0955
0.0000
6i£T-n
L-15^9
10S
145
TABLE 23
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND 17 = 0.50
(a) y/H = -1.875
Correction foctors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI=-3.0Q
GAP«A= 1.5
ZETA*
2.CC
X/M* C,
. Y/H=—
1.C7
Z/H® C.
ETA* 0.50
( W , L I
(U,l)
tW,D)
(U,D)
-0.0402
-0.0143
-0.1428
-0.0600
-0.0210
-0.0143
-0.C916
0.2C13
- 0 . loor
-0.0743
-0.0143
0.2522
-0.0305
-0.0143
-0.1442
0 . 1 361
-0.5442
-0.1442
-0.0143
0. 2587
-0.0098
-0.0000
0.0014
-0. 1961
0.0095
0.0000
0.0526
0.0652
CH I = 3.00
GAMMA® 1.5
ZETA*
2.00
X/H® 0.
Y/H=-
1 .87
Z/H= 0.
ETA* 0.50
1W.L1
(li.LI
IW,0)
( U • D I
-0.0402
0.0143
-0. 1157
-0.0268
-0.021C
0.0143
-0.0642
0.2064
-0.0966
-0.0468
0.0143
0.2622
-0.0305
0.0143
-0. 1171
0. 1498
-0.5333
-0.1171
0.0143
0.2537
-0.0C98
0.0000
c . on 1 3
-C. 1766
0.0095
-0.0000
0.0528
0.0586
CHI* IS. 00
_ .GAM* A* t>5
ZETA*
2.00
X/H® 0.
Y/H=-
1.07
Z/H® 0.
ETA= 0.50
tW,L )
IU.L1
IW.C)
(U'D)
-0.0241
0.0687
-0.0640
0.0143
-0.0042
0.0685
-0.0120
0.2039
-0,0716
0.0056
0.0664
0.2445
-0 .0140
0.0687
-0.0652
0. 1568
-C.4965
-0.0652
0.068 7
0.2409
-0.0101
0.0000
0.0012
-C. 1425
0.0098
-0.0002
0.0532
0.0471
CHI® 30. 00
GAHM A = 1.5
ZF T A =
2.00
X/H* 0.
Y/H*- 1
1.87
Z/H® 0.
ETA* C . 50
(W,L )
( U » L 1
( W , D )
(u r r )
0.0210
0.1195
-0.0155
0.0275
0.0431
0.1191
0.0368
0. 1687
-0.0137
0.0545
0. 11RP
0.1940
0.0322
0.1195
-0.0167
0. 1 340
-0.4259
-0.016Z
n. 1 195
0. 1901
-0.0112
O.OCOO
0.0012
-0. 1065
0.0109
-0.0004
0.0535
0.0347
CHI=45. 00
C APM A ® 1.5
2 F T A *
2.00
X/H* 0.
Y/H®— 1
1.67
7/H* 0.
ETA® 0.50
(w,L )
IU,L )
(W,P>
IU.CI
0.0793
0.1397
0.C026
0.0155
0.106 1
0. I38e
0.C549
0. 1 142
0.0620
0.0727
0.1383
0.1247
0.0929
0. 1397
0.0013
0.0905
-0.3390
0.00 13
0. 1 397
0. 1200
-0.0136
0.0000
0.0013
-0.0751
0.0132
-0.0009
0.0536
0.0237
CH I =60 . 00
GAMMA* 1.5
7E T A =
2.00
X/H® 0.
Y f\\- — 1
.37
Z/H® 0.
ETA® 0.50
1M.Lt
1U.LJ
(W V CI
CU,D)
0. 1273
0.1265
-0.0137
0.00C1
0.1641
0.1243
0.0381
0.0595
0. 1382
0.0560
0.1231
0.0540
0. 1460
0. 1265
-0.0152
0.0463
-0.2520
-0.0152
0. 1265
0.0487
-0.0166
0.0000
0.0016
-0.0462
O.OIfll
-0.0022
0.0534
0.0132
CHI* 75.00
GAH M A = 1.5
7F TA*
2. 00
X/H* 0.
Y/H*-t
.87
Z/H* 0.
ETA® 0.50
(W«L )
( U, L )
(4,0)
(U,C>
0.1310
0.0940
-0.0548
0.0006
0. 1932
0.0372
-0.0058
0.C215
0. 1992
0.0123
0. 0° 32
0.006C
0. 1622
0.°945
-0.0578
n.01~9
-0. 1788
-0.0578
0.0945
-0*0024
-0.0312
-0.0006
0.0030
-0.0183
0.0309
-0.0073
0.0520
0.0026
CHU90.00
Gamma* 1.5
7 E T A =
2.00
X/H® C.
Y/H=-l
.07
Z/H* 0.
ETA* 0.50
( W , L )
( U, L )
iw,p>
IU.CI
0.0648
0.0084
-0.0804
-0.0000
0. 1325
0.0563
-0.0563
o.cone
0.^2 7 8 2
-C.C365
C.C365
-P.OOOO
0. 1173
0.0995
-C.0995
-0.0000
-0. 1170
-0.0995
0.0995
0.0000
-0.0530
-0.0111
0.Q1 1 1
-0.0000
0.0647
-0.0433
0.0433
0.0000
146
TABLE 23.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND tj = 0.50
(b) y/H = -1.50
Correction foctors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
to free air
closed
on bottom
only
to ground effect
00
GAMP A ■ 1.5
ZETA- 2.00 X/H=
0. Y/H=-1
.50 Z/H* 0.
ETA* 0.50
U»L>
ii.o)
JC,DI
0.0649
0.13R5
-n. i3f*5
-0.0000
0. I7EB
0. 13C4
-0. *304
0.0000
0 . 2 7 B 5
-C.0O33
0.0933
-0.0000
0.1130
0.1630
-0. 1630
-0.0000
-0.1130
-0.1630
0. 1630
0.0000
-0.0481
-0.0245
0.0245
-0.0000
0.0658
-0.0326
0.0326
0.0000
6+r6i- r r
L- 15^9
147
TABLE 23.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, C - 200 ' AND I? = 0.50
(c) y/H = -1-125
—
Correction foctors for
correcting from
a wind tunnel
which is
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
—
GAHHA- 1.5
— 1 »
ZETA* 2, QQ X/H.* 0, Y/H*-
, 12 _ 2/H- q*_
.... ETA* 0,50
-0.2300
-1.1363
-0.5450
-0.0400
0.6408
-0.0120
0,0000
0.0191
0.0125
0. 0000
0.0443
(Wall
-0.2419
-0.2175
-0.5924
1U.LI
-0.0400
-0,0406..
-0,4574
-0.0400
(Ha 0 1
-0.525?
-0.5007
-0.0399
-0.5450
tU.D)
0.0285
0. 2979
0.6452
0.2240
—
ETA* 0.50
-1.1092
-0.477SL
0.0400
0.6408
■ - ■
CHI- 3.00
GAWWA- 1.5
ZETA* 2.00 X/H
* 0. Y/H=— 1
.12 Z/H* 0.
-0.2300
-0.0120
-O.QQOO
0,0191
-0.1761
{HaLl
-0.2419
-0.2 175. .
-0.5741
-o.anoo
0.0445
0.066S
1U.L1
Q.Q4O0
0 . 0.4.00 .
-Q.1P98
O.OUQQ
IW.01
-0.4587
-0.4333
0.0399
-0.4779
0.2776
1U.P)
0.10J6_
0.3441
0.6452
* 0. Y/H—
1 . 12. . _ It H* O,
.ETA* Q, 5Q.._
CHI-15.00
GAMHA* 1.5
ZETA* 2.00 X/H
-0.4941
-0.2559
-0.1883
0. 1916
_ n n 1 9k
0.0129
(Ha t- 1
(U.L )
-0.2006
0.1915
-0. 1 75U
0.1914
—1.01 38
-0,3447
-0.0001
0.0192
-0.1422
-0.0001
0.0448
0.0535
(W.D)
-0.3255
-0.2999
0.1912
-0. 1447
0.1916
(U.D)
0.1069
0.3825
0.5948
0. 3290
0.5902
CHI ■3D, 00 GAHH A- 1 ,5 ZETA* .2,00. JLZ1L* Jk Y/H* ^1.1 2 Z/M-. .0 ...... . ETA* 0.50
(H,L1 -0.0871
(U.L1 0 ±3314
(U,0L -0.1956
(U,Q ) 0.199J _
0.0591 _ -0.3236_
0 J31i. =&*AZSi t
Q.1699_ __ _ 0.3329
0.3450 _ 0.11510
-0.0734 -0.8272
-0.2)49.
-0.2149 0.3338
0,3055 0.4459
-0.0137
-0,0002—
0.0193
-0. 1064
0.0143
-0.0003
0.0450
0.0396
« 1 .5 ZETA* 2.00 X/H» 0- Y/H— 1..12 _ Z/H* 0* ETA* 0.50
[ W t L )
0.0522
0.0862
-0. 1080
0.0688
-0.5975
-0.0166
(U.L )
2^3919
PJill ...
. -0.J16.9Q .
0,3924
-0. 1586
-D, 0005 _
(Hi D 1
-0.1392
-0.1136
0.3904
-0. 15B6
0.3924
0, 0194
(U.P)
0.1486
0.2510
0,2545
0,2238
0,2485
-0,0752
0.0174
-0.0005
0.0450
0.0272
CHI-60.00 GAHHA* 1.5 ZETA«_ 2 .-6Q X/ii*Q«-._- Y/H* -1,1 2 It H* 0. E T A * O .SO
IH,L!
0,1494 0.1961
0.1053
0. 1722
(U.L)
0.3612 -0,3412-
-0.0911
0.3624
(W.Ol
-0.1608 . -0.1359
0.3579
-0. 1806
(U.0)
0.0875 0.1498
0.0653
0.1342
CHI*75. 00
GAMMA* T. 5 ZETA* 2.00
X/H* 0. Y/H* -1.12
If H- C
(W, L)
0.1262 0.2046
0.2753
0. 1641
0.2066 0.286?
-Q. 1542,
0,2913
_ IHiDL “
-0,2214 -0.1999
0,2758
-0.2429
Ui*£l__
0.0475 0.0708
-0^03 13_
0.0668
CJU-90.QO
J1AKMA-. 1,5 ZETA- 2.00
X/H* 0* . "mi--U12
Z/H* <
(H.L )
-0.0140 0.1320
0.3919
0.0494
IU.I >
(L.249D Q.248Q
0.1911 _
..o.zaoii
(Ha 01
-0.249Q -0.2480
0.1971
-0,2800
(UaD)
-0.0000 0.0000
0.0000
-0.000Q
-0.3709
-5, 1606.
0,3624
0.0574
-0.0223
- 0.0012
0.0196
-0.0467
EJA^JJ^Q.
-0.1871 -0.0379
-0.2429 -D.0Q47
0.2913 0,0215
-0,0422 -0.0153
-0.0494 -Q.Q634
-0.2800 tO.H310
0.2800 Q. 0310
Q.0000_ ^0»QOQQ
0.0239
-O.QOI3
0.0447
0.0156
0.0405
_dO»mnLi
0.0430
0.0040
0. 0023
-Q. 0320
(LTL32IX
0.0000
148
TABLE 23.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND tj= 0.50
(d) y/H * -0.75
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free oir
to ground effect
CHI *-3. 00 G AMV A = 1.5 ZETA* 2.00 X/H* 0.
Y/H=-0.75 It H* 0.
ETA* 0.50
I Uf L }
-0.0313
-0.7913
-0.7610
-0.9112
-1.3944
-0.0200
0.0199
( U , L )
-0.0059
-0.0856
-1.2503
-0.0059
-1.3634
0.0000
0.0000
<U f 0)
-1.3554
-1.2993
-0.0850
-1. 3634
-C.0859
0.0081
0.0641
(U.D1
0.0473
0.3646
1.1743
P.7665
1.1676
-0.2191
0.0981
CHI* 3.00 GA«PA* 1.5
ZETA* 2.00 X/H* 0,
Y/H=-0.75 Z/H* 0.
0.50
(W,L)
-0.8313
-0.7913
-0.7614
-0.R1 12
-1.3039
-0.0200
0. 0 19V
(U«L)
0.0859
0.0850
-1.1272
0.0859
-1.2410
rQ.QQQQ
-0. 0000
IU.DI
-1.2331
-1. 1765
0.0858
-1.2410
0.0859
0.0079
0.0646
tU.D)
0.2056
0.4913
1.1748
0.4030
1.1676
-0. 1975
0.0882
CHI*15*QCL
GAMP.A? .1*5.
ZE TA= 2.00 X/H*
.0, Y/H*
-0.75 1 / H= 0.
. ET A* Q_,5Q
- -
(Uf L )
-0.7450
-0.7038
-0.6682
-0.7243
-1.2715
-0.0207
0.0205
tUlU
0.4102
0.4100
.. -0.3630
. 0.4102
-0*9708
. -0.00Q0
-0.0002
(W,D)
-0.9711
-0.9136
0.4096
-0.9788
0.4102
0.0077
0.0652
(Uf D 1
0.4034
0.6335
1.0637
Oj* 5627
1.0564
-0.1593
0.0708
(Uf L )
-0.511 1
-0.4653
-0.4017
-0.4881
-0.9846
-0.0230
0.0228
(U* L 1
0.7073
0.7068
-0,5811
0,70 73.
-0.6971
. -0.0000
-0.0006
(U,D>
-0.6894
-0.6315
0.7060
-0.6971
0.7073
0.0076
0.0656
(Uf D)
0.4562
0.6270
0.7514
0.5749
0.7434
-0.1 187
0.0520
CHl*45*0_0_
gamma* 1^5
ZETA* 2.00
X/H*
0 ,
Y/H*-0.75
Z/H- 0,
ETA* 0.50
(W,L1
-0.2330
-0.1785
-0.0462
-0.2061
-0.6112
-0.0278
0.0276
CU,LI
0.8140
0,M29
-0.4202
0.8141
... -0*5364
-0,0000
-0.0012
(Uf O)
-0.5285
-0.4708
0.8112
-0.5364
0.8141
0.0078
0.0656
(UfDI
0.3697
0.4882
0.3451
0.4529
0.3356
-0.0832
0.0353
CHI*60. 00
GAMP A* 1.5
ZETA* 2*0.0 .
X/H- O.
Y/H— Q. 75
U H* 0.
ETA* 0.50
( Uf L 1
-0.0551
0.0204
-
—
0.2919
-0.0173
-0.2562
-0.0378
0.0377
Q*7272
0.7247
-0,3031
0.7274
-0,4989
-0,0002
-0.0028
( W, D 1
-0.4902
-0.4340
0.7207
-0.4989
0.7274
0.0066
0.0649
(U.D)
0.2385
0.3083
0.0065
0. 2890
-0 .0058
-0.0505
0.0193
CHI-75.00
GAMMA* 1.5
_ 7 E TA = 2.00
X/H*
0.
Y/H=-0. 75
It H* 0.
ETA* 0,50
{ H.L1
-0.0915
0.0329
0.5335
-Q*_0296
0,0013
-0.0619
0.0625
(U,U
0.5621
0.5555
-0.3967
0.5642
-0.5103
-0.0021
-0.0087
(UfO)
r0. 4984
-0.4486
0.5423
-0.5103
0.5642
0.0119
0.0617
( U, D )
0.1 177
0.1408
-0.0924
0. 1370
-0. 1000. ...
-0,0194
0.0037
CHI = 90. 00.
GAMMA* 1.5
ZETA* 2.00
X/H*
. 0 .
Y/H=-0. 75
Z/H* 0.
_EIA= Q*1Q 1
(U t L )
-0.2729
-0.0530
0.6745
-0.1711
o.iln
-0,1018
0*1161
(Uf L 1
0.4609
0.4444
-0.3R55
0.4889
-0.4089
-0,0200
-Q.Q445
(U.O)
-0.4609
-0.4444
0.3855
-0.4869
0.4809
0.0200
0.0445
(Uf D)
-0.0000
0.0000
0.0000
-0.
0.
-0.0000
0.0000
L-1549
L-15^9
TABLE 23. - Continued
1^9
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 2.00, AND 77 = 0-50
(e) y/H = -0.375
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air to ground effect
CHI=-3. OO _GAMMA = 1.5 . ZETA= 2.00 X/H = (1, Y/H=-0.37 If H= 0. ET A = 0.50
(W.u -3,153? . . -3.0702 1.5456 .. -3.1152 0.7841 -0.0387 0.0371
fU.l) -0.226? -0.2267 -3. 8539 -0.2269 -4.0231 -0.0001 0.0001
tW,D) -4.0502 -3.9064 -0.2267 -4.0201 -0.2269 -0.0301 0.1137
(U,0) -0.0534 0.3659 2.2546 0.2177 2.2706 -0.2711 0.1482
CHI= 3.00 G AMM A = 1.5 Z E T A = 2.00 X/H* 0. _ y/H=-0„37 If H= 0. ETA= 0.50
1 W t L 1
-3. 1539
-3.0782
1.1547
-3. 1 152
C . 40 77
-0.0387
0.0371
CU,L 1
0.2269
0.2267
-3.6195
0.2269
-3.7621
0.0001
-0.0001
(W.Dl
-3.8130
-3.6673
0.2267
-3.7P21
0.2269
-0.0309
0. 1 148
(U» D I
0.3P26
0.7599
2. 2046
0.6266
2.2706
-0.2440
0.1333
CHI * 15.00
G AMM A * 1.5
ZE TA- 2.00 X/H =
0. Y/H= -0 * 3 7
Z/H= 0.
ETA* 0.50
(W,L )
-2.8727
-2.7946
0.6504
-2.0328
-0.0711
-0.0399
0.0383
( U f L )
1.0658
1.0648
-2.9652
1,0654
-3. 1299
0.0003
-0.0006
(W.D)
-3.1619
-3.0135
1.0645
-3. 1299
1.0654
-0.0320
0. 1164
iu,d>
0.9744
1.2770
1.9797
1. 1706
1.9654
-0.1962
0.1065
CHI* 30. 00
C AMM A* 1.5
ZETA* 2.00 X/H = 0.
Y /H=-0 .
,37 Z /H - 0.
ETA* 0.50
IW.Ll
-2.1302
-2.0436
0.5073
-2.0860
-0. 1870
-0.0442
0.0424
ru,Li
1.7408
1.7385
-2.0881
1.7400
-2.2543
0.000R
-0.0015
IW.Cl
-2.2870
-2.1369
1 . 7377
-2.2543
1.7400
-0.0326
0.1174
(U, D 1
1. 1791
1.4014
1.1800
1. 324 1
1.1644
-0. 1450
0.0773
CHI = 4 5. 00
GAMMA*
1.5
ZE T A = 2.00
X/H= C.
Y/H*-0- 37
Z / H= 0.
ET A= 0.50
IW.Ll
t U . L )
( w • 0 1
< U p 0 1
-1.2945
1.8260
-1.6109
0.9534
-1.1902
1.8213
-1.4610
1.1039
0.7078
-1.4120
1.8196
0.3021
-1.2413
1. 0244
-1 .5785
1.0530
0.03T7
-1.5705
1.8244
0.28 W
-0.0532
_ 0.0015
-0.0324
-0.0996
0.0511
-0.0031
0. 1174
0.0509
CH 1*60. 00
GAMMA*
1.5
ZE T A = 2.00
X/H* 0.
Y/H*-0 . 37
Z/H* 0.
ET A* 0.50
IW.L )
(l),L )
(W.D)
(U* D )
-0.7578
1.4527
-1.2103
0-5694
-0.6171
1.4423
-1.0643
0.6522
0.9793
-1.0149
1.4383
-0.2063
-0.6860
1 . 4494
-I. 1P00
0.6267
0.3325
-1.1800
1.4494
-0.2287
-0.0713
0.0033
-0.0304
-0.0574
0.0689
-0.0071
0.1156
0.0255
CHI=75.00
GAM»A=
1.5
ZE TA= 2.00
X/H= 0.
Y /M=-0 .37
Z/H* 0.
ETA* 0.50
(W.L )
IU.L1
(W.C1
IU.C)
-0.6717
1.0219
-0.9790
0.2371
-0.4462
0.993P
-0.8486
0.2572
1. 1503
-0.7951
0.9005
-0. 1978
-0.5580
1.0146
-0.9566
0.2554
0.5294
-0.9566l
1.0146
-0.2228
-0.1137
. O.DD7L
-0.0224
-0.0183
0. 1098
... -0.Q2QB
0.107?
0.0016
CHI =90. 00
gamma*
1.5
zr TA= 2.00
X/H= 0.
Y/H=-Q« 37
Z/H* 0.
ETA= 0.50
fW.L 1
( U» L 1
-0.8092
0.775R
-0.4428
0.7067
1.2124
-0.6484
-0.6308
0.7839
0.6308
-0.7539
-0.1790
-Q.Q08I
0.1880
-0.0772
<W,01
(U.0)
-0.7758
-o.onoo
-0.7067
-0.0000
0.6484
0.0000
-0.78 39
-0.0000
0.7839
0.0000
0.0081
-0.0000
0.0772
0.0000
150
TABLE 23.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1-5, C - 2-00, AND ij> 0.50
(I) y/H » 0
Correction factors for correcting from a wind tunnel which is
closed
on bottom
only
to free oir
closed
on bottom
only
to ground effect
-6*7406
-0*4213
-7.9112
-0-3287
-6.6532
- 0.4232
-7.7822
0.0572
7.5039
-7.782 2_
-0.4232
3.3221
CHI*. 3*00 l* 5 _
6.8436
- 7*1666
0.4227
3.3572
-6.6532
0 * 4232 —
-7.4340
Q.3546_
IH>U
. lUtU
|W t Dl
(U,0 I
A±-l*5 2LI &
-5.9180
2.1398
-5.9426
1*9396
-6. 1516
1.9559
-O.Q902
Q.QQ12 .
-0.1360
-0,2760
CHI * 30 *.00. __5AM{*Ah_ 1*.5 itTAi.
-4.3224
2.0330
.X/H* CL. Y/H- Q,
-0.0996
0 • 0020
-0.1383
-0.2007
-2.3873
.2*1822
-2.6190
1.6641
0.9690
- 2.6190 _
2.7029
0.0819
- 0.1373
-0.1327
-1.1628
1 * 2815 .
- 1.4837
0.1S03
-Q.QJ7L
0.2293
CHI»75.00
1.5
It TA= 2.00 X/H* 0. Y/H- 0. ...
Z/H* 0.
(W.L >
-1.2166
-0.7557 1.7064
-0.9806
IU.L1
1.3371
1*2585 -0.9990
1. 3062
1W f 0)
-1.3545
-1.0397 1.2475
-1.2467
itljDl
0.3186
0.3290 -0.2530
0.3325
CHI*90^00 _
GAMHA* 1.5
7ETA- 2.00 X/H* 0. Y/H= 0.
It H» 0.
tW,LJ
-1.2978
-0.6153 1.6496
-0.9549
IU.L1
0.9981
0.8112 -0.7638
0.9549
KW^D)
-0^9901
-0.8112 0.7638
-0.9549
(U.0)
- 0.0000
0.0000 - 0.0000
0.0000
0,9511 _
-1*2467
1.3062
-0.2986
0.9549
.-0*9549.
0.9549
-0.0000
- 0.10 78
_-O*0J4O
-0*1428.
0*0412
-0.0432
-0,0000
0.3391
_ - 0.1437
0*1437
0.00 00
L-15^9
151
TABLE 23.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND rj= 0.50
(g) y/H = 0.375
CHI — 3.00
GAMMA- 1,5
/ETA* 2.00 X/H*
0, Y/H=
0.37 Z/H* 0.
El A* 0.50
—
—
(W.Ll
-3.3569
-2.8804
2.0362
-3. 1 152
0.7841
-C.2417
0.2349
( U* L 1
-0.2273
-0.2263
-3.501 1
-0.2269
-4.02Q1
-0,0004
0.0005
(W.O)
-4.4080
-3.5227
-0.2263
-4.0201
-0.2269
-0. 3879
0.4974
(U, 0)
-0.4458
0.7509
2.3831
0.2177
2.2706
-0.6635
0.5332
CHI- 3.00
GAMMA* 1.5
ZETA* 2.00 X/H*
0._ Y/H*
0.37 If H* 0,
ETA* 0.50
(W»L J
-3.3569
-2.B804
1.6312
-3. 1152
0.4077
-0.2417
0.2349
( U , L )
0.2273
0.2263
-3.2513
0.2269
-3.7821
0.0004
-0.0005
<W,D)
-4.1812
-3.2731
0.2263
-3. 7821
0.2269
-0.3991
0.5090
<U,01
0.0299
1.1057
2.3831
0.6266
2.2706
-0.5967
0.4792
CHI -15. 00 GAMMA * 1.5 ZETA- 2.00 X/H* 0. Y/H* 0.37 If H= 0. ETA* 0.50
IW.Ll -3,0616 -2.5911 "" 1.1029 -2.0328 -0.0711 -0.248R 0.2418
l_U|_L > _ 1.0678 1. 062 6 -2.5830 _ 1.0654 -3.1299 0.002 4 -0.0028
( Wf D ) -3.5441 —2.6049 1 . 0624 -3.1299 1.0654 -0.4142 0.5249
lU t Dl 0.6968 1.5490 2.0799 1.1706 1.9654 -0.4737 0.3764
-0.2731
_ 0,0P5.L
-0.4217
-0. 3352
0.2653
-0.0069
0.5331
0.2631
IMjL)
-1.5631
-0.9289
1.1170
-1.2413
0.0377
-0.3218
HI. LI
1.8367
1.8097
-1.0289
1.8244
-1.5785
0.0122
< W,D1
- 1.9940
-1.0512
1.8089
-1.5785
1.8244
-0.4155
IU, D 1
0.8453
1.2086
0.4137
1.0530
6.2839
-0.2078
0.3124
-0.0147
0.5273
0. 1555
C HI-60.0 0 GAMMA* 1. 5 2E T A - 2.00 X/H* 0, Y/H- 0.37 2/H-0* ETA- 0.50 .
(U,U -1,0979 -0.2869 1.3721 -0.6860 0.3325 -0.4119 0.3991
|U,L» 1.4783 1.4146 -0.6597 1.4494 -1.1800 0.0290 -0.0348
1 HfO ) -1.5664 -0.6813 1.4127 -1.1800 1.4494 . -0,3165. 0.4987
IU.D) Q. 5362 0.6027 -0.0961 0.6267 -0.2287 -0.0905 0.0559
CHL-I5.O0 _GAMMA=.. 1.5 ZEIA = 2.00
1 M ■ L 1 -1.1271 -0.0092
(.11, LI 1,093 ft 0.9148
(W.D1 -1.2663 -0.5340
1U.0) 0.2517 0.2402
X/H= 0. Y/H - 0.37 Z /H* Q.
1.5225 -0.5580
-0.51 Q9 1.0146
0.9087 -0.9566
-0.1281 0.22S4
ETA- 0.50
0.5294 -0.5691 0.5408
-0^9546 0.0792 -Q. 0997
1.0146 -0.3096 0.4226
-0.2228 -0,0036 -0.0152
CHI-90.00 GAMMA* 1.5 ZETA* 2.00 X/H = 0. Y/H- 0.37 1/ H- 0. _ErA2_jft^5Q
<w,u
-1.3715
0.0906
1 . 5394
-0.620ft
0.63QS__
-0.7407
0.7213
1U|U
0.9363
0,5149
-0.4379
0.7839
-0. 78 39
0.1524
-Q»269IL
tW.D)
-0.9363
-0.5149
0.4879
-0.7839
0.7839
-0.1524
0.2690
<U,D>
- 0.0000
0.0000
0.0000
-0.0000
0.0000
-0.0000
0.0000
152
TABLE 24
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 4.00, AND rj = 0.50
(a) y/H = -1.875
CHI — 3.00 GAMMft= 1.5 Zf.TA = 4.00 X/H- 0. Y/H — 1.87 It H- 0. ETA= 0.50
(W P L) -0.0059 -0.0031 -0. 1*66 -0.0045 -0,5033 -0.0014 0.0014
-0.0142 -0.0142 -C.04P5 -0.0142 -0.0P46 -0.0000 0.0000
(W,D) -0.0054 -0.0570 -0.C14? -0."846 -0.0142 -0.0007 0.0277
IU.D1 0.0987 0.2310 0.2695 0.1971 C.2691 -0.0984 0.0339
CH 1= 3.00 1.5 ZETA* 4.00 X/H* 0. Y/H— 1.87 Z/H* 0. ETA = 0.50
(W P t) -0.0C59 -0.0031 -C. 1433 -0.0045 -0.5763 -0.0014 0.0014
IU,L1 0.C142 0.0142 -0.0203 0.0142 -0.0564 0-0000 -0.0000
(y,C) -0.0572 -0.0237 0.0142 -0.0564 0.0142 -0.0007 0.0277
|U,n 0.1159 0.2350 0.2695 0.2045 0.2691 -0.0886 0.0305
CHI= 15.00 G AM W A - 1.5 ZFTA* 4.00 X/H* P. Y/H— 1.87 Z/H= 0. ETA- 0.50
| W » L ) 0.01 13 0.0142 -0. 12C1 0.0128 -0.5466 -0.0015 0.0014
(tl,tl 0.0681 0.0630 O.C332 0.0681 -0.0030 0.0000 -0.0000
1W P CI -0.003P 0.0248 0.C65C -0.0030 0.0601 -0.0008 0.0278
U1 P D1 0.1284 0.2246 0.2520 0.2000 0.2516 -0.0716 0.0246
CHI= 30. 00 GAMVA^ 1.5 ZET A* 4.00 X/H= 0. Y/H— 1.87 It H* 0. ET A= 0.50
JW f L) 0.0603 0.0635 -0.0642 0.0619 -0.4840 -0.0016 0.0016
|U f Ll 0.1180 0.1179 0.CS2G 0.1180 0.0465 0.0000 -0.0001
<H,0) 0.0457 0.0743 0.1179 0."465 0.1130 -0.0008 0.0278
1U.D1 0.1102 0.1024 0.2022 0.1640 0.2016 -0.0530 0.0184
CH 1*45. 00 GAMMA* 1.5 ZET A* 4.00 X/H* 0. Y/H— 1.87 Z/H= 0. ETA= 0.50
1W,L) C. 1265 0.1304 0.0092 0.1285 -0.4046 -0.0020 0.0019
|U»t) 0.1366 0.1364 0.1009 0.1366 0.0646 0.0001 -0.0002
1W # DJ 0.0638 0.C924 0.1364 0.0646 0.1366 -0.0008 0.0278
( U • D ) r .0697 0.1212 0.1340 0.1081 0.1333 -0.0384 0.0130
CHI-60.00 GAMMA* 1.5 ZETA* 4.00 X/H= 0. Y/H— 1.P7 Z/H= 0. ETA* 0.50
(W,L> 0.1907 0.1962 C.O026 0.1935 -0.3259 -0.0028 0.0027
(U,U 0.1196 0.1191 0.PP27 0.1195 0.0464 0.0001 -0.0004
(W,D) 0.0456 0.0742 0.1190 0.0464 0.1195 -0.0008 0.0279
|U t D) 0.0270 0.0596 0.0654 0.0515 0.0645 -0.0245 0.0081
CHI-75.00 GAMMA* 1.5 Z£TA* 4.00 X/H- 0. Y/H— 1.87 Z/H= 0. ETA* 0.50
(H P L) 0.2299 0.2400 0.1383 0.2351 -0.2641 -0.0052 0.0050
(U,L) 0.0752 0.C733 0.0334 0.0747 -0.0029 0.0004 -0.0015
tH.CJ -0.0036 0.0249 0.0727 -0.0029 0-0747 -0.0007 0.0278
( U a D ) 0.0022 0.0165 0.0144 0.0133 0.0129 -0.0111 0.0032
CHI-90.00 GAMMA- 1.5 2ETA= 4.00 X/H* 0. Y/H— 1.37 Z/H* 0. ETA= 0.50 _
<W P L) 0.2034 0.2386 0.1725 0.2199 -0.2199 -0.0165 0*0187
(U,L1 0.0647 0.0390 -0.0303 0.0653 -0.0653 -0.0007 -0.Q264
CW.Ol -0.0647 -0.0390 0.0303 -0.0653 0.0653 0.0007 0.0264
(U,c) -0.0000 0.0000 O.COOO -O.OOOO O.OOOO -0.0000 o.oooo
6^l“ r l
L-15^9
153
TABLE 24.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 4.00, AND 1 ) = 0.50
(b) y/H = -1.50
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
■ 1 r
to ground effect
i
CHI=-3.00
GAHMA* 1.5
7 1 : T A *
4.00
X/H= 0.
Y/H®- 1
.50
1/ H= 0.
ETA® 0.50
IW.L1
IU,L1
(U.C)
IU,0)
-0.0151
-0.0?23
-0.1511
0. 1077
-0.0126
-C. 022 3
-0. 1354
0.3145
-
0.4440
0. 1200
■0.0223
0.4183
-0.0138
-0.0223
-0.1577
0.2818
-0.9076
-0.1577
-0.0223
0.4179
-0.0012
0.0000
0.0066
-0.094 1
0.0013
0.0000
0.0222
0.0328
CHI = 3.00
GAHM A * 1.5
ZE TA =
4.00
X/H® 0.
Y/H®— 1
.50
Z /H* 0.
ET A = 0.50
tW,L)
(U*L>
(M«D 1
(U»D)
-0.0151
0.0223
-0. 1073
0.2112
-0.0126
0.0223
-0.0916
0.3255
■0.4348
0.0761
0.0223
0.4133
-0.01 38
0.0223
-0. 1 1 39
0.29^0
-3.0945
-0.1 1 39
0.0223
0.4179
-0.0012
-0.0000
0.0066
-0.0047
0.0013
-0.0000
0.0223
0.0295
CH1*15.00
GAHM* 1.5
ZETA =
4. CO
X/H= C.
Y/H=- 1
.50
Z/H= 0.
ETA® C.50
(UtL 1
(U,L J
(W f 01
cu.rj
0.01 16
0.1065
-0.0242
0.2252
0.0143
0. 1065
-O.CO*5
0.3175
-0.3914
0.0071
0. 1065
0.3909
0.0129
0. 1065
-0.0308
0.2937
-0.0443
-0.0308
0.1065
0.3905
-0.0013
-0.0000
0.0066
-0.0685
0.0013
-0.0000
0.0223
0.0238
CH 1=30.00
GAHP A= 1-5
ZETA =
4.00
X/H = 0.
Y/H=- 1
1 .50
Z/H® 0.
ET A = 0.50
IW,U
IU,L )
(W,0)
IU»D>
0.0074
n. 1 PUS
0.0529
0.1913
0.0903
0. 184P
0.C6P6
0.2606
-0.2965
0.0^4?
0. 1347
0.3127
0.0889
C. 1848
0.0463
0.2428
-0.7423
0.0463
0. 18 48
0.3122
-0.0014
-0.0000
0.0066
-0.0515
0.0015
-0.0000
0.0223
0.0178
CHI *4 5. 00
GAH0A® 1.5
zr t a ®
4. CO
X /H= 0.
Y/H=-l
1.50
Z/H= 0.
ET»= 0.50
{ W v L 1
( U , L J
C W , C ]
IU.CJ
0.1095
0.2 144
n.oc io
0.1236
0.1931
0.2143
0.096?
0. 17 30
-0.1749
C. 1124
0.2142
0.2055
0.1913
0.2144
0.0745
0.1603
-0.6145
0.0745
0.2144
0.2049
-0.0010
-0.0000
0.0066
-0.036e
0.0018
-0.0001
0.0223
0.0127
_ CH1*60.00
GA^PA® 1.5
ZTTA®
4.00
X/H= 0.
Y/H = -
1.50
7/H® 0.
El A= 0.50
( W i L )
lUtLI
I W * 0 )
IU,CI
0.2560
0. 1009
0.0528
n.053?
0.291?
0.1837
0.0686
0.0846
-0.0533
0- 1 °?4
0 .097 3
0. ? n 93
0. IP 89
0.0462
0.0767
- C. 4873
n . 0462
0.1889
0.0964
-0.0025
-0.0000
0.0066
-0.0235
0.0025
-0.0002
0.0223
0.0079
CHI-75.00
GAvy A= 1.5
/r ta=
4.00
X/H = 0.
Y/H=-
1 .50
Z /H- 0.
ETA® 0.50
<M.L I
IU.L >
IW t 0)
III* D I
o.3unn
n. ir 39
-C. 0229
C.O 113
0. 3501
0. 123C
-0.00 72
0.C254
0 . 04 3 3
0.0094
0- 13? 1
0.C1 61
0.3454
0. 1240
-0.0295
0.0222
■0.3251
-0.0295
0.1240
0.0146
-0.0046
-0.0001
0.0066
-0.0109
0.0047
-0.0010
0-0223
0,0033
CHI-90.00
GAMY A = 1.5
zcta®
4. CO
X/H- 0.
Y/H=-
1.50
Z/H= 0.
ETA® 0.50
<W,L )
( U i L )
IH.CI
<U»C I
0.2911
0.1130
-0. 1 130
-0.0000
0. 3240
0 • 09? r
-0.099?
-0.0000
0.1134
-C . 05 37
0.0^37
0.CO0O
0. 3056
0. 12CC
-0.1208
-0.0000
-0.3056
-0. 1208
0. 1208
0.0000
-0.0145
-0.0070
0.007B
-0.0000
0.0184
-0.0210
0.0210
0.0000
TABLE 24.- Continued
154
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND rj = 0.50
(c) y/H = -1.125
Correction foctors for correcting from 0 wind tunnel which Is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00
GAHPA- 1*5
7ETA-
4.00
X/H* 0. Y /H-
IN,L)
-0.0557
-0.0524
—1.0489
(U.L)
-0.0397
-0.0397
-0.3055
(UfOl
-0.3423
-0.3263
-0.0397
1U.0I
0.3317
0.4672
0.7321
CHI- 3.00
. „GAMHA= 1.5
Z E TA =
4.00
X/H= 0. Y/H=-
Tm,li
-0.0557
-0.0524
-1.0254
IUf L )
0.0397
0.0397
-0.2288
( H , 0 1
-0.2657
-0.2496
0.0397
(U.D1
0. 374 1
0.4961
0.7321
-1.1? It H- 0. Q.SC
-0.0541 -1.5709 -0.0017 0.0017
-0.0397 -0.35C2 0.0000 0.0000
-0.3502 -0.0397 0.0079 0.0239
0.4293 0.7315 -0.0776 0.0379
1.12 It H= 0. ETA= C.50
-0.0541 -1.5428 -0.0017 0.0017
0.0397 -0.2736 -0.0000 -0.0000
-0.2736 0.0397 0.0079 0.0239
0.4620 0.7315 -0.0979 0.0341
CHT-15. 00 GAJWA* 1*5 ZETA* 4.00 X/H* 0.
V /H=- 1.12 If H- 0. ETA- 0.50
( W y L 1
-0.0091
0. 1902
-0.1 196
C.4005
-0.0056
0. 1901
-0.1035
0.4990
-0.9356
-0.0627
0.1901
0.6830
-0.0074
0. 1902
-0. 1275
0.4715
-1.4450
-0. 1275
0.1902
0.6824
-0.0017
-0.0000
0.0079
-0.0710
0.0018
-0.0000
0.0240
0.0275
CHI-30.00
GAPFA= 1.5
7E TA * 4.00 X/H«
O. Y/H*- 1 . 12
Z/H= 0.
E T A= 0.50
( W,L)
0.1224
0.1263
-0*7529
0.1243
-1.253G
-0.0019
0.0020
j
0.3303
0.3303
0.0532
0.3304
0.0083
-0.0000
-0. 0001
1 H * U )
0.0162
0.0323
0.3302
0.0083
0. 33C4
0.0079
0.0240
tUiO )
C. 3429
0.4169
0.5429
0. .3962
0.5422
-0.0534
0.0206
CHI-45.00
gahma* i.s
7E TA = 4.00 X/H*
0- Y/H*-1
.12 Z/H= 0.
£T A= 0.50
(W.L)
0.2971
0.3019
-0.5237
0.2995
-1.0173
-0.0023
0. 0024
(Uii i
0.3848
0.3847
C. 1032
0. 3848
0.0582
-0.0000
-0. 0001
(W,D)
0. 066 1
0.0822
0. 3°46
0.0502
0.3848
0.0079
0.0240
. f Uf 0 )
P.2261
0.2788
0.3502
0.2642
0.3494
-0.0381
0.0146
CHI -60. 00
GAMP A = l.S
/ E TA =
4. 00
X/H= 0.
Y/H*-
1 . 12
Z/H* 0.
ETA* 0.50
IW*U
_ iu»u
(W t D>
(U,D>
0.4565
0.3442
0.0175
0.1059
0.4632
0.3439
0.0336
0.1393
-0.2941
0.0546
0.3435
0. 1544
0.4598
0. 3442
0-0096
0. 1301
-0.7810
0.0096
0.3442
0. 1533
-0.0033
-0.0000
0.0079
-0.0243
0.0034
-0.0003
0.0240
0.0091
CHI- 7 5. 00
GAPMA* 1.5
7ETA =
4.00
X/H- 0.
Y/H=—
1 . 12
Z/H* 0.
ETA* 0.50
-
— (W»U
(U,U
!U f 0)
iu .01
0.5229
0.2445
-0.1101
0.0251
0.5352
0.2434
-0.0941
0.0499
-0.1045
-0.0731
0.2420
0.0P96
0.5289
0.2445
-0. 1180
0.0462
-0.5848
-0.1180
0.2445
0.0076
-0.0061
-0.50G1
0.0080
-0.0112
0.0063
-0.0012
0.024Q
0,003?
CH1-90.00
GAMPA* 1.5
7ETA*
4.00
X/H* 0.
Y/H*- 1
1.12
Z/H* 0.
ETA- 0.50
(W.ti
(Uf L 1
(U»0|
(U ( 01
0.4034
0.2463
-0.2463
-o.ocno
0.4453
0.2337
-0.2337
-o.aono
0.0474
-0.2120
0.2120
0.0000
0.4222
0.2559
-0.2559
-0.0000
-0.4222
-0.2559
0.2559
0.0000
-0,0188
-0.0095
0.0095
-0.0000
0.0231
-0*0222
0.0222
0.0000
L-15^9
155
TABLE 24.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR 7 = 1.5, K = 4.00, AND rj = 0.50
(d) y/H = -0.75
8
Correction factors for correcting from a wind tunnel which is
—
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
, » T
CHI=-3.00
CAPH A* 1.5
ZE TA =
4. CO
X/H* 0. Y/H=-0. 75
Z/H* 0.
ETA* 0,50
( W,L I
( U , L )
(V,D)
tU,D)
-0.3130
-0.0900 _
- 1.0466
0.5894
-0.3073
-0.0900
-1.0127
0,7510
-2.5120
-0.9893
-C. 0900
1.5618
-0. 7101
-0.0900
-1.0477
0.6998
- 7. 1292
-1.0477
-0 .0900
1.5609
-0.0029
-O.OCOO
0.0C1 1
-0. 1 104
0.0029
0.0000
0.0350
0.0512
CHI* 3.00
GAP l *A* 1.5
ZETA*
4.00
X/H* 0. Y /H*-0 . 75
Z/H= 0.
ET A = 0.50
(W,L 1
l U , L )
I W, D )
m,0)
-0.3130
0.0900
-0.BP30
0.7016
-0.3073
0.0900
-0. 3491
0.8471
-2.4471
-0.8256
0.0900
1.5616
-0.3101
0.0900
-0.9041
0 . °0 1 0
-3.0573
-0.8.94 1
0.0900
1.5609
-0.0029
0.0000
0.0011
-0.0994
0.0029
-0.0000
0.0351
0.0461
CHI* 15.00
GAPP A* 1.5
7ETA*
4.00
X/H* 0. Y/H=-0.75
Z/H= 0.
E T A= 0.50
I W,L )
IU,L)
(H,DI
(U, D)
-0.2138
0.4312
-0.5668
0.7954
-0.2078
0.4312
-0.5327
0.9129
-2.2235
-0.5092
0.4311
1.4495
-0. 21C8
0.4712
-0.5679
O.R758
-2. 9232
-0.5679
0.4312
1.4485
-0.0030
0.0000
0.0010
-0.0803
0.0030
-0.0001
0.0352
0.0372
CHl=30.00
GAPP A= 1 . 5_
ZE TA =
4.00
X/H* 0. Y/H=-0.75
1/ H= 0.
El A~ 0.50
(W,L )
_ lil.kL
tu,o>
cu f oj_
0.0629
0.7513
-0.2681
0.7090
0.0696
0.7511
-0.2339
0.7979
-1.7969
-0.2103
0.751 1
1.1283
0.0663
0.7513
-0.269 1
0 . 7 7 0 1
-2.3777
-0.2691
0. 7513
1. 1272
-0.0033
0.000 1
0.0010
-0. C603
0.0033
-0.0001
0.0352
0.0278
CHI *45. 00
GAHHf* 1.5
ZF T A =
4.00
X/H* 0. Y/H=-C.75
Z/H= 0.
E T A = P.5C
IH*L)
IU.U
(W,0)
HJ,0)
0.4173
0.8822
-0. 1526
0.4922
0.4254
o.eeie
-0. 1184
0.5547
-1.2520
-0.0948
o.e*’ 16
0. 6653
0.4214
0.8821
-0. 1536
0.5351
-1.8312
-0.1536
C .8821
0.6840
-0.004 1
0.0001
0.0010
-0.0429
0.0040
-0.0003
0.0353
0.0196
CH I *60. 00
GAPPA* 1.5
/ETA*
4.00
X/H* 0. Y/H*-0 . 75
Z/H= 0.
E r A= 0.50
(U,L1
( U, L )
1W.01
(U t 01
0.7039
0.8099
-0.2413
0.2656
0.7152
0.8090
-0.2070
0. 3048
-0.7143
-0. l p 34
0.8086
0.2384
0.7096
0.8096
-0.2423
0.2927
-1.2P46
-0.2423
0.8096
0.2365
-0.0057
0.0003
0.0010
-0.0272
0.0056
-0.0006
0.0353
0.0120
CHI*T5.00
GAMP A = 1.5
ZF TA =
4.00
X/H* 0. Y/H=-0. 75
Z/H* 0.
ETA* 0.50
(M.L )
HI , L )
tW.Dl
(U,01
0.7357
0.6362
-0.4646
0.1239
ZE TA*
0.7566
0.6328
-0.4307
0. 1404
4.00
-0.2635
-0.4070
0.6313
-0.0518
X/H* C. Y/H=-0.75
0.7462
0.6353
-0.4658
0. 1358
Z/H= 0.
-0.8250
-0.4658
0.6353
-0.0549
ETA* 0.50
-0.0105
0.0010
0.0012
-0.0120
0. 01Q4
-0.0024
0.0351
0,0045
CHI-9Q.00
GAPPA* 1.5
|H#U
tu.u
(M, D)
HI, D I
0.4212
0.6479
-0.64 79
-o.ocoo
0.4864
0.6198
-G. 6198
-O.OCOC
0.0942
-0.5952
0.5952
0.0000
0.4520
0.6519
-0.6519
-0.0000
-0.4520
-0.6519
0.65 19
0.0000
-0.0308
-0.0040
0.0040
- 0.0000
0.0344
-0.032 2
0.0322
0.0000
156
TABLE 24.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 4.00, AND tj = 0.50
(e) y/H = -0.375
Correction factors for correcting from a wind tunnel which Is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI 3 - 3. 00
GA M P A = 1.5
ZET A-
= 4.00
X/H* 0. Y/H— 0.37
It H* 0.
ETA* 0.50
1W,L J
IU,L)
IW.DI
(U,0 )
-3.25C9
-0.3436
-5.4750
0.9265
-3.2390
-0. 3435
-5.3908
1 . 1460
-4.8065
-5.3681
-0.3435
4.6726
-3.2448
-0.7435
-5.4537
1.0662
-5.5778
-5.4537
-0.3435
4.6706
-0.0061
-0.0000
-C.C213
-0.1396
0.0059
0.0000
0.0629
0.0798
CHI * 3,00
GAPYA® 1.5
ZET4 =
4.00
X/H* 0. Y/H— 0.37
Z/H* 0.
ETA® 0.50
IW*L 1
IU.L )
tw, 01
IU,D)
-3.2509
0.34 36
- 4 . 9f 55
1.4764
-3.2390
0.3435
-4.9010
1.6040
-4.7729
-4.8784
0. 3435
4.6726
-3.2448
0.3435
-4.964 1
1.6121
-5.5356
-4.9641
0.3435
4.6706
-0.0061
0.0000
-0.0214
-0.1257
0.0059
-0. 0000
0. 0631
0.0718
CH 1= 1 5. 00
GA0PA* l.s
ZETA =
4.00
X/H* 0. Y/H®— 0. 37
If H= 0.
ETA* 0.50
I W* L 1
CU.L1
(W f OI
( U t D )
-2.9036
1.6409
-3.9367
2. 1493
-2.8912
1.6407
-3.8518
2.3005
-4.3782
-3.8291
1.6406
4.2275
-2.8973
1.6408
-3.9151
2.2506
-5.0858
-3.9151
1.640e
4.2255
-0.0063
0.0001
-0.0216
-0.1014
0.0061
-0.0001
0.0633
0.0578
CHI® 30. OO
GAMP A® 1.5
ZETA*
4.00
X/H® 0. Y/H=-0 .37
Z/H* 0.
ETA® 0.50
I U t L >
1U,L 1
IW,D)
(U»D I
- 1.9595
2.8296
-2.8100
7.2238
-1.9457
2.8290
-2.7247
2.3427
-3.2066
-2. 7020
2.B289
2.9757
-1.9525
2.0293
-2.7083
2.2996
-3.9383
-2.7883
2.8293
2.9734
-0.0070
0.0002
-0.0218
-0.0758
0.0068
-0.0003
0.0635
0.0430
CHI-45,00
GAMP A - 1.5
ZETA*
4.00
X/H= 0. Y/H— 0. 37
Z/H= a.
ETA* 0.50
IW.Ll
IU.L)
IW,D)
(U»D )
-0.C329
3.2568
1673
1.7500
-0.8161
3.2555
-2.0818
l.e417
-1.7269
-2.059 1
3.2554
1 .3450
-0.0244
3.2562
-2.1455
1.0116
-2.4448
-2.1455
3.2562
1.3422
-0.0006
O.OOOS
-0.0216
-0.0536
0.0082
-0.0007
0.0636
0.0301
CHI=60.00
GAMPA® 1.5
ZETA*
4.00
X/H® C. Y/H — 0.37
Z/H= 0.
ETA® 0.50
IW.Ll
IU.L)
IW.O)
(U,0I
-0.0PC9
2.9109
-2.01?3
1. 1226
-0.0575
2.9080
—4.9319
1.1739
-0.3199
-1.909 1
2.9C76
-0.0192
-0.0690
2.9097
-1.9955
1.1559
-1.0248
-1.9955
2.9097
. 02 30
-0.0119
0.0012
-0.0218
-0.0333
0.0115
-0.0017
0.0636
0.0180
CHI-75.00
GAMMA* 1.5
Zf T A®
4.00
X/H* 0. Y/H— 0.37
Z/H® 0.
ETA® 0.50
IW.Ll
<u,u
IW.CJ
IU.0I
-0.1398
2.2612
-2.0625
0.5349
-0.0975
2.2506
-1.9731
0.5539
0.7042
-1.9553
2.2490
-0.4260
-0.1103
2.2568
-2.0412
0.5482
0.0133
-2.0412
2.2568
-0.4319
-0.0216
0.0044
-0.0213
-0.0133
0.0208
-0.0062
0.0631
0.0057
CHI-90.00
GAMPA* 1.5
ZE TA =
4.00 X/H* 0. Y/H— 0.37
Z/H* 0.
ETA® 0.50
IW.Ll
IU.L)
IW.D)
1U. 0 I
-C. 74 25
1.9710
-1.9710
-o.oroo
-0.6248
1.P9G6
-1.89^6
0.0000
1.3495
-1.6747
1.8747
o.oooc
-0.6P45
1.9557
-1.9557
-0.
0.6845
-1.9557
1.9557
0.
-0.0580
0.0153
-0.0153
-0.0000
0.0597
-0.0571
0.0571
0.0000
6^ T-1
L-15^9
TABLE 24.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, < = <-00, AND I) = 0.50
(I) y/H = 0
157
Correction factors for
correcting from
a wind tunnel
which Is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00
GAM
—
M A* 1 • 5_
r ■—
ZETA* 4.00 X/H*
. Y/H* C.
—
Z/H* 0.
ETA* C.50
tH.L)
(Uf L )
(W,D>
(U * D )
-26.6287
-1.6926
-31.2097
0.0204
-26.5971
-1.6926
-30.9998
0.3750
31.074 1
-30.9818
-1.6924
13.2942
-26 .6127
-1.6926
-31. 1287
0 • 2286
30.0157
-31. 1 2 C7
- 1.6926
1 3.288 3
-0.C160
n.oooo
-0.0910
-0.2083
0.0156
0-0000
0.1289
0.1464
CHI* 3.00
GAMMA* 1.5
ZETA
4.00 X/H*
). Y/H* 0.
Z/H* 0.
F T A* C.50
IH,U
tU.L )
tW,0)
(U,D)
-26.6287
1.6926
-29.6173
3.2308
—
-26.5971
1.6926
-29.6064
3.5502
24.6715
-29.5883
1.6924
13.2942
-26.6127
1.6926
-29.7359
3.4184
23.62 74
-29.7359
1.6926
1 3.28P3
-0.0160
-0.0000
-0.0815
-0. 1076
0.0156
-0.0000
0.1294
0. 1318
CH 1= 1 5.00
GAMMA* 1.5
ZETA
4.00 X/H- 0. Y/H* 0.
Z/H* 0.
ETA* 0.50
( W» L )
(U»L )
IW,D>
(U,0)
-23.7870
7.7589
-24.6885
7.6738
-23.7543
7.7581
-24.4760
7.9286
14.4132
-24.4579
7.7580
10.9519
-23.7704
7.7585
-24.6062
7.8234
1 3 . 394 1
-24.6062
7.7585
10.9463
-0.0166
0.0004
-0. 0822
-0.1496
0.0161
-0.0004
0. 1 302
0. 10S2
CHI=30. 00
GAMMA* 1.5
ZETA
4.00 X/H*
3. Y/H= 0.
Z/H* 0.
ETA* 0.50
( H • L 1
IU.L1
( W , D }
1U,D1
-16.7297
1 1 . 7753
-16.8191
8.8235
-16.6934
11.7734
-16.6055
9. 0125
7.1995
-16.5074
11.7733
5-3955
-16.7113
11.7744
-16.7364
8.9347
6 .2070
-16.7364
11.7744
5.3892
-0.0184
0.0009
-0.0828
-0.1112
0.0179
-0.0010
0.1308
0.0778
:hi=45.oo
GAMMA* 1.5
ZETA
* 4.00 X/H*
3. Y/H= 0.
Z/H* 0.
ETA* 0.50
< W v L 1
IU.LI
<W,0]
(U,0 1
-9.57 17
1 1.1334
-10.5591
6.5789
-9.5276
11.1294
-10. 3450
6. 7079
4.8448
-10.3268
1 1 . 1292
0.3352
-9.5493
11.1315
-10.4761
6.6564
3.8759
-1C .4761
11.1315
C . 3277
-0.0224
0.00 19
-0.0830
-0.0775
0.0217
-0.002 I
0. 1311
0.0535
C H 1*60. 00
GAMMA* 1.5
ZETA
= 4.00 X/H*
3. Y/H* 0.
Z/H= 0.
ETA* 0.50
(H»L )
IU.LI
( W f D )
lU t D>
-5. 2831
7.9987
-6.9348
3.5459
-5.2220
7.9893
-6.7212
3.6225
4.63 l 3
-6.7030
7.9890
-1.7407
-5.2521
7.9943
-6.8520
3.5920
’.6851
-6.8520
7.9943
-1.7507
-0.0310
0.0044
-0.0828
-0.0461
0.0301
-0.0050
0.1309
0.0305
CH 1 *75. 00
GAMMA* 1.5
ZETA
* 4.00 X/H*
0. Y/H* 0.
Z/H* 0.
ETA* 0.50
(W,L >
1U,L)
(H,D>
(U,D)
-3.9769
5.2398
-5.0676
1.3155
-3.8699
5.2073
-4.6579
1.3 371
4.7246
-4.8396
5.2060
-1.1799
-3.9226
5.2246
-4.986B
1.3302
7..B044
-4.9868
5.2246
-1.1943
-0.0543
0.0151
-0.0808
-0.0147
0.0526
-0.0173
0.1290
0.0069
CH 1=90. 00
GAMMA* 1.5
ZETA
* 4.00 X/H* i
0. Y/H* 0.
Z/H* 0.
ETA* 0.50
tW.L)
(UjtU
IW,0)
(U,0)
-
-3.9462
3.8850
-3.8850
-0.0000
-3.6944
3.7061
-3. 7061
0.0000
4.6893
-3.6870
3.6870
-0.0000
'-3.3 197
3. '*197
-3.8197
0.0000
3.8197
-3.8197
3.0197
-0.0000
-0.1265
0.0653
-0.0653
-0.0000
0.1253
-0.11J6
0.1136
0.0000
158
TABLE 24.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 4.00, AND i}- 0.50
(g) y/H = 0.375
Correction foctors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
' only
(ground effect)
only
only
to free air
to ground effect
CHI— 3,00„.
CAM* A- 1.5
7CTA = 4.00
X/H= 0. Y/H= 0.37
Z/H* 0.
ET A = 0.50
1W.L1
-3.3021
-3. 1884
-3.9052
-3.2448
-5.5778
IU«L )
-0.3430
-0.3433
-5.1365
-0. 3435
-5.4537
iw.o)
-5.7067
-5.1467
-0.3432
-5.4537
-0. 3435
IU.D1
0.6783
1.3914
4.6916
1-0662
4.6706
CHI- 3.00
GAMMA- 1.5
ZETA* 4.00
X/H = 0. Y/H= 0.37
Z/H= 0.
E T A = C . 50
l*.W
-3.3021
-3. 1884
-3.8916
-3.2446
-5.5356
tu.n
0.3433
-4.6447
0. 3435
-4.9641
- 1M*P)
-5.2192
-4.6549
0.343?
-4.964 1
0.3435
IVjtPt
1.2634
1.9045
4.6916
1.612]
4,6706
GAMMA « 1.5
ZETA- 4.00
X/H= 0. Y/H* 0.37
l /H = 0.
ETA- 0.50
-2.9564
-2.8390
-3.4925
-2.8973
-5.0858
- tU»l)
1.6423
1.6393
-3.5925
1.6408
-3.9151
<W»01
-4.1733
-3.6028
1.6393
-3.9151
1.6408
(U| 0 1
1.9711
2.4046
4.2471
2.2506
4.2255
—
CHI-30.00
GAMMA* 1.5
ZETA* 4.00 X/H =
0. Y/H~
0.37 Z/M= 0.
E T A = 0.50
(W,L)
-2.0181
- 1 .8078
-2.3994
-1.9525
-3.9303
1U»L )
2. 8328
2.8257
-2.4634
2.0273
-2.7833
(W,D>
-3.0436
-2.4737
2.8257
-2.7FE 3
2.8273
tu,o>
2.0945
2.4704
2.9972
2.2996
2.9734
CHI-45. 00
GAMMA* 1.5
ZE T A =
4.00
X/H* 0. Y/H* 0.37
Z/H= 0.
ETA= 0.50
IM,L)
-0.9037
-0.7461
-0.9548
-0 . ° 244
-2.4449
tUtU
3.2635
3.2487
-1. F200
3.2562
-2. 1455
IU t D)
-2.4064
-1.8302
3.2486
-2. 1455
3.2562
lUibi
1.6730
1.9254
1.3702
1.0116
1 .3422
„CHI*60._00
GAMMA- 1.5
ZETA =
4.00
X/H* 0. Y/H= 0.37
If H= 0.
ET A= 0.50
(H.U
-0. 1773
0.0377
0.4166
-0.0690
-1.0248
i».t>
2.9264
2.8923
-1.6719
2.9097
-1.9955
1W,D)
-2.2545
-1.6822
2.8921
-1.7955
2.9077
(U.D)
1.0808
1.2149
0.0125
1 . 1559
-0.0230
-0.0573
-0.0003
-0.2530
-0.3879
-0.0573
0.0003
-0.2551
-0.3488
-0.0591
0.0015
-0.2562
-C.2796
-0.0656
0.0035
-0.2604
-0.2051
-0.0794
0.0073
-0.2609
-0.1386
-0.1063
0.0167
-0.2590
-0.0751
0.0564
0.0003
0.3070
0.3252
0.0564
-0.0003
0.3092
0.2923
0.0583
-0.0015
0.3123
0.2339
0.0647
-0.0036
0.3146
0.1708
0.0702
-0.0075
0.3152
0.1138
0. 1067
-0.0174
0.3133
0.0590
CHI-75.00
-GAMMA* 1,5
ZETA* 4.00
X/H= 0. Y/H=
C. 37 Z/H* 0.
E T A= 0.50
<w,i>
-0.2974
0.0579
1.3959
-C. 1183
0.0133
IUiU
f 2.3097
2.2012
-1.7291
2.2568
-2.0412
IWtP)
-2.2897
-1.7384
2.2005
-2.0412
2.2568
. 11UB1
4 0.5354
0.552C
-0.3087
0.5482
-0.4319
CK1»90.00
1 1 , .
ZETA* 4.00
X/H- 0. Y/H=
0.37 Z/H* 0.
ETA* 0.50
tW.L)
1,0254 _
-0.3485
1.9553
-0.6845
0.6845
— __ UULi —
2^152-6
1.7039
-1.6931
1.9557
-1.9557
CW.DI
-2.1526
-1.7039
1.693 1
-1.9557
1.9557
(U»D)
-0^0000
0. 0000
0.0000
-0.
0.
- 0.1791 0. 17 62
0.0529 -P,Q556
-0. 2484 0. 30 28
-0.0127
-0.3409 _ 0. 3360
0.1969 -0 .2518
-0.1969 0.2518
- 0.0000 __ 0 .0000
L-15^9
159
TABLE 25
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR v = 1.5, K = 0.70, AND tj = 0.25
(a) y/H = -2.25
8
Correction factors for correcting from a mind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
— .
to ground effect
'CHI— 3*00
GAMMA* 1*5 it! A-
y/H=-
■4J6?
£JA- 0*2.3
(W»U
“0*1H2
-0.U271
-G.UQ99
0,1097
-Q, .027.0-
-0.0093
0.1735
-0,0870
-0.009*
“0.1717
-0.1510
-0.0242
0*001X1
0.0599
IHftDl
10.01
-0.1151
“0*5360
-0 .0606
0.1576
-0.1310
0.0324
-0.0096
0.1341
0.0359
-0.5684
0.0903
0.1255
CHI = 3*00
GAMMA= 1.5 2ET A =
_ Oj_/i A/h= Jl*_
Y/M=^2«_4v
. Oa__ .
£1 A- u .23
uYu
IU.LI
“0.1112
0.0086
-0,0271
0,0099
0,1046
-0.0088
-0.0870
-0*1696
... -0*1369
-0.0242
-0*0010-
0.0599
0*0002
(W*0J
tu.oi
-0.0968
-0,4664
-0,0446
0,1606
'0,0093
Q, 1735
-0.1369
0.0474
0.0096
0.1341
0.0381
-0.3138
0,0923
0.1134
CHI-15.Q0
GAMMA* 1.5 2ETA*
0.70 A/H- 0.
Y/H-
“2*25.
4/H«_ Oj
__£.;A*__0*21
jw»u
-Q.1018
-Q, 0157
0.1066
-Q .0772
-0.1552
-0.0246
0*0615
0*QQ12
IU.L1
0.04Q7
0.0473
_ 0*026 7.
0*0461
-0,1072
-0*0054 —
(MfPl
. .. (u.pi .
-0.Q654
-0,3499
-Q,Q123
0.1553
0.0442
0.1616
-0,1072
0,0648
0*0461
0, 1216
0.0418
-0.4146
0*0947
0,0906
CHI -30*00
GAMMA* 1.5 2ET A*
0. 70 a/H= 0.
Y/H =
“2*26.
A/ Hr 0,.
EJA= 0 Ai>.
< W • L )
IU*L )
-0,07*3 7
0.0673
0,0161
0,0822
0,1277
0.0616
-0,0508
0,0797
-0,1209
-0.0757
-0.0255
“0*0124
0*06*9
. Q.JJQZ5
0.0952
0*0640
<W*D)
10*01
-0,0299
-0.2392
0,0195
0,1295
0*0752
0*1261
-0,0757
0,0654
0.0797
0*0865
0*0458
-0*3047
CHI -4b *00
GAMMA- 1.5 2ETA*
0,^0 X/H = 0,
Y/H =
4/H = 0*
ETA* 0*2 3
' i i
2j=J2
“0.0*51 _
0,0*90
-0.0081
-0.1542
0*0561
0,0961
0,0339
0,0904
0,1604
0,0760
0.0334
0.0834
-0*019U
0,0921
-0*0584
0,0512
-0.076b
-0.0584
0,0921
0,0403
-0*0263
-0*0231
0*0502
-0.2054
0,0772
0*0041
0.0923
0.0392
CHl-60.00
GAMMA- 1.5 2ETA-
0,7 0 X/H = 0,
Y/H*
-2.25
2/H* Qt
ETA* 0.2b
19*L)
(0*L )
-0.0208
0.0413
0,0966
0,0875
0.1916
0.0735
0 * 0023
-0.0348
-0.0554
-0.0231
0*0945
0*0042
(W«D|
( 0*0 )
0,0009
-6,0817
" 0,0282
0,0494
0,0657
0.0416
-0.0554
0,032*
0.0828
0.0608
0.0663
-0.134* -
0.0837
0.0167
CH1»75.00 GAMMA » 1.5 ZET A g Y/H»“2*25 1 / 0* E T A * 0 *25
o*u««
0*0642
0*0009
CHI *90.00 GAMMA ■ 1*5 2ETA* 0*70 ^/H«0* Y/H«-2.23 U H= 0* E TA- Q*25
_.Ya*3Li~
(U.L)
0*9396
-0.0045
0*1225
0.0252
__._P.2085
Q.Q182
-0.0169
Q.Q567
0*0169
—0.0567
0.0566
. -0.0613
0*1395
1M»DL
IU.DI
0,0045
-0.0000
-0.0252
0*0000
-0.0182 .
.... 0.0000
-0.0567
-0.0000
0.0567
0.0000
0.0613
-0.0000
0.0315
0.0000
(U*LJ
-0.9001
0*1200
0.2Q9S
Q. 0004
-0.003*
-0.0010
-o ,0045
Q.C619
0.0517
0.0647
-Q.o^a;
( W * D T
0,0057
0*0061
0*0287
-0*0582
0.0647
0.0*39
“0,0.229
0*0165
0.0130
Q.0156
-0*0121
-0.0385
l 6 o
TABLE 25. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.70, AND T) = 0.25
(b) y/H = -1.875
Correction factors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
[—3*00
GAMMA- 1*5
ZETA = 0./0 X/H-
_0* . Y/H--1.8/ UH~ 0*
LI A- 0*25
<w»L>
-0*1787
-0aQ56L
0.1914
-0*1394
-0*1579
-0*0394
(U»L)
-0.0116
-0.0139
-0.0604
rQ«_0132
-0*2166
0*001 /
~IW*P)
-0.1680
-0.1238
-0.0125
-Q *2 168
-0.0132
0*066V
IV*D1
-Q*6626
0*1955
0*2259
0*0329
0*1687
-0*5955
0*0*2 /
-0*0007
0*0930
0*1626
C HI- 3* 00 G AMMA- 1*5 ZETA- 0-70 X/H- Q* Y/H=-l .67 i/M» 0. ETA- 0.Z5
IWtL)
-Q*178.2
-0*056.7 _.
0*1793
-0*1394
-0*1601
IU.L)
0*0116
0*0139
-Q*Q2t>4
0*0132
-0*1992
* w * 01
-0a1366_ .....
-0*1047
0*0125
-0*1992
0*0132
IU»D1
0*2024
0*22o’>
0*054/
0*1687
-0*0394 0*0627
-0*00X2 0*0007
0*0626 0*0943
-0*5394 0*1477 -
tW.L)
_ -a* 1656 -
-0*0410
-0*1/16
1 U *L )
0*0544
0.0664
0*0121
Q * Cd jQ
. - JWtD)
-Q.Q9Q9 _
-0*0639
0*0591
-0.1597
.. .... WtDI
-0*3559
. 0*2005 .
0*2123
0*0813
— 0 .1502 — 0 » 0399 0*0347
-Qtl 53LI -Q.QC66 0*0035
0*0630 0*0666 0*0956
0*1315 -0*4624 0*1196
CHI-30.00 GAMMA- 1,5 It TA- 0*23 X/H* Q« Y/H— 1*87 i/H=_ J5 a. LlA_= 0*25.
MrftU -0il3Q2 0»QQ 26 0*1886 -Q*G889 -0.1150 -0*0413 0*0915
tU»U 0*0883 0*1154 Q.Q622 0*10 78 -Q.1155 __ - Q*0L94 0*0076..
»W*D| -0.0400 -PaP2Q8 Qa 0?89. -Q*ll55 0*1078 0*0755 0*094/
tUtpl -0*2380 0*17 16 0*1.661 0*0855 0*1034 -0.3235 0*0861
CHI *45.00
GAMMA- 1.5
2ETA-
0*70
;;/H- 0. Y/H--1.87
2/H- 0.
ETA* 0.25
(W*L)
-0*0876
0*0589
0*2211
-0.0452
-0*0662
-0*0424
0*1041
fU*L)
0*0865
. 0.1>53
0.i08>6
. 0 *1223
-0*0879
-0*0556
_ 0*0131
l#»D|
-0.0054
0*0015
0.1055
-0*06 / V
0*1223
0*0628
0*0694
1 U . DJ
-P*_1526
0,1235
0.1065
0*0683
0*0424
-0*220 V
0*036X
CHI-60. 00
GAMMA= 1.5
...Z.EIA=
0* / 0.
X/H* Qj. _ Y/H— L».87
i/h= o*
ETA- 0*23 _
' '
"
(W*U
-0*0537
0*1079
0*2516
-0*0160
-Q*0i.Ql
-0*0327-
0*4236
[ U *L 1
0 *04^4
0* 1 451
a*fta2d
0.1Q7Q
_ _ -0*0X76
-Q «0fr2fr
0*0191
(W*0l
0*0139
-0*0008
0*0/5 8
-0*0/76
0.10/0
0*0915
0*0743
«u*01.
rQ.0835
0*0/06
0.053 /
0*0435
-0*0053
“0*42-69
©*0272
CH I *75 . 00
GAMMA* 1.5
ZFTA= 0.70
X/Ht
5*. Y/Ha-1 .87
IWtLl
( U »L 1
-0*0243
-0.019?
0*1330
0.0979
0.2650- —
0.073^
... <W»DI
0*0276
-0*0235
0*0221
IU*D)
-0*0270
0*0262
0*0186
CHI -90,00
GAMMA 3 1*3
LET A 3 Q. 70
X/H=
0* Y/H 3 -1*B7
• 0745
*0200
0*0613
-0*0163
0*1021
- 0*0469
IWtLl
0*0309
0*1294
0*2535
-0*0325
0*0325
0.0635
Q.1420
{U.L1
—0*0316
0*0571
0.0390
0.0684
•n 4 0644
-p.LOOl
-e*oi 12
IWiD ]
0*0318
-0.0571
-0.0390
-0*0684
0*0664
0*1001
0*0442
{ U t D )
-0*0000
0*0000 ..
0*0000
-0.0000
0*0000 -
-0*0000
n*oooo^
6 ^T -1
L-15^9
LIS
161
TABLE 25.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, f = 0.70, AND tj = 0.25
(c) y/H = -1.50
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI “-3*00
GAHM A = 1.5
ZETA = O./C
-Z/H* 0.
. ._.r/H=-i,50.
. . Z/h- 0,
ETA= 0 .23
IW*L)
IU*L 1
-0,3202
-0,0156
-0,0879
-0,02 01
0*3265
-Q.1137
-0,2249
-0*0186
-0,0952
-0 i 3 176
-0.0953
0*0030
0.1370
„ -0*0015 _ .... .
IW»D|
IU»D|
-0,2437
-0,6379
-0*2039
0*2566
-0.0174
0.31Z2
-0*3176
0*0317
-0.0166
0.2137
0.0739
-0.6695
0.1137
0*2250
CHI “ 3.00
GAMMA * 1.5
ZET A= 0* 70
X/H* £*
... . . r/h*-liiO.
<L/m= 0*
_ EIA= 0*25
I W »L I
( U *L ]
-0.3202
U.0156
-0*0879
0*0201
0.3033
-0.0810
-Q*2249
0*0166
-0.1069
. -.0*2932
-0,0953
-0*0030
0*1370
0*0015
( W *D 1
|U*D|
-0,2160
-0,5449
-0* 1 79b
0*269^
0*0174
0.3122
-0*2952
0*0636
0,0186
0.2137
0.0792
-0*6086
0*1155
0*2055
CHI-15.00
GAMMA = 1.5
ZET A = Q. 70
X/H= 0.
.. . Y/Ha -1.50
E_TA = 13 .2 5
IMlU
(U.L)
-0.3014
0.0725
—0 * 0 6 4 4
0.0961
0.2 771
-0*11119 .. .. .
-0,2046
Q*jQ8fil
-0.1154
-Q.2412
-0.0968
“0*0156
0*1401
0*0080
U*D)
IU,D)
-0.1526
-0.3916
-0.1245
0.2 726
0.0620
0.2864
-0.2412
0*1046
0.0861
0.1691
0.0866
-Q.4965
0*1166
0,1676
CHI “30.00
&/.H- tU
Y/tL=-1.50
Z/H= 0*
ETA- 0*25
1 W t L 1
( U • L 1
-0.2511
. 0*1134
0*0007
0*165 7
0.2834
0.0636
—0 • 1 4 9b
0*1463
-0.0894
-0,1757
-0.1013
. -Q*0349 .
0,1505
0*0174
IW»D)
(UtD 1
-U.U736
-0.2564
-0 * Y 6 2 4
0*2379
0.1342
0.2230
-0*1757
0*1147
0. 1483
0. 1220
0*1001
-0.3710
0,1133
0*1232
CHI >4b,Uu
GAMMA = i.5 _
ZET A- 0. f 0
Z/H= 0.
Y/H--1.50
A/n = 0,
ETA = 0.25
IW*LI
iu*m
-0,1928
U.1UU4
0 • 0b32
0,1930
0.3148
0.11U9
-0,0639
0,1b 32
-0.0424
-0. 1297
-0*1069
-0*0628
0*1690
0*0297
<M*D)
( U *0 J
-6.0156
-0,1652
-0.O2 74
0.1739
0.136/
0.1419
—0 ,12 9 7
U ,0923
0.1632
0.0415
0.1141
-0.2575
0*1024
0*0616
CHI >60.00
GAMMA “ 1,5
. ZET A=. .0. 70
A/H- 0,
Y/H — 1,50
Z/M- 0*
t T A= 0.23
< W«L )
1 U »L )
-0.1466
0.0317
0*1531
0,1814
0,346b
0*1246
-0,0431
0,1373
0.0035
-0. 1061
-0.1036
-0.1056
0*1962
0*0441
(W*DI
IU*0>
0.0279
-0,0963
-0,026b
0.101 i
0*06 79
0*0 7 3 9
-0,1061
0.03 73
0. 1373
-0.0144
0.1340
-0.1536
0*0792
0,0442
CHI “75.00
GAMMA = 1.5
ZET A- 0,70
_xy.H= _Q±
Y/H=-i*30
Z/H* 0.
ETA* 0.25
(W*U)
<U*L)
-0,1087
-0.0604
0,1677
_0il490
0*3562
0*1104
-0,0376
0,1006
0.0344
-0.0937
-0.0709
-0.1610
0*2255
0,0464
( W t D )
(U.P)
0,0658
-0,0381
-0,056/
0,0396
0*0093
0*0267
-0,0937
0*0250
0.1006
-0.0212
0.1595
-0.0632
0*0370
0*0148
CHi=vo.oo_
_ GAMMA- 1.5
ZET A= 0 #_/ 0
X/H-. Oi
Y/H=-i*50
Z/h= 0*
ETA* 0*25
IW»U
(U,L)
-0,0300
-0.0906
0,1809
0*1033
0*3375
.0*0 756
-0*0521
0,0612
0.0521
-0.0812
Q.Q22Q
._. -0*1718
0*2330
Q*0221
IW#U)
1 U «D >
0.U9U6
-Q.QQOO
-0,1033
U*00UU
-0,0756
0,0000
-0.0812
-G.0000
0.0812
0.0000
0.1718
-0.0000
“0*0221
0.0000
162
TABLE 25.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0-™, AND 1}= 0.25
(d) y/H = -1.125
s
Correction factors for correcting from a wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 1 1 ■ ,_J
to ground effect
CHI— 3*00 a AHMA« Ltl AfciA; */h- U* T/ He~l*-*2 .4/H?..U*
. i**U _
-0*5812
-0*1153_
0*3627
>0*3362
0*0627
>0*2230
0*2449
U>*L )
>0*0207
—0.0294
-G ■ i ^66
-0*0264
-Q t UkhR
JMfOi
-0.3940
>0*3056
-0*0230
>0*4466
-0*0244
0*0726
0*1411
. tytfti
-0*7794
0*3554
0*4360
0*0275
0*2695
>0*8070
0*3242-
frAM M A" 1*5 iEIA" fl ilfl ii/H- fl *
JttlkJL - -0*5812
10»L) 0*0207
(tf ,01 -Q*JS9S—
tU*OJ ->0 ,46 77
-0*1151-- 0*5123
Q-.0218 -Q.15P7
-0*2731 0-0260
0*3744 O *4380-
-0*3542
U.Q264
-0*4345
0.0750
0*0222
—Q. 43Bb
-0*2220
-0*0058
0*0791
" 0* 7377 -
0*2449
0*1454 -
0
CHI *13.00
GAMMA- 1*5
2ETA» 0*70 X/H*
0. Y /H*-l • 12
1/H* i*
ETA« 0*25
ftilL >
. -0*5329
-0*0753
fi*44#5
-0*3258-
>0*0270
-0*2270
0*2504
tU*L 1
0*0945
0*1415
-0.0487
0*1244
-0*3425
-0*0296
0*0171
IHfPl
iMlOl
-0*2707
-0,4700
>0*1936
043872
Qt.1169
11*4029
-0*3625
0*1378
0*1244
0*2340
0*0916'
-0*6078
0*1487
0*2493
_
CHI*30* 00
OlUMi* l.ft 2ETA*
0-70
X/H-
0*
Y/H — 1-12
2/H= 0*
F T A- 0*25
(M*L t
' ’-0*4746"
0*0281
0*4 32 5
->Q*2402
-0*0337
>0-23.94
0*2483 .
(UtU
* 0*1383
0.*24Qt
0*0700
0*2040
. -0*2618
-0*0657.
0*0369
(U*Di
-0*1304
—0*0947
n f i && 1
•q * a 14
Ot 2040
£1*111*
. l±2 1
itttftl
-0*3044
0*3411
0.3066
0*1554
0*1403
-0*4600
0*1848
... | ■ -
CHI *45.00
tkmA* 1*5 2ETA=
0*70
X/H-
0*
Y/H— 1.12
1/H 1 0*
ETA- 0.25
(W*L)
lUtL)
__ -0 x 4ft®8.
0*1003
0*1571
0*2769
—
4*4624
0.1502
-0*1428 .
0.2154
-0*0023
-Ot 1847
-0*2418
-0*1191
0*2999
(w*6)
-0*0445
>0,0444
0*1799
-0*1847
0*2154
0*1401
0*1401
(VfPI
0,2502
0*1975
0*1240
0*0360
-0*3246-
0*1243
CHI *60*00
GAMMA- 1*5 ifcTA-
0*70
X/H-
Q*
Y/H--1.12
Z/H- 0-
ETA- 0-25
IMfU
(U*L1
-0*0127
0*2439
0-2414
—
0-5030
0-1619
-0*0785 .
0-1724
. . 0-0354
-0*1194
-0*2701
0*3444
P-QflQQ
<u*oi
0*0452
-0*0442
0-1022
-0*13 94
0*1724
0*1846-
0*0954
(Ufpi
>0*1284
0-1472
6*1011.
0*0743
. -0*0242
-0*2029
0*0729
CHI *75*00
GAMMA- 1-3 2CTA-
6-70
X/H*
Q-
Y /H — l - 12
Z/H= Q*
ETA- 0*25
iw * Li Z
(U*L )
—0*1021 0*3244
-0.1448 0*2240
—
. 9*5234
8-1743
-Q..Q644
0*1214
0*0609
-0*1143
>0*2379
0*3888
O* 1 Q7A
_ .LMj&L .
IU#0)
Oj 131.8 ...
-0,0414
-0*Q844_
-0*0142
-0*1143
0*1214
0*2642
0*0197
Qi5Mi
0*0459
0*0305
-0*0265
-0*J)918_
0*0294
-f-
i
CHl»90*oi
GAMMA* 1*5 ZETA*
0*70
X/H-
0.
Y/H—1.12
2/M* 0*
ETA- Q*25
" \::t ~
IMiki
(U* L )
-0.1974
0*1242
0.5014
-0*0761
0*0741 -
-0*1233
0*963
-0-2045
0*1754
0-1411
0-0942
-Q.Q942
-0*2988
0*6-11-
(M«D )
0*2045
-0*1754
-Q-14L1
-0*0942
0-0942
0*2988
-0*08 U
iu,ai
-Q.QQOQ
Q-QOOO
Q-QOOO
-0*0000
0-0000
-a*oooa
0*080 v
6+fCC-l
L-15^9
163
TABLE 25.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 0.70, AND t? = 0.25
(e) y/H - -0.75
8
Correction factors for
correcting from
a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CHI— 3.00
GAMMA- 1*3
_2I
-XAi.
' 0.7Q
J ut
-Q*. y/h=-
0*75
2/H= 0.
ETA* 0*25
LWlL)
-1*0096
-0.1111
0.9081
-0.5414
0* 3564
-0*4660
0*4303
tUtU
-Q.Q233
-Q.Q441
J-H. 3 03 8
-0.0366
-0 • 6646
0.0113
-0.0073
-0*6239.
_
-0.4162
-0.036 /
-0.6646
-0*0368
0.0409
0*2486
IV»D)
-1.0246
0*5265
0.6333
0 . 02 02
0.3313
-1*0448
0*5053
chi ■ 3.00
GAMMA- 1.5
^2£TA*
0* 70
_X/H»
O. Y/H=-
3*75
Z/H* 0,
ETA* 0.25
(W*U
-1.0Q94
-0*1111
0. b 16 1
-0,5414
0* 2666
-0*4680
0*4303
(U.L)
0.0233
0 * 044 1
-Q.2374
0.0366
-0. 6301
-0.0115
0.0073
(W*0)
-0.5M6
-0*3689
0,0367
-0,6301
0. 0366
0(0443
0 • 2612
IU.D)
-0*8747
0*5569
0*6333
0.0660
0. 3313
-0.9627
0*4669
CHI-15.00
GAMMA- 1,5
2ETA-
0*70
0. Y/H*-
0*7?
Z/H = 0.
ETA= 0.25
... (W*D
-0*9674
-0*Q**do
O.q^Q t
“0*40* t
0.1311
-0.4/76
0.4408
LLLlLJ
0*1123
0*20a4
__
-0.QB41
1 713
“0 « 3 2 3 0
-0(0590
Q*Ql321 —
t W »D 1
-0*4670
.
-0*2485
0.1700
-0.5230
Oi i (13
0.0560
0*2745
1U.D1
-.0*6239
0*3726
0.5814
0*1800
0* 2613
-0.6039
0*5926
CHI -30.00
GAMMA* 1.5
ZET A =
0.70
X /b
,
0. Y/H=-
D.75
2/h* 0.
ETa* 0.25
(W.L J
-0.8642 "
0*1191
0,0435
-0.355/
0*0541
-0(5085
0.4748
(U.L)
0*1448
0* 34V 3
0.1026
0.2716
-0. 3692
-0*1270
QiQ-ZXJ
(W.D )
-0*2838
-0. 1022
0.2647
“0 , 369A
0. a / 18
0*0654
0*2670
_ ( U .0 )
0*5022
0_,445_I_ .
0,2060
0. 1547
-0*6176
0*2962
CHI -45.00
GAMMA- 1*5
ZETA =
0*70
X/H
0* Y/H--0.75
2/H* 11*
£IA= 0*25
(W.L)
-0.7677
0*3246
0.6647
-0,2100
0.0301
-0*35/7
0*5346
IU.L)
0.0594
0*3966
0.2301
0*2730
-0*2466
— 0*2136
0*1/34
I W*D 1
-0,1062
-0*0198
0.2467
-0.2468
0.2730
0*1406
0*2270
(U.D)
-0*2055
■»-
0*3643
0.2 vQo
0.1601
0*0258
-0*4456
0*2041
CHI-60,00
GAMMA* 1.5
2ETA =
0*70
X/H
0, Y/H--0.75
lift? Oi
ETA* Qi25
(W.L) ""
-O t 7253
0,5009
0.(558
-0.1172
0*0716
-0*6081
0*6181
(U.L)
-0.1172
0.5 755
0*2.818
_ Hi2Q75
-0*1735
r 0*323.2
0* lbflO
(W.D)
0*0596
-0,029 i
0.130O
-0.1735
0*2075
0*2331
0*1436
(U.pl
-5*1961
0*2129
0*1662
0.0914
-0*0391
-0*2876
0*1225
CHI-75.00
GAMMA* 1.5
2ETA =
0, 70
;;/h
0. Y/H--0.75
. _ Z/ttEL
LT A= 0*25 .
(w»lL
-0.6953
Q.61a2
0.8191
-0.0914
0*06/8
-0*6039
0*7036
(U.L)
-0.3054
0.3302
0.2763
Q. 1 407
__ -0*1335
-Qi4A6L
0*1665
(W.D)
0,2333
-0.1262
-0.0424
-0*1335
0* 140 /
Q • 3666
0*00X3
(U.D)
_ -0,1040
0,0864
0.0732
0.035b
-0*0315
-0*1396
0*0320
CHI-90.00
GAMMA* 1.5
2 ET A =
0, to
X/H
0. Y/H*-0. 75
2/H* 0.
£TA = 0*25
(W.L)
-0.5628
0 * 6466
0.626 7
-0*0933
0*0953
“0*48/5
0* 7421
(U.L)
-0.4042
0.2604
0.2451
0*1059
-0*1059
-0*3100
0*1745
' 0,4042
- 0*0000
- 0,2604
0«0000
- 0.2451
0*0000
-0*1059_
-6*pooo
0*1059
0*0000
0*5100
- 0.0000
-0*1745
0*0000
164
TABLE 25.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR T = 1.5, C = 0.70, AND tj = 0.25
(f) y/H = -0.375
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
1
| »-3»QQ
GAMMA ■ 1»5 ZE
I A* 0*70 X
/H» {
1. Y/H 3 -Q
*_57 22B-5--0*
__EIA*_0.25
.
(•♦L)
-1*5767
-0.0583
1*2036
-0*7295
0*7309
-0*8472
0*4710
(UiL j
-0.0224
-0.1)646 ...
-0.3H27 . ...
-0*047,2- __
-0*4637
-0*0246
-0*0176
(WtPI
-0.9013
-0*4769
'0*0566
-0*8637
-0*0472
-0*0376
0*3868
IU*D)
“1*4670
0*6600
Q • *745
0*0117
0*3844
-1*4787
0*8483
CHI* 3*00
GAMMA = 1*5
ZET A =
u* 70
X/H» 0. Y/H— 0*37
Z/H- 0*
... £.TA.-,Q«Z5 .
IW*L)
-1*5767
-0*0585
1*0715
-0*7295
0*5710
-0.8472
0*6710
( U*L )
0*0224
0*0648
-0*2806
0*0472
-0*8234
-5.1Q248
0*0176
(U* 0)
-0*8765
-0.3970
0*0536
-0*8234
0*0472
-0.0531
0*4264
tu*o>
-1.2787
0*8975
0*9745
0*1001
0* 3844
-1.3788
0*7974
CHI»15*00
GAMMA* 1.3
ZET A-
0 * to
Z/H— o* Y/H— 0*37
Z/H = Of
ET A = 0*23
<W*L)
-1*5250
0*0388
0*59/9
-0*6542
0*3189
-0*6708
0*6930
(UtL)
0.0917
0*3034
-0*045 7
0*2.172
-0*6824
“0.1235
0*0661
4 W*D 1
-0*7493
-0*2031
0.2373
-0.6824
0*2172
-0*0669
0*4793
1U*0 1
-0*9510
. 0*90Q9
...._ .0*6 9 Z s
0*2213
0*3199
-1*1723
0*6796
CHI *30*00
GAMMA 3 1.3
ZUA S
. .0* 70
X/H= 0* Y/H— 0*37
Z/H = Q*
ETA = 0*23
.
(U*LI
-1*4102
0*2993
0*0394
— 0* 4b49
0 • 14 7b
-0*9434
0*7641
4U*LI
0*0750
...0*3096
0*2301
0.3341
-Q • 4b96
“0*2392
Q.A755 -
<w*0 )
-0*5106
0*0213
0*4038
“0*4696
0. 3341
-0.0410
0*4911
<U*0 1
-0*6596
0*7707
0*6960
0*2333
0* 1628
-0*9130
0*3173
CHI *45*00
GAMMA* 1.5
ZfcT A -
. 0*70
X/H = 0* Y/H-“0*J7
_ Z/H* 0*
E TA= 0.23
4W»L)
-1*3361
0*6184
0.9704
-0*2686
0*0983
-1*06 73
0*8870
(UtL )
-0*0846
0*5 763
0*4048
0*3213
“0 ■ 2996
“0*40bl
0*2550
(W*D)
-0*2510
0*1338
6*3898
-0*2996
0* 3213
0*0463
0*4334
<U*0 1
-0*4719
0*5452
0*4636
Q.i9l2
0*0149
-0*6631
0*3539
CHi *60*00
GAMMA* 1*5
ZET A-
0* 7 0
X/H- .0,... . . _Y/H— 0,5/
Z/H = 0.
ETA= 0*23
—
(Will
-1*3588
0*9061
1*1434
-0*1466
0*1012
“1*2102
1*0547
(UtL)
-0.3290
0*3417
0*4 3.41
0.2343
-0.1998 .
riUAAiS. . . -
0*1072
( W*D )
0*0209
0*0924
0*2348
-0*1998
0*2345
0*2207
0*2922
(U*0)
-0*3248
0*3094
0*2631
0*1049
-0*0495
-0.4297
0*2046
CM I *75*00
GAMMA- 1*5
ZLT A =
0* <0
.Z/H". 0* . Y / H-— 0* 3 f
i/M- 0 •
ETA = .Ii4i3_
1 W»L 1
-1*4026
1*1170
1 * JOu 1
-0*1122
0*1086
“1*2905
1*2292
(UtL )
-0*5573
0*4604
0*4138
0*1348
-0*1475
-0*7121
0*3056
4 M * 6 j
0*3358
-0*0903
-0*0194
-0*1473
0*1548
0*4834
0*0511
(U*0)
-0*1.716
0*1233
0*1101
0*0394
-0*0352
-0*2109
0.0819
CHi *90*00"
GAMMA- 1*5
Z_EIA-
0*70
X/H = . 0* Y /H--0* 3 7
Z/H* . 0,
eta=
V :: ’-T~ -
( W * L )
-1.3358
1*2335
1*3902
-0.1111
0*1111
-1*2241
1*3446
(U»L )
-0*6863
0*3 765
0*34/5
0*1140
-0*1140
-0*8003
0*242.5
(W*P)
0*6863
-0*3763
-0.3475
-0.1140
0*1140
0*8003
-0*2425
4U»DI
-0*0000
0 * OQOO
0*0000
-0*0000
0*0000
-0*0000
0*0000
6+ 16T-T
L-15^9
165
TABLE 25.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 0.70, AND r\ = 0.25
(g) y/H = 0
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 1 1
to ground effect
CHI --3.GQ
GAMMA 2 1.5
2ETA-
0.70
X/H= (Ja . Y/H= Q, .
. 0*
fcTA* 0*25.
( W • L |
lU.LI
-2.0746
0.0153
0*0047
-0*107i_
0.9889
-0.3456
-0.6150
-0*0518. .
0.9192
-0.9533
-1*2598
0*0671
0*619/
-0.0555
<*•01
(U*0 »
-1.1026
-2.5027
-0*4004
1*7675
-0.1002
1.6460
-0*9333
0.0070
-0.0518
0.4070
-0*1493
-2*5097
0.5529
1.7605
CHI * 3.00
GAMMA * 1.5
,1£TA°
0.70
Q. Y/H= .0*
2/H= Q* _
LT3 = 0*25
tU.L )
-2.0746
-0.0153
0 aO<24 7
0*1073
0.6/71
-0*1521
-0.6130
Oj 0 3 1.6
0.7236
. -C *.9107 ...
-1.2598
-0*0671
0.8197
0.0 5-55
iw*PI
4 V • 0 »
-1*1594
-2.2827
-0.2233
1*7954
0.1002
1.6460
-0.910/
0.1047
0.0516
0.4070
-0.2487
-2.3874
0.6874
1.6907
CHI -15.00
GAMMA = 1.5
2ET A*
0.70
x/h= o. mi_= Q*.
22h = 0*_.
ETA- 0.23
(U#L )
-2.0567
-0.0942
0.1545
0.7961
. .0*24*1 _
-0.7280
0.2376
0.4102
-0.7536 . .
-1*3287
-0* 3-3X2
0.8825
0.2.216
_ IHjOI
^ lUiPl
-1*1564
-1*6485
0 • 1 h69
1. /260
0. 4723
1. I 1 it
-0.7536
0*2396
0.2376
0.^352
-0*4029
-2*0881
0*9005
1*4864
ZET A»
. .22 H = 0 * .
ETA- 0*25.
1U.L )
Iki.L 1
-2*0530
-0.2777
U.5650
0*964 1
-0.5118
.0*3606
0. 1901
-0.5126
-1*5412
-0*6383
1*0767
0*5040. -
. IM»D1
(UtDi
-0.9905
-1*1108
0.5247
1.4200
0.7830
1.3648
-0.5126
0.2736
0. 3606
0. 1650
-0*4780
-1*6445
1*0373
1*1464
CHI -45.00
GAMMA “ 1.5
ZET A =
O. Yu
x/Hs a. Y/H- a.
A/H= U*_ .
£Ta- 0.23
IttlL )
(UiL )
-1.1666
-0.5471
1.0939
L. 3343
0.8760
-0.2924
0.1187
-0.32 Oil
-1.6742
-Q.8660
1.3863
Q.AA7B
ItftO)
tU.DJ
-0.7044
-0*9442
0.6621
0*9487
0.6444
0*9144
-0.3206
0*2039
0. 3409
0.0100
-0.3835
-1*1700
1.0029
0*7648
GAMMA = l.b
ZETA"
2/Hs 0 T Y/H= n.
7/Ma ^
-£I*= 0*2 3
(WiLl
-2.4171
— 0> 6041
1.6027
0.6916
1*7426
fl.iTl.li
-0*1606
0*1129
-2.2642
-1.0489
1.7634
0 1 _
U»D)
_LU»CI
-0*2969
-0.6036
0.5674
0.5126
0*6524
0*4831
-0*2098
0.1100
0.2448
-0.0536
-0.0870
-0.713*
0*7772
0.4028
GAMMAs 1.5
ZFTAt
O. 7Q
X/h« q. y/h« n.
_ 6TA» 0.33
lUtU
III 4 I 1
-2.6558
-0.9448
1*9907
O.AA42
2*1147
0.6079
-0.1201
(X.240Q
0.1145
-2*6367
-1.1040
2*1108
LU ti>J
1H»D1
(UtD)
0.2621
-0.2754
0.2105
0.1699
0.2515
0*1421
-0.1527
0.0407
0.1600
-0.0346
0.4-148
-0.3142
0.3432
0*1291
— -
CHI =90*00
GAMMA 2 1.5
2ET A =
0.70
X/H= 0. Y/H= 0.
i/h± Qm
ETA" 0*25,
(WjL)
IU.LI
-2.6696
-0.9394
2.1977
0.3119
2*3046
0.2966
-0.1170
Q. 1 17Q
0*1170
-0*1170
- -2.5726
=1*0544
2*3147
Ufcik l
<W*DI .
(U.D)
0.9394
-0.0000
-0*3119
0.0000
-0*2968
Q.OQUO
-0*1170
0.0000
0*1170
-0*0000
1.0544
-0*0000
-0*19*9
0*0000
16 6
TABLE 26
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1-00, AND r?- 0.25
<a) y/H « -2.25
Correction factors for correcting from a wind tunnel which is
6+^T-rr
L-l^
167
TABLE 26.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR } * 1.5, C - 1-00, AND V = 0 25
(b) y/H = -1.875
Correction factors for correcting from a wind tunnel
which is
.
8
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
1 ■
CHI— 3.Q0
. I W.L)
-0.1490
2FTA« l.QQ )Uti= 0* Y/H— 1*87 -il*
-Q.Q56/ 0*0733 -0*103/
-ft . Q 1 4 7 _ -G 4_Q.fi .3 2 - 0 .0142
-0*3312
-0*2100-
-0.0433
0.0003
0*0221
-0*3956
0*0490
0.0000- ’
tttiOL
tU.Oi
-Q.188Q
-0.3336
-0*1242 -0.0140
0*1296 0*2364
-0.2100
0*062*
-0*0142
0*2134
0.1126
U23
CMI * S>QQ -
tyiLi
GAMMA" L*J5
-Q.149Q
-0.0567 0.0705
-0*1057
-0*3242
-0*0633
-Q.QQQ3
0*0490
lUtLJ
(M*D1
tUiXXi
0*0119 —
-0.1652
-0.2739
-0*1005 0*0140
0*16-66 0.Z364
-0*1877
0*0631
2/h» CL*
0*0142
0*2136
0*0223
-0.3370
0*0671
0*1057
CHI "15*00
(WtD
1*5
-otirn'.
-0.0406 0*06^2.
-0.0913
n» 06 fl 2
-0*2956
-ft. 1*71
-0*0465
-n.nn 1 a,
0*0303
-r, , nnfift
iUtU
(WiD)
<U*D1
, Q.P565
-0.118B
-Q.162Z
-0.0533 0*066/
0.1BV6 .0*2166
-0*1421
0*1053
0*0662
0*1952
0.0222
-0*2680
0*0666
0*0662
--
---
2 / H i-XU
CH I "30*00
IWtLl
GAMMA ° 1«L ...
-0*1084
0 .00 3 B 0.1239
-0.051/
0.1185
-0.2333
*0*046/
0*0556
(UiLl
(WtDi
-0.0714
-0*1114
-0.DQ66 0.1150
0*1623 0*166/
-0*0960
O.iOiO
0.1165.
0. 1435
0*0244
-0*2134
0*0695
0*0406
i/h= a*
-El A*-0*25
-
CHI "45*00
_ *Tw»L)
OAMMA * l ( i 5
-0.0606
0.0620 0.1827
0.138? O.g 696
-0*0036
Q* 1 385
-0.1605
-G. Q7^7
-0*0570
-Q.QQ/i
0*0654
-n. QQQ3
(U*L) .
<W*D|
|Ut0l
-0,0467
-0.0697
0.0146 0.1314
Q.U57 0*1019
-0*0737
0*0775
0*1366
0*0738
0*0*: / 0
-0*1472
0*0663
0*0363
-
ZFTA* 1.00 A/H = Q , Y/H"— 1.87
Z/H" 0.
CHI "60*00
( W ♦ L )
GAMMA" 1*5 —
-0*0417
n - 1 t Afl
0.1141 0.24Q2
Q . 1 ?66 Q.Q444
0*0294
0*1369
-0.0679
-0*0753
-0.0711
-Q.niAi
0*0667
. -0*0013-
<UtLJ
IW»DI
tUtOJ
V 1 1 1 VS.-
-0,0436
-0*0177
0*0079 0*1116
0*0659 0*0402
-0*0757
0.0484
0*1269
-0*009* — -
0*0321
-0*0841
0*0636
0*0176
r. A MM Am ] ^ K
ZETA= 1*00 X /H = 0. Y/H— 1.6/
2/H" 0.
IA." 0*25
CHI "75*00
(WtU
-0.0629
0*0625
0.1438 0.2790
0.0932 0.0316
0.0253
0. 1Q11
-0.0313
-0*0662 .
-8*0387
0*1185
—0.0079
(W*Dt
tU*D»
-0.0440
-0.0079
-0.0185 0*0627
0*0247 0*0080
-0*0883
0.0259
0.1011
-0.0172
Q.0444
-0.0319
0*0006
- :
7 PT As 1*00 X/H* 0* Y/H"— 1*87
1/H" 0.
FTA ,
— T
CHI "90*00
GAMMA* 1*5
_ a _ n a *4
0*1500 0.1 914
. -fi*Q082_
_ 0*00 82 ...
-n.0752 /:
^~0*15A2
-8*8276
Ot^f T8
Oil 688
JJLlLJ
(U*L )
IH.Dl
_ w iwCJl
0.0272
_-A*0Z2Z
0.0551* * 0*0026
-0*0561 — Q *00.2 6
0.0927
-0*0927
-0.0922
0*0927-
—8.0655
0*0455
—0*0000
tU»Dl
-0.00Q0
0*0000 -0*0000
-0*
0*
—
168
TABLE 26.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, £ = 1.00, AND rj = 0.25
(c) y/H = -1.50
Correction foctors for
correcting from o wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
1
to ground effect
T 4 — 1
^hI » dcr GAMMA- 1.5 zeta- i,oq x/h= q. y/h— 1.50 4/h= q.
<w*u
(U*L)
--
-0*2792
-0.0210
-0.1236
-0.0215
0.1278
-0.1734
-0.2028
-0.0215
-0. 34o6
-0. 3409
-0*0764
0.0005
0 • 0 1 8 7
“0*4361
(W.D)
(U*D)
-0.3221
-0.3695
-0.2273
0,2263
-0.0211
0.3299
-0.3409
0.0666
-6.0215
0.2919
0*0793
- 0*0001
0*1136
0*1596
CHI* 3,00
GAMMA* 1.5
ZETA- 1.00
;;/H= 0* Y/H=-I.50
Z/H-" 0*
FTi= n ,
fc-Lfl >*** 2
—
(W. L ]
^0*1792
-0.1236
0*1186
-0.2028
(U,L)
(W»D)
0*0210
-0*2915
0.0215
. ..... -0*1945
-0.1386
0.021 1
0.0215
-0.3103
0 Q7Z4
-O.OOQ5
(U»D)
-0.2929
0,2447
0.3299
0.1008
0.2919
0*0187
“0.3937
Q.Q7 93
0*0901
9a 1156 -
0*1439
1^*00 GAMMA- 1*5 ZETA- 1>0Q X/H= Q t Y /H- -1. 50 1
. _ -0*2596 -0.0995
IVtL) 0*0999 0*102.9 __
<*»PI -0,2255 -0.1260
IVf&l -0,1710 0*2 554
9*1261 -0*1811 “C.1US -0*0785
-9* 0 6 16 — — 0,1026 -Q,24*7 -0*0026
0*1005 -0*2447 0,1926 . ___ Q.Q192
Q,3Q20___ 0,1407 _ 0,2641. -0,3177
0*0016
0 * 0004 .
0*1187
0.1147
CHI-30.00
GAMMA- 1.5
ZETA- 1.00 X/H =
0, ¥ / Hj -
1 , 5 Q X/H = Q .
E.TAr 0,2 5.. .
-
(WtU
(UfL)
-Q.2Q78
9*1707
-0,0326
0,1 776
0*1765
0,0064
-0,1220
-0,2461
-0*0858
... .
(U*DI
.... -0*1533
-Q*Q912
-0,Q547._
0*2254
0*1720
.0*2269
-0*1743
0,1437
0.1768
0.1856
-0*0061
0.0210
-0*2349
0*0894
0*0000.
0*1196
0*0816
CHI -45,00
GAMMA- 1.5
ZETA- 1.00 ’ X/H»
0. Y/H--1.50
Z/H- 0.
ETA- 0.2 5
( N • L)
-0,1514
0.0535
.JbiML..
0.0463
“9*0515
-0*1528
-o » 1 341
-0.0999
(U.L)
0.1915
0.2047
(W*P1
10*0}
-0,1088
-0,0480
-0,0171
0,1643
Stmt
9*1285
'“0.1341
0,1132
V > A J*rl_
0*2035
0.0039
tO » 0121
0.0253
“0,1612
9.1050
OiOfil2_
0*1170
0,0511
CHI -60. 00 GAMMA- 1,5 ZETA- 1*00 X/H- 0
.r./H»rU5.Q £ZM= 0, ET A- 0.25
-- <W*L1 -6*1281 9*12.91
UUkl 0 » 1 S73 0*1830
<W*QJ.. -0,0896 -0,0168
IW*P) -0,0219 0,0952
0.3253 -0,0043
Si±£<t$2 0*1819
0,16.06 -0,1247
0*0452 0*0722
-0*0640
-0*1247
Q* 1819
-0*0014
-0*1238
-Q.Q245
0*0351
-0.0941.
CHI *75,00 GAMMA* 1 ,5 ZEIA^ . 1,00 X/H- 0* Y/H— i . 50 z/ h- 0.
ETA= 0*25 .
IH«L1 -0.1602
LU lU Q . Q 05 7
LWjJLL . _ -0*0701.
IVfftJ -0*0922
0,1728 0*5743
0*1361 0*0306
-0,0432 0,0802
0,0362 0,0076
-0,0074 0,0008
P . 141 Q — Q » 1?76
-0,1276 0.1410
0,0343 -0*0270
-0*1528
-11*05 5 3
0*0575
-0*0364
0*1334
0,0011
0*1079
0*0229
0.1802-
-Q » QQ 49
0*0844
0,0019
CHI -90.00
GAMMA- 1.5 ZETA-
1,00 X/H-
0, Y/H— 1,50 Z/H= 0,
ETA- 0.25
S¥ #JJ .
lWtkl
-0,1074
0*0272
0,1868
Q ■ 0 866
0.3907 -0.0428
0a0074 0*1222
0.0428
-0.1446
-0*0950
0.0950
- IMaPI
. _ . IU*Oi
-0,0272
-Q .OQQQ
-0,0066
0,0000
-0.QQ26 -0.1222
0.0000 -o.
-0* 1222
0.1222
0*
-0.0000
0*0356
0*0000
6+iCl -r l
169
TABLE 26.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, f = 1.00, AND 17 = 0.25
(d) y/H = -1.125
CHI »-3»QU G AMMA 8 1.5
-0,5449
*0324__
- 0 . 592 a
-0.4527
0.1367
-0.0003
0.17*3
0*2357
CHI* 3.00
GAMMA = 1.5 ZETA =
1*00 A/H = 0.
, Y/H=-l
•12 Z/H = 0*
ETA = 0.25
(W»L)
-0*54*9
-0.2637
0*2657
-0.4004
-0 .264b
-0*1445
0.1367
(U.L)
0*0334
0*0346
.“0*2 92 8
0*0343
-0.5377
-0*0009 .
0*0003
(W.D)
-0.5520
-0*3563"
0.0339
-0.5377
0.0343
-0*0144
0.1793
(U.D)
-0.3442
0*3372
0*4771
0.1245
0.4076
-0,4687
0.212b
CHI *15.00 GAMMA = 1*5 Z£IAiL_ AiOfl. AZH 3 ._£j tm-l.li Z2H* Q. £IA* . Q*25 _
( W.L )
-0*5121
-0.2231
0*2445
-0.3636
-0.2647
-0.1484
0*1406
(U.L )
. 0*1364 .
0*1644 ...
-0.1624 -
0.1630 . .
-0.43-73
-0.0046
0.0013
(W.D)
-0,4536
-0*2516
0.1610
-0.4373
0.1630
-0.0162
0*1856
(U.D)
-0,1796
0*3677
0.4329
0.1963
0.3623
-0.3780
0*1694
CHI =30, GU
GAMMA*. 1*5
_Z.EIA= X/h =
0* Y/R*-l*12
Z/H = 0.
ETA = 0*25
(W.L)
-0*4263
-0.1109
0*2862
-0.2645
-0.2028
-0.1618
0.1536
(O.LI
„ 0*2654
..._JU27fi6
-Q.Q578__
0.2759
-0.3184
-0*0105
0*0029
IWfDI
-0.3327
-0.1307
0.2710
-0.3184
0.2759
-0.0143
0.1877
I U *D 1
-0.0630
0*3336
0.3114
0.2147
0.2380
-0.2777
0.1191
CHI *45.00
GAMMA* 1.5
4 t IAt_ 2*00 ..A/h =
0 . r/ri=-i*l2
<-/H = v*
ETA- 0.25
--
(W.L)
-0.3357
0*0310
0.3 /U 8
-0.1461
-0*1037
-0.1876
0*1790
JUfU_.
0*2867
0*3114
0*0207
0*3068
-0.2376
-0.0201
0*0046
(M.O)
-0*2433
-0*0559
0*2961
-0*2376
0.3068
-0.0057
0.1817
(U.D)
-0.0152
0*2453
0*1626
0.1728
0.0861
-0.1880
0.0725
CHI *60.00
GAMMA= 1.5
2ETA = 1,00 X/h=
0. Y/H--1.
.12 Z/H = 0.
ETA- 0.25
(W.D
-0.3007
0,1533
0.4564
-0.0702
-0*0086
-0.2305
0.2235
(U.L I
0.2230
0,2667
0.0461
0.2613
-0.1986
-0.0384
0*0054
(W.D)
-0,1835
-0,0359
0.2359
-0.1986
0*2613
0.0151
0.1627
(U.OJ
0,0007
0,1396
0.0509
C. 1085
-0*0234
-0.1078
0.0310
CHI *75.00
OAMMA5_l*5
2ET A= 1,00
.;/h= 0. Y/H*-l,12 l/H- 0 ,
ETA- 0.25
(W.L)
-0.3463
0,2281
0,5134
-0,0632
0.0563
“0.2831
0*2913
(U*D
0.1152
0,1905
4*0334
0,1936
-Q.179A
_ -0*0784
-o.ooai
(W.D)
-0,1199
-0,0605
0,1257
-0,1795
0.1936
0.0596
0*1190
(U.DI
_0,0Q52
0_*J&07
. .. Ot 0066
0.0480
-0.0403
. . -0*0428
0*0027
CHI-90.00
GAMMA* 1.5 ZETA*
1,00 x/h=
0* Y/H 3 -1i
>12 L/H- 0*
ETA- 0,25
—
(W.L)
-0.3819
0.2614
0,5325
-0.0942
0* 0942
-Q.28 78
0*3556
(U.L)
0.0272
0,1176
0,0025
0*1581
-0.1582
-0*1308
-0*0404
(W.D)
-0*0272
-0,1176
-0.0025
-0*1581
0.1581
0*1308
0*0404
(U.p)
-0,0000
0,0000
0.0000
-0.0000
0*0000
- 0*0000
0,0000
TABLE 26.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1.00, AND 1 J - 0.25
(e) y/H = -0.75
Correction foctors for correcting from a wind tunnel which is
closed
closed on bottom
only
to free air
closed
closed on bottom
only
to ground effect
-1*0508
-0*0547
—I * 10 34
—0 *62 36
0* i. to JL.t»
-0*647 3
-0*0570
0. 7120
-0* 7 taa
-1.0050
0*0544 .
Q*190Q
“1<lQQ5Q
-0.0567
^..0 *5677..
-0*0984
-fl*67SQ
CHI * 3*00
GAMMA= 1.3
ZET A= 1.00
X/H= 0. Y/H — 0.
15 . .i/H* 0*
..ETA* 0*25
. _
(W.L)
-1*0508
-0.5357
0 .0390
-0* 7 766
0*1019
-0*2720
(<J*L )
0*0547
0*0578
-0*5726
0.0567
_ — Q * 945 5
-0.QQ7Q
(W,D)
-1*0524
-0*6390
0.0370
-0.9433
0*036 7
-0.1068
fU.D)
-0,4577
0*302 7
0* 7 120
0.1366
0*5677
-0*6143
“ CHI-15.00
GAMMA* 1.5
ZETA* 1.00
J4/H* o* Y/H — 0,
73 .
ETA* Q*23_
<w»u
-0.9875
-0,4384
0.526b
-0*7062
-0*0176
-0*2793
iu.l r
0.2561
0.2719
-0.3890
Q * 266.4 _
-0.7623 ._.
. . -0*0103
IW.DI
-0,8994
-Q_*4396
0*26/9
-0.7623
0*2664
-0*1169
<u*Pi
-0*2027
0*3664
0*6366
0*2926
0*4914
-0*4954
-0,8254
0*4124
-0.6801
-0*0291
.jlzh^-Oj lia= 0*25
y 0 i -0*5213 — 0* 04b /
p_9b 0*4330 - “0*5636
3/2 - 0*6636 0*4350
376 0*3310 0*2911
-0* 6611
0*4162
-0*492_9
0*0251
0*0094
- 0 * 39 46 .
0*4361
o*oao
0*3149
0*0176
0*3119
0*1137
-0*5141
0*2959
-0*34 78 _
0 .024 6
Y/H— 0* 73 4/H.vOi ETA5 _ 0*23 ..
<t/3 -0*1/13 0*0631 -0*4266
bi+b 0.4b23 -0*2930 ...... .~Q«Q664
433 -0*2930 0*3623 -0*052B
b/7 0*136/ -0*0372 -0*1321
0*2723
0*0446
GAMMA J 1.5 Z£TA =
1*00 X/H* Q*
_Qa.34A3.
0*2549
-0*0505
0*0680
.Ha.LL42
0.0535
0.1795
0*0140
-0.1395
0*2536
-0*2392
0*0636
0* 122 3-
-0.2392
0*2336
-0.0557
=0*6140
-0*1123
0*0369
- 0.0521
0*0012
0*1488
0*0041
CHI *90.00
( W*L |
GAMMA - 1* 5 2ETA=
-0*7029
-0.0272
- 0*0000
JL.0.0 A /Ha 0
0*4106
0* ( 5b 4
0*0024
-0.0024
0*0000
iiH=_dA
-0*13 i t
-0*1960
- 0*0000
-0*1667
- 0*0000
L-15^9
171
TABLE 26.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, r = 1.00, AND tj = 0.25
(f) y/H = -0.375
Correction factors for correcting from a wind tunnel which is
8
closed
on
closed
bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
CHI >>3.00
—
C> A MM A = 1.5
1
2ETA =
L^QU.. X/H = Q. . Y/H*-
Q.3-L
_Z/H= fix.
£TA= 0*25
IMtLi
-1.B402
-0.6923
1.6124
-1.3353
1.1728
-0.5049
0*4429
(U.L)
-0.0811
-0.0934
-1.0287
-0*0879
-1.6011
0.0067
-0*0055
IW*PI
-1*8903
-1.0617
-0.0926
-1.6011
-0.0679
-0.2892
0.5194
<u*ot
-0 . 9899
0*7361
1.0997
0.0309
0.7431
-1.0209
0. 7072
CHI = 3*00
GAMMA = 1.5
2t T A =
1x0 fiL X/l
4= 0. Y/H=-
Q.XL
Z/H = Q*_
_EIA = -0.25 .
(W*C)
-1,6402
-0*8923
1.3592
-1.3353
0.9055
-0.5049
0*4429
,
IU*L)
0.0811
0x0934
-0.9135
0.0879
- ^ A 5232
-0.0067
0*0053
r—
IW»0)
-1,8420
-0.9666
0.092b
-1.5232
0.0879
-0.3188
0.5544
i-
IU.D)
-0.7375
0,6419
1.0997
0.1947
0.7431
-0.9321
0*6472
t.
CHI-15.00
GAMMA = 1.5
At I A =
1.00 X/
1= 0. Y/H— 0.37
4/rt= Ox
LI A- .0.25 _
-
(VtL)
-1* 1211
-0* /469
0.9664
-1.2017
0.4927
-0.5194
0.4568
0*37 2X
0.4337
=0x8430 ....
Q . 4062
-i .2636
-0.0342
0.0275
(WtCLl
-1.6210
-0.6622
0.4299
-1.2636
0.4062
-0*3574
0*6014
-
(V«QJ_
-0,3386
0.9409
0.9766
0.4164
0.6233
-0,7570
0*5225
Z
CHI *30.00
GAMMA 1.3
ZtT A =
1.00 ;;/h- 0 . y/h=-
Q.H
Z/H = g*_
£16= 0*2.5
IMfLl
-1,4293
-0.3651
Q./6/4
-0.6617
0.2248
-0*5676
0*4985
(U.L 1
0.5617
0.68/7
. -Q.1966
-Q. £786
-0.0708
Ot 0552
-1.2454
-0.2601
0.6/67
-0.6766
0.6325
-0.3668
0*6185
(UtDl
-0.0676
0.8451
0*66/5
0.4793
0*3268
-0*5472
0*3457
CHI * 45 .00
GAMMA = 1.6
Zf T A =
1.00 X/Hc
n. y / h « - n » ^7
XYH. Q.
FTia 0,?*'
-
IMtLi—
— 1 . 1497
0.0252-
Q t ftlQ7 „ .
-0*5025 - -
0*442L
0.5782
(U«L )
0.5085
0.6977
0.0836
0.6187
-0*5705
-0*1102
0,0791
—
(Mtp)
IU«0)
-0*8963
0,0123
0,0153
0,5635
0,6.892
0,3446
-0,5705
0*3661
0*6187
0,0193
-0.3279
-0,3518
0.5857
0,2174
CHI *60.00
GAMMA* 1,5
Z£TA =
1,00 X/H*
0. Y/H*-0,37
Z/H- 0*
etab Q>2!}
— -
1 W*L )
IU*L 1
-1,0748
0,3115
0,4224
0.5406
0,9256
0.1806
-0,2792
0.1839
-Q. 3879
-0.79*6
0*7017
0x8826. -
UfOl
IU»Pj
-0.6151
0 * 0 liZ
0,1044
0,2956 .
Ox 5 06 Q
0,1341...
-0,3879
0,2038
0,4582
-0,0931
-0.22.72
-0.1884
0.4922
0.0917
CHI-75.00
GAMMA* 1.5
Z£TA= 1,00 X/H* 0,
Y/H—0.37
Z/H* 0.
ETA® 9.26 ■
iw#u
“1,1654
0,6366
1.0283
-0.2133
0*2060
-0*9620
0*8619
IU,L)
0.1260
0.3350
0.1293
0 . 3ns%
-Q. 2907
— 9t 1 7 76
0*0296
(W»D)
-0,3393
0.0354
0.2642
-0*2907
0.3OA5
-0*0486
0.3241
. IU,0)
0,0077
0,0895
0.0343
0.0775
-0.0691
-0*0699
0.0119
CHI *90.00
GAMMA* 1.5
ZET A= 1.00 X/H= 0.
, Y / H* -Ox 3.7
Z/H= 0.
ETA* 0.25
J
<W»L>
-r.2200
0.7422
1.06/4
-0.2150
0.2150 .
-1.8110
0*9571
: (U*L)
0,0272
0,1312
0.0023
0*2267
-0.2267
-0.0955
' iw,oi
-0,0272
-0,1312
-0.0023
-0*2267
0,2267
0*1995
0*0955
(U.D)
-0.0000
0,0000
0.0000
-0,0000
0,0000
-0*0000
o.aoao
172
TABLE 26.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y * 1.5, C = 1.00, AND T} = 0.25
(g) y/H = o
Correction factors for correcting from o wind tunnel which is
closed
on bottom
only
to free air
closed
on bottom
only
to ground effect
-Q.Q718
-2.5BB6
-G * 13 61
-1*0417
...
-1*0107
-0*1375
...1*9.62.8..-
-2*5773
0*0718
-2*6121
-1*6376
L ETA® i,oo
-0*853 0
Of 1381
-0*8374
1*7612
-0*8050
0*13/5
1*9628
“1 *6653
0*1056
-1*8585
0*2136
1*4767.
-1*8565
0* 1056
9*8305
GA MMA" A» 1*00 X/H® 0*
-2 *44U7_
0*3169
-Q*b3bl
Of 6442
-0*3454
1*7900
1 * 0 V 1 6
-0*3105
-.1*465/
0*4849
-1*537 9.
0*4890
CHI «3O*00
GAMMA* 1*5
2ET A*
1*00
X/H = 0* Y/H® 0*
Z/H = 0*
ETA* 0*25
( W»L )
-2*1363
-0*0684
. .. .0*976 0
._-l*0445
0*3879 ......
-1*0919
0*9760
( U«L 1
0*4125
1*0386
0*2745
0 * / 359
-1*0460
-0*3234
0*3029
( W*0)
-2*0410
0*23/0
1.0331
-1*0460
0*7359
-0*9950
1*2830
(U*D»
-0,5878
—
._ll5091
.1*326.7
0*5584
0*3368
-1.1463
0*9507
_ CHI -45*00
GAMMA 3 1*5
2ETA =
O'
o
X/H® 0* Y/H® 0*
Z/H* 0*
ETA® 0*25
(W*L)
-1*9245
0*5974
1*1586
... -0*5968
0*2422
-1*3212
1*1942
(U*U>
0*2568
1*0939
0*6121
0.6957
-0*6548
-0.4389
0*3982
(W»D>
-1.5841
0*5714
1*0829
-0.6548
0*6957
-0*9293
1*2262
(U.D)
-0*3266
1*0093
0.8069
__ 0*4160
0.0205
-0*7426
0*5932
CHI -60*00
GAMMA- 1.3
Lt 1 A®
1*00
X/H® 0* Y/H- 0*
4/H = 0*
ETA® 0*25
( W*L )
-1*9778
1*1600
1*5364
_ -0*3263
0*2303
_ -1*6496 .
1*4883
(U*L >
0*0327
0*8851
0.6279
0*4996
-0*4283
“0*4670
0*3835
(W*D>
-1*1302
0*5819
0*8614
-0*4283
0*4996
-0*7020
1*0102
iu*oi
-0*1595
0*4993
0*3814
0*2245
-0*1094
. -0*3840 . _ ... .
0*2748
CHI -75.00
GAMMA 3 1*5
ZETA®
1*00
X/H* 0* Y/H® 0*
2/H® 0*
ETA® 0*25
•
—
-2.2113
-0*0531
-0*6195
-0*0411
-1*9662
-0*3796
-0*3078
-0*1242
.-Z tW l
0*0272
-0*0272
..-SUOftPSL.
1 # 00 X/H* 0.
0*0023
-0.0Q23
-0*2387
0*2387
“0* OftOOL _
-0*2116
0*2116
-Q*QOOO
6t£ T-T
L-15^9
173
TABLE 27
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 2.00, AND r/ = 0.25
(a) y/H = -2.25
$
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 ,
to grour
id effect
CHI ■-3.0U
GAMMA" I,J
ZETA*
2,uo
.‘i/H = o. Y/H— 2*25
Z/H= 0.
ET A= 0.25
UHL.L.
-3*QZ1 2
-3*30<6t.
-0.0142
-0.01 36
-0*3922
lUfLI
(W*P)
{ U t D )
-0*0099
-0.0902
-0.0846
-0.0099
-0.0414
u. 1606
-0.0319
-0.0099
0.1853
-0.0099
-0.0876
0.1073
-0.0876
-0.0099
-0.0000
-0.0027
. -0*143.9.
0*0060
0.0461
• - . -9*9513_.
CHI ■ 3*00
GAMMA" 1*5
ZtT A"
2.00
X/H* 0. Y/H— 2.25
Z/H = 0.
ETA" 0.25
(W»L )
-0.0212
-&i0 Qhb
._ -0*0126
-0.0125
0.0099
. 0.1853 ..
-0.0135
0.0099
-0.0684
Q. 1 1 55
-0* 3857
-0.0684
0.0099
. -0*0077 .
0*0000
-0.0027
rQ.1726
-- -0*0067
-0.0000
0*0463
(W*0)
. .... (u*pj
0*0099
-0.0711
0*0099
-0.0221
_ 0*1634
CKI -is *00
GAMMA" 1.5
ZfcTA-
2*00
X/H" 0. Y/H*-2 * 25
Z/H" 0*
ETA- 0*25
... - tW»Li
-0.0098
Q.0Q51
0.QQ24
-0 3612
-0.0080
0.0000
-0.0028
0*0070
-0.0002
0.0466
IU,L)
t W*D J
(UtDI
Q.Q4T6
-0,0347
. . -0*0216
0*0474
0.0147
0.1564
0.0244
0*0473
0.173L
0.0475
-0.0319
_ 0.1179
-0.0319
0.0475
0.1706
CHI •3076o
GAMMA- 1* 5
2ETA =
~2 _ ,‘00 _ " "
X/H= 0. Y/H— 2*25
Z/H = 0.
ETA* 0.25
.. ....
0*0222
0*0388
0.0401
0.0587
0.Q821
0.1384
Q.Q311
0.0826
0.0021
0.0991
-0* 3135
0*0021
0.0826
0.1356 ___
-0.0035 .
0.0000
-0.0028
-0.1043
-0*0022— .
-0*0004
0.0468
0.0284
(U*L >
IWtOJ
<U«0 )
0*0826
-0*0008
-0.0052
0.0822
0.0489
0.1275
CHI *45*00
GAMMA* 1*5
ZETA-
2 « jo
;/H= 0. »/H— 2.2$
H = i* •
E l A- J * 2 5
tW.L )
0*0641
0.0843
0.0903
0.0749
-0.2543
-0.0108
0*0094
<U*L)
(Wf D)
IU»D)
0.0963
0.0118
-0.0076
0*0954
0*0615
0.0855
0.071 3
0.0952
0.0907
0.0962
0.0146
0.0661
0.0146
0.0962
0.0873
0.0001
-0.0028
-0 . 0736
-Q. 0008
0*0469
0*0195
CHI >60.00
GAMMA" 1.5
AET A =
2.UC
X/H= 0.
Y/H— 2.25
Z/H = 0,
ETA= 0.25
-0.0148
0.0001-
-0*0026
-0*0466- -
<W*L }
iu,Li_
(W*0)
(U.p)
0.1002
p«0862 .
-0.0002
-0*0129
0.1280
0.U842
0*0492
0.0435
‘"“i7oo~“
a*1547
0,0549
0.0164
0..0138
0.1408
0.0590
0*0636
0.1150
0,0860.
0*0024
0*11125-
-0.1952
0.0024
0.0860
Q.Q383 _
0*0130
-0*0016
0*0469
0*0110 —
'xThT'oY
CHI -75.00
(WiL)
GAMMA = 1.5
0.1072
ZET A =
Y/H— 2.25
0.1800
0.0264
0.0529
0.PM1
Z/H- 0.
_0*li2Z
0.0611
-0.0295
0.0116 _
ETA= 0.25
-Q* 1462
(U»L)
( W*D )
(U.DI
0.0612
-0.0311
-0.0065
-O.0295
0.0611
Q.OOli
0*0001
-0.0015
-0,0161 . .. .
-0*0042
0*0459
- -
CHI-90.00
GAMMA" 1,5
ZETA-
2*00
X/H" 0*
Y/H— 2*25
Z/H= 0*
ETA- 0*25
IWjL-L.
-_ 0 _* Q6 1 7
0.1550
0.201 7
.0*1056
— Q* 1 Q**
.0.0,18
Q| .
(U.L)
0.0589
0*0245
-0*0136
0.0640
-0*0640
-0,0050
-0*0395
< * 1 0 )
-0.0589
-0,0245
0 • 0 l 3 8
-0.0640
0*0640
0*0050
0*0395
(U»D)
- 0,0000
0,0000
- 0.0000
-Q.QOQO
0.0000
- 0*0000
0*0000
174
TABLE 27. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR r = 1.5, C = 2-00, AND rj- 0.25
(b) y/H = -1.875
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
T 1
to ground effect
1
[—3.00
gamma - i,5__ I£TA= iAjOg xjh*
Q« Y/H — 1*07
4/H = Q*.— .
EIA= 0.23
< w*u )
-0*0402 -0*0210
-0.1006
-0*0303
- 0 * 3«*42
-0*00 vo
[ u *vj
-0.0143 , t9*Q143
-0.0743
-0*0143
-0* 1442
-0.0000
( W»D )
-0*1420 -0.0916
- 0 . 014:1
-0.1442
-0.0143
0.0014
[U»DI
-0*0600 0.2013
0.2622
0.1361
0.2367
-O.iVbi
0*0095
o.oooo
0*0326
0.0&3A
[■ 3.00
GAMMA* 1*6
ZETA* 2.00
0. Y7n5^1jJ
3 7 Z/H° fl .
XIA=_Q*25
._ ...
( WiL )
-0.0402
-0.0210
-0.0966
-0*0305
-0.6333
-0*00 v 6
[ U ,L )
0*0143
0.0143
-0.0466
Q*Q143_.
-Q.1123
o.aooo
<wtd~i
-6.1157
-0*0642
0.0143
-0.1171
0*0143
0*0013
(U»D1
-0.0268
0*2084
0*2622
0*1490
0*2567
- 0 * 1 <60
0.0095
-0*0000
0*0626
0*0366
Z E T A =
2.00 X/h*
0. J t/HS!
-_U8J
EIA- 0*25
... . .......
.. .
(W.L)
[U.L )
-0.0241
0.0687
-0.0042
0.0685
-0.0736
Q *(105-6
-0.0140
. .0*0687
-0. 4903
“0,0652
-0*0101
..... 0.0000
0*0096
-0*0002—
IW.DJ
(U.O)
-0.0640
0,0143
-0,0120 .
0*2039
0.0684
0*2445
-0.0632
0*1566
0 • OtJB <
Q.C40V
0*0012
-0*1423
0*0532
0*04/1
CHI -30.00
GAMMA 3 1.5
2. GO X/H=
o. j_/h=
-1*0 (
£ZH= 0*
_.ETA= 0.22
(W.LI
0*0210
0.1195
0*0431
-0.0137
0.0545
0.0322
.0*1195
-0.4259
. __-Q*0167
-0*0112
-0.0000
0*0109
-0*0004
0*0535
0*0347
fW.O]
(U*0)
-0.0155
0*0275
0.0360
0.1687
0.1188
Q.1940
-0.0167
0.1340
0.1195
0* 1901
0*0012
-0*1065
CHI *45.00
GAMMA- 1.5
IL IA2_
5 .rtf) Y /Us
0* Y/H=
-1*87
4/H- 0*
ETA- 0*25
<WtL)
iij*i \
0*0793
0.1397
0*1061
0*1388
0.0620
0*0727
0.0929
0*1397
-0.3390
0.0013 _
-0*0136
0*0000
0*0132
-Q.QQQ V
1 u i
(M.O)
IU*D)
0.0026
0.0155
0*0549
0*1142
0.1383
0.1247
0.0013
0*0905
0*1397
0*1200
0*0013
-0*0751
0*0536
0*0237
CHI *60.00
GAMMA- 1.5
ZETA*
2.00 X/h-
0. y/h-
-1.87
Z/H- 0.
ETA- 0*25
(W.L)
0*1273
0*1641
0.1382
0*0560
0*1460
-0*2520
-0*0164
-0*J>141
-0*0022—
(U.L )
0j,l26 5
.0*1243
0*1265
0*1265
0*0467
0*0016
-0*0442
0*0534
0*0132
(W.D)
(U.O)
-0*0137
0*0001
0*0301
0*0595
0.1231
0*0548
-0.0162
0.0463
C HI " 7 6*00 6A MMA= 1.3 iEIA~ . 2*00 X/H = 0* ..Y/H— 1.87 22H- 0*
(W*L)
0.1310
0*1932
0*0872
0*1992
0.1622
-0.1760
"0*0573
-0*0312
-Q.npnft
0*0309
(U.L )
0.0940
0*0123
-0*0676
0*0189
0*0945
-0*0024
0*0030
-0*0163
0*0520
0*0026
(W.D)
(U,D )
-0,0548
0.0006
-0,0058
0,0215
0*0832
0 . 0060
CHI -90.00
GAMMA = 1.5
ZETA- _**00 . X/H=.
0. Y/h-
\z mm * A Q / 2 / H - 0#
_ „ 41 y.' *7 f i v w — .
|W,LI
1 1 * _ 1 \
0*0648
0.0804
0 • io25
0*0563
-0,0663
0,0000
0*2502
-0,0365
0*1178
0*0995
-0 • 1 i ; 8
. -QlQV.95
-0.0530
-0*0111
0*0667
—0*0433
1W ♦ 0 J
(U*D)
-0.0884
-0.0000
0*0365
-0.0000
-0.0995
-0.0000
0*0995
0*0000
0*0111
-0*0000
0*0433
0*0000
L-15^9
175
CHI -75*00 GAMMA- 1 .5 ZETA- 2*00 _Qm Y/H— 1*50 2/H* Q,
1W*L) 0* 1332 0*2389 0.2473 0*1065
1U»L ) 0*1607 0*1460 -0*0196 JO #15 80
<*•01 -0*1213 -0.0443 0*1410 -0.1164
(UfD) 0*0156 0.0363 -0*0005 0*0340
LTA- Q*25_ __ -
-0*2063 -0*0534 0*0523
-C* 1164 0*0019 -0*0120
0*1508 -0*0046 0*0722
-0*0137 -0*0183 0*0023
CHI *90*00
GAMMA- 1.5
ZE.TA» 2*00 X/H= (
Y/H--1.50
. 2/h s 0* ...
. LTA= 0*i5 ... .
(W#LI
0*0252
0*2126
0*3114
0*1130
-0.1130
-Q.0S78
0*0996
(U»L 1
0*1536
0x1^56 .. _ .
-Q.QZS2
Q.163Q
-0*1630
-fl»Q093
-0*0574
-0*1536
-0*1056
0*0782
-0*1630
0* 1630
0*0093
0*0574
(U*D )
-0.0000
0*0000
0*0000
-0*0000
0*0000
-0*0000
0*0000
TABLE 27.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C = 2.00, AND 7 ] = 0.25
(d) y/H = -1.125
Correction factors for
correcting from
s
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
to free air
closed
on bottom
only
to ground effect
-0*2660
-OtOAfil.—
-0.5873
-0,0457
2 fOQ X/H*
0. Y/H c -1* 12
0*
EXA* 0.25
>0.1957
-0.4447
-0.2300
-1.1363
-0.0361
>0.0399
. -0*3 9 tO
-D.Q4QQ
-Q. 5*5Q
-q* oaoi
-0*4230
-0.0398
-0.5450
-0.0400
-0.0423
0*3673
0.6539
0,2240
0.6408
-0.2698
0.0342
O.OQOJ^-
0.1220
0.1433
GAMMA* 1.5 ..
-0,2640
0.04 01
-0,5210
0,0349
-2ELAi
-0,1957
0*0399
-0*3546
0*4064
-0*4779
0.2776
-1.1092
-Q»4T19__
0,0400
0.6408
-0,2197
0*4319
-0.3564
- “<3*1914 .
0.1907
0.6037
0.0353
-Q.QOQ7
0.1250
0.1028
-0.2600
0,1613
-JSIAje IaOQ X/H =
-0.0888
0.3800
Q. 1159
0,3889
-0,0324
0*2725
0.2357
_ Qa35_45_._
-0.0562
0.1561
0.2649
fl.2676
-0.1259
0.0675
0.0112
-0.0046
0.3880
0.2656
0*2160
^.0282-
0.3524
0.0784
-0.1806
0.1342
12Us*il*12
0.3745
-0*0 974
0.2605
-0.0191
0.1644
-0.2913
-0.2429
0.0668
-0. 8272
-0.0412
0.0391
-0*2149..
0.0010
-0*0017
0.3338
-0.0451
Q.W41
0.4459
-0.1441
0.0745
_EIA- 0*25
-0.5975
-0*0496
0*0471
-0.1586
0*0020
-0.0035
0.3924
-0.0450
8*1262
0*2485
-0.0989
0*0487
EJA«_- 0*2.5
-0,3709
-0.0669
0*0685
— Q . 1 HQ A . _
Q . ttflZi-j
0.3624
-0.0430
0.1244
0.0574
-0.0566
0.02 39
-0,1871
-0.1057
0.1008
-Q. 2429
O-rOl 06
0,2913
-0.0354
8*1470
-0.0422
-0.0174
0.0087
0.0494
— 0.2800-
-0.2800
- 0,0000
-0,0494
■0.2-800
0,2800
0,0000
-0.1654
— 0.0067
-0.0067
- 0,0000
6^1-1
L-15^9
12S
177
TABLE 27.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 2 00, AND tj = 0.25
(e) y/H = -0.75
Correction foctors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to ground effect
— 1 1 *
CHI «~3« 00 G AMMA = 1,5 ZETA= 2.00 X/H = Q» Y/hs-O.73 -EIAs- 0*2-3
I N*L)
-0.0971
-Q • 7293
-0.4735
-0*6112
-A • 3 944
-0*0639
o*o#iv
( U *L )
-0,0861
-0,0866
-1 , i 066
-0.0869
.-1* 3636 ..
-QtOQQi
0*0403 — —
IWiD )
-1*4991
-1*13:41
— 0*0 033
-1*3634
-0*0639
-0*1337
0*2 206
. <UtD)
-0.1162
0*3213 .
1.2 016
0*2663
1*1676
-0*362#
0*3660
C HI- 3.00 GAMMA= 1.5
Z.0Q ... JUii?_X3U 1
^JA»_ 0 ^i 5
(W*L)
(U*L )
-0.8971
0.0861
— 0 • 7293
0.0866
— 0*4 c4 i .
—0*6 11a
-1. 3839
-1*2410
-0*0889
0*0002
0*0819
0 . OH 69
— 0to»t3
(W«D)
—1.3 i 9 7
-1*00 / j
0«0a33
-1*2410
0*0639
—0*1366
0*222-7
<U»D)
0*0388
Q*QJill
1*2.016
Q* Aft 30
1* 1676
-0*3463
0*2291
CHl-15. 00 GAMMA- 1.5 ZLTa- 2*00 X/h- Q * Y/H=-0.75 X/H- Q. ETA- Q.25
(W«L1
(U»L )
-0*8129
0*4114
-£L*6J99. -
0*4066
-1.2 /l*'
-9
0*0848
-0.7134
0*41*2
-0.9788
flAOfllZ
-0*0018
(W»0»
-1*1215
-0.7403
0*4084
“$♦.£758
Qi 4102
-0*1427
0*2283
(U.D)
0*2673
0*7447
1*0912
0 * 8627
1* 0364
-0*2734
0*1820
CHI -30.00
GAMMA = 1*3
Z E T A = *.00
;;/h= o* y/h=-q*/3
l/M* 0*
ETA- 0*25
IW.L)
-0*5859
-0*3949
-0.1572
-0.4881
_ . -0*9946
-0*09 76
0*0912
(U.L)
0.7102
0*7035
-0.4263
0.7073
-0*6911
JO* 002 9
_ -Q*0Q36 _
fW.O)
-0.8422
-0*4557
0*7030
-0*6971
_.0*_70I3
“0*1451
0*2414
(U.D)
0.3748
0 * /04a
Q« / t)0v
0*27*9
0*7434 _
-0*2001
0*1296
CHI-45.00
GAMMA- 1.5
Z ET A = 2.00 X/H- 0.
Y/H--0.75
Z/H- 0.
ETA- 0.25
IW »L ]
fU*L )
-0*3229
0.8200
-0*0948
0.6062
0*1828
-0.2061
0.O141 .
-0.6112
-Q.3364
-0*1166
- 0.0039
0*1112
-0*007 9
« U*p_1
-0,6806
0*3207
-0.2955
0* a342
0.6032
0*3 761
“0* 3 304
0*4529
0.«l4l
0.3356
-0.1442
-Q.1322
0*2404
0.0813
CHI -60,00
GAMMA= 1*3
ZETA= 2*00 X/H- 0*
Y/H =-Q* / 3
Z/H = 0 i_.
ELIA 1 : Q.25
(X*L)
IU*L)
-0.77/7
0.7403
0. /S98
0 • 7096
-0 , s T / Z
“CL. 09 9 ... _
-O.X37**
-0. 7- *9
-0.4969
-0«/3 7-
“0./476
— Q. Q 1 76
(W*D»
IU*D|
-0.6364
0.2205
-0.2644
0.3239
0.7076
0.0429
-0.4969
0.2690
0. 7274
-0. 0058
-0.1376
-0.0664
0.2344
0.0349
CHI -75*00
GAMMA- 1.3
ZET A = 2.00 X/H = 0*
Y/H— 0* 73
__i/H= 0*
ETA- 0t25 .
(W*L>
(U*L )
-0*2606
0.5970
0*1900
0.5148
' 0*7260
-0*2698
-0*0296
Q*5642
0* 00 J 3
-Q* 51Q3 _
“0.2311
0*il96
(M*0)
iu.D)
-0.6253
0,1236
-0.2980
0,1329
0*5075
-0.0635
-0.5103
0.1370
0.5642
-0.1080
“0.1150
-0*0133
0*1123-
-0*0042
CH I #90.00
GAMMA- 1*5
ZETA= 2*00. 2/H = 0*
Y/H— 0*75
Z/H- 0*
_ ETA- 0*25 _
—
“ iw.L)
(U.L )
-0.5055
0.5404
0*1589
0.3386
0.8312
-0,3060
-0.17U
Qj.4689
0*1711
_ _^0«_4869
“0*3344
0*0515—
.043301
“0.1503
<W*D)
(U ♦ D 1_
-0.5404
-0.0000
-0.3386
0*0000
0.3060
0*0000
-0*4689
“0*
0,4609
0.
-0*0515
-0*0000
0*1503
0*0000
178
TABLE 27.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, C - 2.00, AND V = 0.25
(f) y/H = -0.375
Correction factors for correcting from a wind tunnel which is
—
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CMt 4-3*00
QAHHA- i,s>
2ET A = 2*00 X/H =
0* Y/H»-0.37
2/H* 0.
ETA« 0.7*1
Tliitu
MtoU
-3*3549
-0*1273
-2*6604
— . rQ.*2263
2*0362
-3.5011
-3*1152
0*7641
-4.070 1
-0*2417
-QlQQQfr
0*2349
ilUAl
-4*4060
-0.4456
-3*5227
0.7509
-0.2263
2*3632
-4*0201
0*2177
-0*2269
2*2706
-0*3679
-0.6635
Q 4 QQQj
0.4974
0.5332
CHI- 3*00
OAMHA- 1.5
2£TA« 2*00 X/H *
0* Y/H-
-0.3/ 2/H* 0*
illeU
-3.3569
0*2273
-2*6604
0*2263
1*6312
-3*1152
. _Q*2269
0*4077
— ^ 4 7fl? l
-0.2417
(ttlPl
-4*1812
-1*2731
0*2263
-3.7621
0*2269
-0*3991
Ukfcl-
0*0299
1*1057
2*3831
0*6266
2*2706
-0*5967
0*5090^
0*4792
CHI«15»~QP
cXmtX* i.b
2£TA- 7.00 X/hT
0* Y/H--Q.'
47 2/H- Q.
p? A= Q* 2 5
UtiLl _
tiixLi
. -3*0416
1*0676
-2.5911.
1*0626
1*1029
-2.5630
-2*6328
1.0654
-0*0711
_ - 3. 1 5 99
-0*2496
0*2418
(WiPI
-3*5441
-2*6049
1*0624
-3*1299
1*0654
-0*4142
0*5249
fU*D)
0*6966
1*5490
2*0799
1*1706
1*9654
-0*4737
0*3764
- J** i/n— u. 1 1
£IA= 0*25
—
UtLi
-2.9441
-1*1207
0*9357
-1*6990
n
0*2463
1*7917
— 1*2331
1 .7400
“2 « ? 543
LM.ftl
-2.6740
-1* 7212
. 1*5673
1*7327
1*2653
-2*2543
1.7400
1*1644
-0*4217
0*5331
141*01
0.9489
.4. .
-0*3352
0*2631-
.
CHI -46*00
gAHHA* 1*5 ZETA-
<00 X/H-
-£Lt Y/H— 0.37
i/H- 0. _
ETA- Q.25
_l»fU
-0*22 8?
1*1110.
-1*2413.
Q* 0377
-0*3218
0*3124
IU*L )
1*8367
uwt . ...
-1.0289
1*8244
*1 a 5785
‘***1 .
-1*9940
-1*9512
_ 1*8089
-1*5765
1*8244
-0*4155
0*5273
IU*PI
0*6463
1*2066
0.4137
1*0530
0*2839
-0.2078
0*1335
CH! -60*00
__4AHHA- 1*5 ~ 2ET A"
2*00 X/H-~
0* Y /H*— 0* 3 /
2/H* 0.
FTAs 0.2b
-
l**Li
~UO»79
-6*2669
1*3721
-0*6660
0*3325
_ “0*4119.
0*3991
l^lkl
1a4763 _
— 1*4146
-0*6587
1.4494
-1 . 1 800
0.0200
tMtfti
— - *1a 4644 -fiifclll
_ 1*4127
-1*1800
1.4494
-0*3865
0*4987
1MI
0*6627
-0*0961
0*6267
-0.2287
-Q«Q9Q5
0*0539
-UTA* 2*00 X/h« 0* Y/H —6.3 r i/H» Q> FTA. Q.2H
-igf-Wl
-uun
WttM
-Ptwyg __ _
9i»iM Z&J& L2S L
-0*534.9 .0* 9 06 7
6*2402. -0*1281
-0*5550
_ 1*0146
-0*9544
0*2554
0*5294
1*0144 _
-0*2228
CHIMQtW ftAflHA* 1*5 &£IA« <la£Q A/h« 0* y/h— q**7 z/h« q. ft*, o.^
-6*5491. _ ... 4*4444
. . 0*0712 =ft4tm
-0*5094 0*4124
-0*0054
X
ItftU) -1*3715 0*0906 1*539* -0*6305
jy*Li 9*9363 0*5149 -0*4879 0.7839
IMjlH I _ — “0* 9343 -0* 5149 0*4829 _ -0*7639
til *01 -Q.OOQD 0 + q qqq 0* 0000 —0 * 0000
0 . 6306 -0*7402 ft*X21 8
-0*7639 0.1354 -fl*249fl
0*7639 -0*1524 0 *2490
6ilQT- r l
L-15^9
179
TABLE 27.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 2.00, AND tj = 0.25
(g) y/H = 0
Correction foctors for
correcting from
0 wind tunnel
which is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
r ' ' T 1
CHI— 3*00
GAMMA* 1*5.
ZETA 3 2,00 X/H= 0* Y/H
0, Z/H = 0, ETA* 0,25
IW*L)
-7.4805
-5,8356
8, 5841
-6,6532
7,5039
-0,8274
0,8174
(M*LJ
-0,4201
-0,4261
. .-6,4997
-0,4232
-7*7422
0,0031
-0*002 9
IWtDl
-8*9302
-6,5122
-0,4259
-7,7822
-0*4232
-1,1480
1*2700
lUtDl
-1.5072
1.4A77 —
iA.fl.4fl 6
0,0572
? t ?221
— -1*6444
--- 1*4304
CHI* 3,00
GAMMA- 1,5
ZET A*
2«Q0
X/H-
0, Y/H*
0,
Z7H« 0,
614* 0,25
(M.L I
-7,4805
-5.8356
7.3756
5*9069
_ --0*8234-
0.6176
IVtL)
__ WaPJ
(U«D 1
0,4201
-8,6364
-0,5600
0,4261
-6,1089
2,1484
-6,0963
0.4259
3*flAflfl
0,4232
-7.4340
-7,4340
0,4232
^ . A3 3 I
-0,0031
-1,2024
_--l*4446
0,0029
1,3250
1,3938
...
CH| *i5,gg
GAMMA 3 lit
ZETA 3
2,00
X/H 3
0. Y/H*
Q*
Z/H= 0.
£TA= 0*25
(U,LI
-6,7925
-5,1028
—
.4*6X23
-5*9424
3*3485
. _ -0*8499
(U83M
IMtDl
<U*DI
1*9248
-7*4264
0,8353
-
1.9539
-4,7532
2* 9 7 fl.9
..^4*7406
1.9538
1*2446
_ 1*9396
-6*1516
1 .0559
-6*1616
1*9396
2.7364
-0,0148
-1.2749
-t *1205 . .
0,0143
1*3984
CHI *3 0*00
GAMMA- 1*5
ZETA-
2,00
X/H-
.0* - Y/H- 0*
2/H- 0*
ETA- 0*25
-5*1036
—3 .263 3
1.0474
-4*1778
1*5618- -
-0,9257
0*9145
_ (UtL 1
2*9165
2*9715
-2 *7439
2,9436
-4,1*41
-0,0293
0,0279
JNfOl
-5.4*71
-2*7568
2*97X3 —
- _-4*1841
2,9434
-1*3031
1.4273
(U*D)
1.4601
2.9334
1.8777
2.2337
1.3473 —
-0*1X34
_ 0*4097
. .
CHI-45, 00
GAMMA- 1,5
ZETA-
2«QQ
X/H-
0* Y/H* 0,
2/H- 0,
ETA- 0*25
(W.L 1
-3.4562
-1.3300
2.5047
-2.3873
0,9690
-1,0709
1,0573
IU,L)
2*7449
_7*A179
-1.2258
2*7829
-2*6190
-0,0379
0,0350
<¥*0J
“3*8745
-1*2387
. 2*8174
-2*6190
2,7829
-1,2555
1,3803
ru,ot
1.2135
2,0611
0.5958
1*6641 .
... Q.QB12
-Q, 4504
Q«3970_
CHI* 60. 00
GAMMA- 1,5
2ETA-
2,00
Ix/Ha
0* Y/H- 0*
2/H- 0,
ETA- 0,25
( W.L 1
-2,6252
.
-0.0193
2,5254
-1.3130
9,9213
. 1 m %\29
1,2937-
(U.LJ
1,9834
2 » 00 68
-0,4709
1*9986
-1,7130
-0,0152
0,0042
(W.D)
-2*8167
-0.4840..
2.0057
-1.7130
1,9986
-1,1037
1*22 90
«U>C»
0*7260
1*0342
-Q.QQ6 7
Q*098Q
-0,4377
-0,1720
0*1347
CHI- 75, 00 GAMMA- 1 .5 ZETA- 2. 00 X /H- Q. LZH5.JU. 2/H = U, £ A* U*25 —
(W.L)
-2.6292
0.6382
2.6060
-0.9806
0.9511 _
-1*4445
\ *4144
<U*L>
1.4201
1*1681
-0.3037
1.3062
-1.2467
0.1139
-0*1341
(W»D)
-2.0499
-0.3171
1.1645
-1.2467
1.3062
-0.8032
. 0,9294
(U.D)
0.3334
0.3098
-0.0758
0.3325
.“0.2986
0*0028
-Q.Q7J7
,
- -
'
CHI-90. 00
GAMMA- 1.5
ZETA- 2.00 A/H-
"0. ’ ” Y/H- O'. "
2/H- 0.
ETA- 0*25
( W »L )
-2.6692
0*9235
2*3515
0*9549
... . 0,9549-
-1.9142
—1*8264-
(U.L)
1.3053
0.4724
-0.4566
Q.9549
-0*9549
0.3504
-0,4425
(W»D)
-1.3053
-0.4724
0.4566
-0.9549
0.9549
-0*3504
0,4425
ju.pj
QtOOQQ _
0*0000
Q.QOQQ
-0,0000
-0,0000
0,0000
180
TABLE %8
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND tf= 0.25
(a) y/H = -2.25
Correction factors for
correcting from o wind tunnel
which is
S
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grout
id effect
' i 1 1
1
cm r *- 3 ,oo
GAMMA* 1,5
ZETA = 4.00 X/H
3 0. Y/H*-2
.25 Z/H ■ 0.
ETA* 0*25
- - (W.L)
-0.PQ2S
-Q.QQ07
-Q.Q3Q6
I UiLl_ _
(W.D)
(U»DI
-0.0099
._ -0*0534
0*0467.
-0.0099
-0.0269
0*1 /2 1
-0.0223
-0*0099
0.16/ 7
— Q. 0099
-0*0510
-0.0210
-0.0099
-0.0000
-0.0025
0.0000
0.0241
a*.ox n
—
_ .tni* 3.UU GAMMA 3 1,5
1W.L) —0.0028
ZETA = 4,00 X/H* 0, Y/H*“2
-0.0007 -0.0294
.25 Z/H- 0.
-0.0016
ETA = 0.25
-0*4000
lU.U )
IW*D)
(U.DI
0.0099
-0,0338
0.0626
0.0099
“0.00 /3
0.1 '/42
-0.0026
0.00*9
0.1877
0.0099
“0*031 J
0*1493
-0.0313
0*0099
0*0000
'-0*0025
-0*0000
0*0241
t n 1 * 1 5 * 00 GAMMA = i.3
2ETA= 4.00 X/H
. Of .... Y / h = -2 • 2 5 2/H= 0.
EIA4 0*25
rw.u
0.0092
0.0114
-0.015 1
0.0104
-0.3807
n>nnifi
(U*L >
fW.DJ
0.0472
0*0034
0,0472
..p.gisQ
0^0346
0.047?
0*0472
0*0059
.0*0000
-0*0000
tU*D)
0,0746
0,1648
0.1756
0.1447
0.1752
-0.0701
0*0241
0*0201
..... _.
GAMMA* 1.5
Z£_T A* 4,00 X/H*
0* Y/H=-2.22 Z/H = 0.
ETA= 0.25
fW.UI
0,0434
0,0456
0.0216
0*044/
-0.3385
— 0*001 3
1 U ♦ L 1
tw.oi
IU.D1
0*0819
0.0378
0.0655
0.0bi6
0*0644
0*1332
0 • 0 b y i
0.081b
0.1410
0 » 0816
0.0403
0«_U81
0.0403
0.Q816
0.140b
0.0000
-0*0025
. . -0*0^25
— — Q.QO I 1
-0*0001 _
0 • 0242
0*0151
CHN45.60
GAMMA* 1,5
Z E T A = 4.00 X/H =
0. Y/H=-2.23
Z/H= 0*
ETA= 0.25
-
f«*L>
0,0897
0.0926
0.0 / 0 6
0,09lA
— -
fU*L 1
<**D)
CU»D)
0.0947
0.0504
0.0403
0,0945
0*0 / /0
0*0866
0,081 t
0,0948
0.0937
0 • 0 946
0*0229
0*0779
0*0229
0*0946
0*0933
0*0000
-0*0025
— 0 *03/6
-0*0001
0*Q242__
0*-0lQ7
C Hi *40*00 , _GAMMA»_1 % 5 ZETA* 4.00 X/H = 0. Y/H=-2*25 2 /h* 0. ' ETA= 0.25
(WfU 0.1350
tUf L > 0.0 826
! fW» 0t 0.03 77
<U*6| 0.0132
0. 1391 0.1199
0.0822 0*0b9l
Q,Qb44 O.Ob^i
0*0938 0* 0464
- 0 ±1231
0*0822 0.0402
0.0402 0,0822
SUl&IU 0 . 0^ 3 i
_ -Q.0Q22 , 0.0019
o.oo oi - a.»gC3
-QiOG25__ 0*02 4 2
.. -Q.Q24Q fliliit
CHI ■ 7 5 .00 GAMMA* 1.5 2 ETA* 4.00 X/H = 6 «
-jW-.U
fU»P)
0.0505
O.O QJA
0 . 1 / 1 /
-0*0018
0 .04V 0
0.0300
0.0116
_CHI-90,.00 GAMM A* 1. 5. _ ZLTA=__A*0Q
T /H a -2 * 25 Z/H«
0.034
0.046 <
-0.011 4
0.0502
0.0058
—O.OOi>L 2 _
Y/H=-2,25 Z/H = 0.
ETA* 0.25
-Q. 19QQ
0.0056
0.0502
0.0103
ETA= 0.25
-0.0041
0.0004 _
-0.0025
-Q.Ql 10
0.0031
— 0.0012 -
^* 02 AL .
0.^027
1“
QiL*n Q .1 770 0.1753
0*G4Q3. _ IU01A9.. -Q.0111
J-WfOl -0*0403 -0.0159 Q.0111
lyjlOi -Q.QQQQ Q .0000 Q.QQUQ
0.1626
0.0390
-0.Q390
-Q.QQQQ
- 0. 1628
-0*0390
0.0390
- 0.0000
0.0143
^a*Oi 3 L.
•Q.QQQQ
6 ^t-i
L-15^9
181
TABLE 28, - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND 77 = 0.25
(b) y/H = -1.875
Correction factors for correcting from a wind tunnel which is
close d
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI»-3.00 GAMMA* 1*5 2ETA- 4.00 _X/H = Q. Y/H*-1.87 i/H= 0*
i«iL)
“Q»P<?59
—0.0031
46 6
-0.0045
-Q. 5B33
<U*L)
tm»D)
— -Q.0142.
-Q ,Q854._
-0.0142
-XUQSTfl .. ..
-0.Q485
-0.Q142
“0.0142
46_
“0 i 0846
-0.0000
0.0000
0* 0277
0.0339
(U.D)
0.0987
0,2310
0.2695
0.1971
0.2691
“0.0984
CH I * 3.00
GAMMA- 1,5
i£T A* 4,00 X/H* 0
* Y/H=-1.87
i/H* 0.
ETA- Q.25
<W*L> "
-0.0059
-0.0031
-0.1433
-0.0045
-0 * <576^
-0 QflU
A < U »L )
L— <*Vt»
(U.OI
0*0142
“0*0572
0.1159
0,0142
“0.0287
0.2350
-0.0203
0.0142
-0*2695
0*0142
-0.0564
Q_, 2045 __
“0.0564
0.0142
Q.2691
0,0000
-0.0007
-0.0886
-0.0000
0*0277
. CHI -15. 00
GAMMA* 1*5
ZETA =
4.QQ K/H=
0. Y/H=-l • 87
l/H= 0.
ETA* 0.23
l W ,L )
"0.0113
0.014?
-Q .120 1
0.0128
-Q Qfli -
( U » L >
I WfD)
IU.0)
0.0681
-0.0038
0.1284
0.06E0
0.0248
0.2246
0.0332
0.0680
0.2520
0.0661
-0.Q03Q
0.2000
“Q.DQ30
0.0681
0.0000
-0 . 0008
-0.0000
0.0278
-
4 CHI *30.00
GAMMA* 1,5
ZETA =
4.0C X/H =
0. Y/M=-l * 87
Z/H- 0.
ETA* 0.25
IWtL) 0.06Q3 0*0635 -0.0647
0*1100 Q 1 1179 Q.0828
_LWjD( 0.0457 0.0743 0.1179
SUU&2 Q . 1 824 0.2022
- Q . Q 6 I9 .. — — — _-Q. 4fl4Q _ »Q.flnu Q.nau
0.1120 0.0465 Q ■ o ooo “0*0001
0*0465 0.1180 -O.QOOa 0.027*
0 . 2 . 0 L6 — -Q.Q43A Q.Q1A4
Chi * 45 . oo
GAMMA* 1,5 ZET A*
4,00 X/H- 0.
Y/H=—l .87
Z/H = 0.
ETA* 0.25
LMiLl
Q . 1265
0.1304
0.009?
0,1285
Will
0 » 1366
0*1164
0.1009
0.1366
0 . 0646
JMjDJ
- Q.QMA .
0.0924
0.1364
G .0646
0. 1366
IMtP )
0*0697
0.1212
0.1340
- Q * 1 0 a L_
0.1333
-Q.Q07Q
0.0001
“0,0008
-QiQ3a4
_Q. QQ1 9
- 0.0002
0.027&
_ Q.Q13Q
CHI -60,00
GAMMA* 1,5
4 ETA-
... 4,00
X/H =
0. Y/H*-
■1.B7
Z/H = 0,
ETA*" 0,25
(W.L5
Qt 1907
-
Q«0*U6
0.1935
-0. 3259
n ^
IU.L1
|W,D1
IU*DI
0,1196
. 0,0456
Q-i-fl27 Q
—
0.1191
0. Q.742
0« 0596
0.0827
0,1190
0.0654
0.1195
0.0464
0 . 05 i b
0*0464
0.1195
0. 0645
0.0001
-0.0008
“0,0004
0*0229
-
- — -
CHI-75.00
GAMMA* 1.5
ZET A =
4.00
X/H =
0. Y/H=-l,fl7
2/H* 0.
ETA* 0.25
IW.L)
IU.W
0,2299
0*0752
0,2400
0,0733
0.1388
0.0334
0.2351
.0, 0747_
-0.2641
-0.0029
C . 0747
0.0129
-0.0052
Q.0Q04
-0.0007
“0 . D 1 1 1
0*0050
1 W ,D J
IU,D»
... ....*rO*6o36
0.0022
0,0249
0*0165
0.0727
0.0144
-0,0029
-JCU02. 76
—
—
CHI *90.00
GAMMA* 1,5
ZETA*
4,00
A/H=^
0, Y/H=-
1.87
4/H= Q,
ETA- 0.25
IW,L }
0,2034
_0j2M6
0.1225
0.2199
-0*2199
-O.Q] fcc;
f U * L 1
IW.D}
i u * b i
0,0647
-0,0647
-0,0000
0,0390
-0,0390
... QtPQQQ
-0,0303
0.0303
.oiOQoa.
0.0653
“0.0653
“Q iQQQO
-0 . 055a-
0.0643
o * ooon
-0.0007
0.0007
“Q.QQQp
“0*0264
0*0264
182
TABLE 28. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR r * 1-*. C * < 0°. AN® 1 = 0 25
(c) y/H - -1.50
8
Correction factors for correcting from a wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 — 1
to ground effect
C HI — a. 0 0 GA MMA" 1.5 i£TA= 4*QH a/H* 0 •
Y/H— 1*50 U H= U*
ETA= 0*25
-0*01 14
-Q.3A62
-0*0026
0*0028
lUlli
-0*0223
-0*1069
-0*0223
-0*1577
-0*0000
0*0000
IMiOl
=0*1442
-0*1182
-0*0222
_ -0*1577
-0*0223
-0*0065
0*0808
iUl-CJ
0*1713
, Q*322i
0*4188
0*2818
. 0*6179
- . -0*1105
. GAMMA* 1*5
2EIA- 4«0Q A/ H*.
o* Y/H--i*>o
A/H= 0*
E.T A= 0*25
—0*0 164
-0*0114
-0*3563
-0*0134
-U.«Si44
=0*0024
0*0028
<U»L )
0*0223
0*0223
-0*063 U
0*0223
-0*1139
0*0000
-0*0000
4M»D1
-0*1205
-0*0743
0*.0222_
-QJ113V
0.Q2Z3
-0*0066
Ot 0395
lit^J
Q .1.3 3? 3 ..
fl*Al&8_ __
0*2960
0*4179
-fl *09.95
0*0418
CHI *15*00
GAMMA* 1*5
2£TA*
4*00
X/H* 0. Y/H — 1. 50
2/.H = 0_*
£JA* 0*25
( W«L ]
0*0102
0*0155
-0*3171
0*0129
— Q* 6443
-0*0027
. 0*0026— _
< U*L )
0^1066
a? 1065
0*0203 __
_0*1065.
-0*0308
0*0000
“0*0001
<W»D)
-0*0374
0*006?
. 0*1065
-0*0308
0*1065
-0*0066
0*0396
(U*D 1
0*2134
0 * 32 86
0*3914
0*2937
0*3905
--&AQ804
0*03.49
—
'
€81*30*00
GAMMA? 1*5
*£TAh_
4*00
X/H- J3.j Y / H ■ =1*3 ft.
4/H-. 0*.
£TA- 0*25
---
U*L 1
0*0659
0*0917
-0.2246
0*0889
-0*7423
-Of 0030
0*0029
(O.L )
' 0*1049
0* 1 647
0*0974
0*1846
0*0443
0*0001
-0*0001
tW.Ot
0*0396
0*0660
0*1846
0.0463
0*1649
“0*0067
0*0397
*0.01
0*1625
0*2666
0*2426
Of 3122
-0f06Qi
0*0261
CH1*46*0Q
GAMMA* 1.5__ 2ETA*
4*00
X/H* 0* Y/H— 1* 50
2/M* 0*
£TA* 0*25
(Nil)
0*1676
0*1946
-0.1031
0*1913
-0*6145
-0*0036
0.0035
|U*L >
0*2145
0*2141
0*1256
0*2144
Q»Q75$
0*0002
=0*0003
0*0676
0* 1142
0*2140
0*0745
0*2144
-0*0067
0*0398
10*01
0.1174
6.1787
0*2061
0*1603
0*2049
-0*0429
0*O184_
CHI -60.00
GAMMA- 1*5 2£TA*
4*00 X/H*
0*2942
Qa Y /H b -1*5.0..
i/H= 0*. ....
_£LA?_jQ*25
-0*4873 _
-0*0061
■—
<W*L 1
0*2842
0.0144
0*2893
UltLl
SL.U93
0*1882
11*0974
0*1869
0*0442
q I - ,
-0*0007
IHtDl
Q *0660 .
0.1880
.0*0462- -
0*1889
eMQU
0*0398
lUiftl
□ .0496
0*0679
Q.09H1
0*0767
0*0964
-0*02 71
0*0112
CHI -75.QQ GAMMA* 1.5 ZET*» 4. QO X/tt-.O* YVH— .L.30- .... 22ti« 0* £IA*-0*25
1H*L I 0.3340 Q.3544 0.1066 0**454 -Q* 3851
Ui*Lk 0.1214 0 a1212 0*0215 0*1240 -0*0295
tH*DJ -0.0341 0*0101 0*1205 *0*0295 .... 0*1240—
IU*DI 0*0103 0*0252 0*0174 0*0222 0*11145
1W.L> 0*2776 0*3357 _ 0*1722 0*21156 -0 * 305 4
IU*L I 0*1258 _ 0*06 36 -0*0720 - .1 0*1208 -0*1208
IM.D1 -Q * 125 6 -0*0838 0*0720 -0*1208- .0*1208
tUtpl -0*0000 -0*0000 0*0000 -Q*0QQQ 0*0000
- 0.0894 0*0090
-0*0277 0*0801
0*0040 —0*0220 —
-0*0040 0*0370
6l£ T-l
L-1549
183
TABLE 28. - Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, ? = 4.00, AND rj = 0.25
(d) y/H = -1.125
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI—3.00 GAMMA* 1*5
UlU .
IU»U
[ft.DI
LUjOJ
-Pi g???
-0.0397
-0*3773
0*2900
4,ug X/
-0*0397
-0*2834
_CLt5Q70_„
r/h=-i»i«
-0*2705
-0*0397
Q*73J4_
LI A* J.25
“1.5702-
-0.3502
-0.0397
0.J315
-o.oflia
- 0*0000
-0*0271
--.0*1393
Q.0056
0*0000
0*0646
. G.0I1X
CHI- 3*00 GAMMA = 1.5
1W.U
-0*0599
-0.0485
tU*L 1
0*0397
0,0397
IW.O)
-0.3008
-0.2066
IU.OI
0*3366
0.5319
C RL* 15.00
GAMMA 3 1*5
2ETA =
4*g0 x
iw.E)
-0.0134
-0.0017
IU.ll
0*1903
0,1900
<W*DJ
-0,1550
-0,0603
IU.0I
0.3703
0.5278
• ■
CHI *30.00
GAMMA 3 1*5
ZET A-
4.00 X
( W . L )
0.1176
0*130 /
( U iL 1
0.3306
0*3300
. tW.Dl
-0.0193
Q.O < be
tUlD)
0*3206
0*4361
CH I *4 5*00
GAMMA = 1.5
ZETA =
4.^0 X
<W.L 1
0.2913
0*3073
(U*L 1
0.3854
0.3841
(Midi
0*0305
0*1258
iHsOi
0.2107
0*2934
CHI *60.00
GAMMA- 1,5
2 1 1 A-
4.00 X,
- . U»L)
0.4464
0*4707
( U.L )
0.3455
0.3424
(W*OI
-0.0181
0.0771
UUPi
0.0970
0*1476
CHI *75.00
GAMMA- 1,5
2ETA =
4 , Of A ,
(W.L)
0.5084
0.5486
(U.L)
0.2493
0 • 2 3 do
(M.D)
-0.1452
-0.0509
(U.DI
0.0330
0.0516
- t -■
CHI-90.00
GAMMA- 1.5
ZET A =
4.00 X,
tW»L>
0.3671
0.4783
-0*1937
0.0397
0* 7334
-0*0541
0.0397
-0.2736
0*4620
ETA = 0*25
. -is SAifl..
-0*2736
0*0397
_Qj 7315
-fi*M56 _
0.0000
-0.0273
. " 0.1254
Y/H«-l*12 2/H= 0*
-0*7520
-0*0473
0*1900
0*6844
-0*0074
0*1902.
-0*1275
0* 4716
-0*5154.
0.U88 l
0*3300
... . . 0*5444
Y / H= — 1 * 12
.. -0*3 5^ Q _
0*1386
0*3640
. 0*3 52 Q
0*0901
0.3422
0*1569-
0. y/h=
0.6550
0.3304
0.0063
. 0*3962 .
X/H- 0
-0*2953.
0*3646
0*0562
0*2442
ETA= 0*25
-1.4450
-0.1275
0. 1902
0.6624
ETA= 0*25
- - “1.25XA.
0.0082
0. 3304
0.5422 —
EIA= 0*25
— ^X*Q1 7 3 -
0*0562
0.3648
0*3494 .
ETA- 0.25
-0*0060
Q.Q001
-0.0275
-Q.1012
0 *0056
- 0*0000
0*0058
-0*0001
0*0473
0*0543
0*0003
-0*0274
-0*0757
-0*0004
0*0675
-0*0007
0*0676
0*0202
0*3442
0.0096
0*13 01
0.*_Z41Q_...
C . 0096
C. 3442
C . 1531
0.0013
-0*0277
— Q . Q 3 j 2
- 0*11X0.9
-0.0018
0*0675
_0*01Z4-
- 0 * 03/9
0*23/2
0*0133
0*2445
-0 • 1 i b U
_ 0 _*_ 046_2
-0 *5648
-0*1180
0*2445
0 *0076
-Q«02Q5
0*0048
-0*0272
-Q»Q 132
-0.0065
0*0671
Os 0054
Y/H=-l*12 Z/H* 0*
IWiD)
0,2773
-0,2773
0*19 46
-0*1946
0.0000
-0*1810
0.1810
0.0000
0*2559
-0*2559
ETA = 0.25
-0.4222 _
-0.2559
0.2559
0*0000
“0.0551-
0.0214
-0.0214
-QiOQQO
184
TABLE 28.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y * 1.5, ? - 4.00, AND tj = 0.25
(e) y/H = -0.75
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
8
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
1 » ' ' 1 1
XH1 — 3.0Q _
fiAHHA* 1*3 Z
£TA« 6.00 JL/ii* Q* Y/H«-0*I5- . 2/H* 0*.
EIA« 0*25
(HiU
-0*3260
-0.2968
-2*1003
-0.3101
-3*1282
-0.0159
0.0156
lUtk)-
-0.0901
-0*0899
-0.904Q
-G.0900
-1.0617
-0*0001
-0*0001
(WiOJ
-ltlllS
-0*1166
-0*0899
-1*0677
-0*0900 — .
_?0*0A42-
0*1211-
HI * 3* 00 &AHMAA_1*A-_- Z£IA^_ _ 6*00^ A/tt*
2/H=. 0*
0*0899
0*9688 -Q.7524
,-0.7398
0*0899.
ZETA* _4*00
Y2h*-Q.75 z./h= o*
■Q.5679
QtQ»Q4
-Q.M64
0.4312
-fi»0H94
0*1326
1 .
-0.1 u .gs
- Q . 0966 .
0*8096
-0.2623 . _
0*0066
- 0*0060
0.8044
-0*2623
0*0096
- 0*0660
0^-1631
Oftfa-i/y
-0*2366
-o*32ia
_ 0*6 16 V
0.7206
‘*0. 7206
0.5259
-0*5339
-0.5226
0.5226
0*6519
-0.6519
L-15^9
TABLE 28.- Continued
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR ? = 1.5, C = 4.00, AND J? = 0.25
({) y/H = -0.375
185
Correction factors for correcting from a wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CMI_»-2j0g GAMMA- 1 j 3 ££TA = A. 00 X/H= 0* Y7H=-0*37 i/H* 0« ETA* 0*25
tW*Ll -3.3021 -3. 1864 -3.9Q52 -3«264fl -3.5778 - 0*05 7 3 0* 0 564
. Ill * L I -0*3436 -0*3433 -5.1365 -0*3*35 -5**537 -0.0403 0*0003
(#»DI -5*7067 -5*i4t»Z. -0*3*32 -5**537 -0*3435 -0*2530 0*3070
<U*D) 0.6783 U1S04 4*fa9L6 1*0642 ..o/fla. - 0*36 / 9 0*3252
Oil.* JaQO. GAMMA" 2*6. £EJA= **0Q A/H= Q. Y/H=-Q*37 Z/H- 0* * ETA" 0*25
<W*L)
-3*3021
-3*1884
-Q.Q57A
ItttLl..
0.3*38
0*3431
-4*6447
0*1435
-4*9641
0.0003
-0*0003
(**01
-5*2192
-4*6549
0*1412
—4 *.9641
0.3*35
-0*2561
0*1002
. 7U«D»
1*2*34
1*9045
4*d916
1 *41 2 1
4.67Q*
-Q *1488 -
0*2023
—2 — .. .
- —
—
— -
_■ ,<#1411*40.
.... 4AHMA- 1*5
ZEIA-L 4*00. K/tt?
Q* YY.H--fl.37
1/ H* Q*
ETA- 0*25
(W*L I
-2.9564
-2*8390
-3.4925
-2*8973
-5*0868
-0.0691
(U.Li
1.6423
1*6393
-3.6925
1*6408
-3*9151
0*0015
-0*0015
tw.01
-4.1733
-3*6028
1.6393
-3.9151
1.6408
-0*2582
0*1123
TCudj
1*9711
2*48*6
4*2471
2*2506
4.2255
-9*2796
. 0*2119
--
.... ._ .. .
CHI ■30*00
GAMMA" 1*5
ZETA- 4*00 X /H -
0* Y /H-— 0* 3 /
Z/H- 0*
ETA" 9*25
1 W * L 1 “
-2.0181
— 1 * 88 78
-2.3994
-1.9525
-3*9383
-0*0456
0*0667
roTiTl
2*8328
2*8257
-2.4634
2*8293
-2*7883
0*0035
-0*0016
IW*DI
-3*0486
-2*6737
2.8257
-2*7883
2*8293
-0*260.4
0*3146
10*0 J
2.0943
2* *704
2.9972
2*2996
2t?734
... -0*2051 _
_ 0*1708
CHI •Aft.00 GAMMA* 1*5 ZETA- **00 X/H^ 0 * V/H= -0 .3/ 2./ H- 0. £TA= 0 *25
<W*L>
-0.9037
-0*7461
-0.9548
-0.8244
-2*4446
- 0 » 0 794
0,0/82
ruvri —
3.2635
3.2487
-1,8200
3*2562
-2*1455
0*0073
-Q.OC75
(w*bt
-2*4064
-1.8302
3.2486
-2*1455
3*2562
-0.2609
0*3152
<U*D1
1.6730
1.9254
1*3702
1.8116
1*3422
-0.1316
8*U3fl
- —
—
-
- -■
CHt»60.00
AaMMA- 1*5
5
4.00
X/H«= 0. Y/H— f.37
Z/H* 0.
ETA- 0*25
.. .
<**U
-0.1773
0.03 n
0.4166
-0*0690
-1*0248
-0*1063
0*1067
tutu
2*9264
2.8923
—1.6719
2*909.1
-1*9955
0*0162
-0*01/4
< W*D1
-2*2345
-1.6822
2*8921
-1*9955
2*9097
-0.25 90
0*5155
(U.DI
1.0808
1.2149
0.0125
1.1539
-0.0230
-0*0761
... 0*0590
CHI-73.00
GAMMA* 1*3
ZETA-
4*00
X/H- 0* Y/H— 0*37
Z/H- 0*
ETA- 0*25
«w#Vf
— 0 * 2974
0.0579
1 .3958
-0*1183
0.0193
-0*1791
0*1262.
<U*LJ
2*3097
2 1 20 12
. -1*7281
2*2568
-2*0412
0*0529
^0
*0566
|W*DLj.
-J*28 97
41*2384
_ ...2*2005
-2*0412
2*2568
-0*2484
6.3628
IU*01
0*5334
0.5520
-0.3887
0*5462
-0.4319
-0*0127
0
|*0O46
— —
. — f-
■4
CMI-90.00
GAMMA ■ 1«J..
ZET A =
4 * 00
X/H* 0* Y/H- -5 *27
Z/H- 0*
ETA- 4*25 ...
—
IW*L)
-1.0254
-0.3485
1.9553
-0*6845
0*6645
-0.5409
H»*kl
2*1326
1.7039
-1.8931
1*9557
“1*9557
0*1969
-8*2*1%
< W»DI
-2*1326
—1 • 7039
1.6931
-1*9557
1*9557
-.0*1969
iaia
KMM
-0.0000
0.0000
0.0000
_-Oi
Qj
- 0*0400
1
«MIL
186
TABLE 28.- Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND 77 = 0.25
(g) y/H = 0
s
Correction factors for correcting from a wind tunnel which is
-
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free oir
— i 1 — ■ — " • t ■ ■ » ■-■■■ —
to ground effect
ouji-3*ou
GAMMA* 1*5
2ETA* 4*UU
XVH* 0* X/ H* U*
O*
ETA* 0*25
l*fL)
33. *112
-26.6127
-n.j|f 1
q _ ui)lC(
(UtLl
<U*DI
-1.4938
-1*4914
-30*1719
1*1237
-30*1460
-1*4912
UtAjOe
-1*6924
-31*1287
0.2286
-SI *128 7
-1*6926
13*2863
-0*0012
-Q.89»9
-1*0597
0*0012
0*95*6
0*9941
CHI* 3f 00
GAMMA* 1*5
jtilAf X/H-
.0.6 Y/H- 0*
1/H- 0*
ETA- 0*25
IWtLl
-24*9264
riit2»77
26*7616
-26.6127
2 3.42 74
0*3160
tu.kl
1.4936
1*6914
- “28,/'592
1*6912
1*692.6
-29*7359_
— . 3*4184
_ -29*7359
0*0012
-0*0012-
IMiOl
-30*6444
<0*01
2*^444
4*3121
13*42.0,6
13.2883
—0* 9106
-Q.94PQ
-0*9-707
CHI - 15*00 GAMMA- 1.5 2ETA- 4.QQ X/H» fl
iMtLl
-24*0943
-23*44112
16.4024
-23*7704
l a 3P41
IVfkl
1*1652
7*75X7
-.23*6102
7*7565
-24*6062 -
7*87 34
-26*6062
7*7505
0 j- £ -
0*0047
-0*9299
- -0*7553
0*3247 -
“0*0068
-.ULftfil....
-25*5342
-23.6161
7* 2 517
IMiPl
2*0481
8*5523
11*0617 _
0*9901
0*7049
CHI»3Q,QQ. 6AHHA? 1*5 1ETA* 4*QQ X/H- 0* Y/H- Q* 1/ H* Q*
IMiU
—17*0709
-14*3522.
9.QBQ0
-16.71 1 3
(UtVl
.... ... IMiOl
tOtDI
11*7904
-17*4742
... *t39#g
11 • 7582
-13.7343
9.4384
-15*7263
11*7562
5*5333
11*7744
-16*7364
0*9347
-16.7364
11*7744
5. 389?
0*0140
-0*9418
—0,0162
1*0024
r —
CHI *45*00
GAMMA-. 1*5
1 ETA =
4, DO
X/H? Jh_ Y/H- 0*
2 / H« 0 *
ETA- 0*25
— I
-9*9716
-9*1216
6*6262
-9.5493
3.8756
IVfLl
11*1444
A1*0 982
-9*4699
11*1315
-10*4761
-0*0329
n 6277
-0,0332
lliHI _
-11*4141
-9*4758
11*0962
-10.4761
11.1315
-0*9400
1*0003
- <0»PI
4*3171
6.9705
0*4926
6*6564
0.3277
— -
. .
—
CHI >60.00
GAMMA- 1*5
2ETA-
4*00
X/H- 0* Y/H> 0*
i/H- 0, .
ETA- 0*25 ......
IMiki
-5*411*
--4*6661
—6*3. 127
” -5.JJ521
3.4831
a
<u,u .
8*0479
7*9198
-5*8709
7*9943
-4*8520
0*0717
-0*074*
lUt&l
-2*JA4A
-5*8769
.. 7*9197
-6*8520
7*9943. _
- -0 *9140 —
i-UtQl
3*4437
3*7X39
t!*562 7
3.5920
-1 . 7507
• 6 . 1 **1
0*97 52
O.lllQ
—
CH { ■ 75*00 GAMMA* X .5 .
2ETA-
4*00
£ZH- Q* Y./H= 0*
U H« 0 *
ETA- 0*2.5
. - -4,7651
-3*0642
_6j2825
-3*9214
3*8044
-0*6424
_ <U.U
5*4322
3*0140
-4,0926
3,2246
-4*9848
0*2074
-4*2147
IlifcL _
-5*«144
-4,0988
5,0136
-4,9846
5 * 2244
-0* 8274
1*3438
1*3062
-1*0135 _
1.33J72
-1*19*3
0*01 34
— r -
. .. z~ri — *-
Oil >90*00.
_ GAMMA- 1*5
1£IA-
. 4 *00
A/R-J3* Y/H> 0*
A/H* 0 *
ETA* 0*25 _
ltlU
— . -5*0741
-2*5720
6*0368
-3.6197
3.8197
- 1*2443
1*24Z2_
w*u
4*4Q81
3*1701
-3*1639
3,6197
-3*6197
0*5844
-0*4496
IMiDJ
— 4»4Q81
-3*170.1
3+14*0
— -3*6197
3 . 8197
(U*D )
- 0.0000
0*0000
- 0*0000
0*0000
- 0.0000
- 0*0000
0*4494
0*0000
L-1549
l- 15^9
187
TABLE 29
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.60, AND i) = 1.00
(a) z/H - -0.20
Correction factors for correcting from a wind tunnel which Is
closed
closed floor
open
closed
closed
or bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
. Y/H*
-0.6340
-0.0337
0.9092
Z/H--0.20
-0.T859
ETA- 1.00
0. 898 7
-0.0551
-0,9036
-0*
-0.9036
-0.0551 I
0. 3910 \
0.0225
0. 1821
-1 . 1463
CHU1S.M
ZETA- Q. A Q
uai
0*1102
- 0*3642
>n.TO?A
0.3537
-0.8279
0*8320
UU U
UUU.-
IMjIlL
UJ T P1
-J*Si42_
0.096V
0.0024
-0*527 i
0.60 R/H* 0.
Q*Z592
0.5797
-0. 6893
0.7862 _
Y/H=
__2*o£ii
-0.2735
0.1355
0*8267 .
ueiiSL.
0.0910
0.1082
Q*643 l
Z/H=-0 . 20 ETA= 1.00
-0*8819..
0.2456
-0.6946
0.2 382_ _
.. P.3 5ZI ...
-0,6946
0.2456
-Jl, 3C94
-0. 1154
C . 3304
-0. 9413
Z/H--0.20 E T A = 1.C0
-0.4445
0. 3464
-0.4455
0.2594
C , I4PQ
-C.4455
0.1464
0. 1273
-1.V09J
-0.2499
0.4479
-C,r?66.
;v l
CHI -45*00 KAMUs 1.3 -XETA- 0*60
Z/H = -0. 20 ET A = 1.00
- 0.0211
-0.C031
0. 6741
cafe
M* 1-5
ZETA- 0*60
X/H- 0. Y/H- 0.
Z/H--0.20
ET A- 1.00
mmR
0*3537
. .2.4867
-0.7P59
0.6880
-1.0574
1.1395
m+*
tuiliT
0.0762
-0. 5395
0.0551
-0.8627
-0.0225
0.0211
-fl-1284
-0.9105
0.0337
-0. °627
0.0551
0.2343
-Q. 0478 .
UUU
-KfT55
0*7467
Q.902 2__ .
0.0996. __
Q> 39 1 0 .
-1.0749
- Ot 647.1
1.1553
0.1081
-0. 1333
0.5934
-U2Q37
0.2333
-0.2439
0.5268
uuu
-1*4071
1*0438
1*7321
-0.2357
Q.093O
- 1 . 1666
1 .2795
UUU
IU.D1
-0.1238
JU5159
-0*4568
0*6944
-0*6445
0*6369
0.3936
-0. 1C 34
0.4PU3
0.3010
-0.2672
0- 1805
-0.2672
0. 3C 10
-0.0112
-C.4243
0.58J2
-0.6373
0.3935
-0*3773.
0. 4564
A —
C£!i-&0. 00
GAMMA* 1*5
ZETA-
0.60
X/H- 0. Y/H-
0. Z/H--0 . 20
E T A= 1.00
i»»n
-1*349?
1*2420
1*7343
-0* 12P5
.... 0*0954-
-0.1737
0.2044
-0.0527
-1 2207
1.3705
... JiWJi_ _
-0*4549
0.5785
-0*3527
0. 806 1
-0.7324
0.4598
,0.6393 —
±m
0.2044
-0*1737
Q.0929
-0.6593
0.7522
0.6017
-0. 5557
0.3669
CHI. 73. 00
GAMMA. 1*5
ZETA-
0.60
X/H - 0. Y/H-
0. Z/H--Q.20
ETA = l/oQ
—
uuu
-1.339?
1*3580
. _ 1*7574
-O.J12 94
_Q*0569
-1-2398
1 .4571
UUU-
UUQlL
1
^0*8244
^ tuasia
.
0.9860
-0.9425
0 . 2*41
0.8829
-0.7919
J3-2155
0.1325
-0. 1269
0*0.359
-0.1269
0.1325
-0*03 1 1
-0.9569
0*9787
-Q.2T51
0*8535 _
.. -0*8156
_
*MTA7
l,kjna
1 -77A4
-0.0973
0*0973
- 1 . 2209
1.5173
rtiuu
*1* 1820
1*2493
1.1734
0*0973
-0.Q973
_ -1*2795
_ x*i&2g. :
■■ U»Ol
UU83 -
f 1*2619
_ -1*2122
-0* D973
0*0973
__ 1*2655
-1*1646
— aum,
-*<1*0000
0*0000
0*0000
=0*
_JQ_*
-Q.flflQQ
lUOOOfi
188
TABLE 29.- Concluded
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 0.60, AND V - 100
(b) z/H =0.20
Correction factors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00 GAMMA- 1.5 ZETA- 0.60 X/H* 0.
Z/H* 0.20 ETA* 1.00
(H.t)
1U»L)
(W t D)
iu,o)
-4.5097 3.0847 5.5675 “ ’ -0.469B 0.5241 -4.0399 4.1546
0.0693 -0.1234 -0.2415 -0.0276 -0.5585 C.0969 -0.0955
- 0.3091 -0.5922 0.0678 -0.5585 -0.0276 (.2475 -0.0336
-2.6866 2.2013 2.2501 0.0125 0.2335 -2.6991 2.ie3?
CHI- 3.00 GAMMA- 1.5 ZETA* 0.60 X/H* 0.
Y/H* 0. Z/H* 0 . 20 ETA* 1.00
( U* L ) -4.5097
(U,L) -0.0693
IU.01 -0.0739
(U t O) -2.5510
3.6847
5.3953
-0.4698
0.4218
-4.0399
1546
0.1234
-0.0057
0.0276
-P .5341
-C.0969
0.0958
-0.7693
-0.0678
-0.5341
0.0276
0.4602
-0.2352
2.2165
2.2501
0.0636
0.2335
-2.6146
2. 1529
CHI-15.00
GAMMA- 1.5
ZET A= 0.60 X/H* 0.
Y/H* 0.
Z /H= 0-20
ETA* 1.09
(Mill
-4.4931
3. 7543
5.1162
-0.4285
0.2552
-4.0647
4 . 1 32£
1U.ll
-0.3643
0.6155
0.4529
0.1287
-0.4507
-0.4930
0.4869
1 M. 01
0.4 140
- 1. 0775
-0.3566
-0.4507
0. 1237
0.3647
-0. 6268
1U.01
-2.3028
2.1991
2.2009
0. 1347
0.1998
-2.4375
2.0644
CHI-30.00
GAMMA- 1.5
ZETA* 0.60 X/H- 0.
Y/H- O.
Z/H* 0.20
ETA* 1.00
(W.L)
iUs L )
i u r m
-4.4534
-0.8291
LQ517
3,9452
1.2278
- J « 4 4 7j6
4,9048
1.1201
-0.8120
-P.3191
0,2063
-D . 320 7
0.1293
-0.3207
0.2063
-4.1343
-1.C354
1.3724
4.2643
1.0215
-1. 1271
(U.Dl
-2.0357
2.0791
2.0507
0.1589
0.1112
-2.1946
1 .9202
CHL-45.00
GAMMA- 1.5
ZETA* 0.60 X/H* 0*
Y/H- 0.
~ Z/H* 0.20
ETA* 1.00
tM.L)
-4,4181
4.1825
4.8285
-0.1947
0.0811
-4.2235
4.3772
(U,L 1
-1,4628
1.8561
1.7892
0.2093
-0.2006
- 1.6722
1.6462
(U.Dl
1 . 727?
— 1 .8967
^i.4ij_i
-0.2086
0.2093
1-73DR
- 1,6831
1U>D)
-1.7771
1.8422
1.8094
0. 1252
0.0199
-1.9023
1. 717C
CHI-60.00
GAMMA- 1*5 ZETA*
0.60 X/H* 0.
Y/H* 0,
Z/H* 0.20
ETA* 1.C0
--
IW.L1
-4.4038
4,3832
4 . 835 1
-0.1091
C.0742
-4.2947
4.4923
(U.L)
-2.2758
2,5488
2.5128
0.1588
-0.1377
-2.4346
2.390C
(U.Dl
2-4519
-2.5QT6
-2.2304
-0. 1377
r . 1538
2.5P96
-2.3639
lit *11)
-1.4328
1.4 700
1.4498
0.0707
-0.0230
-1 ,5035
1.3993
CHI-75* 00
GAhMA- Ul. ZE IA*
0.60 X/H* 0.
Y/H* 0.
Z/H* 0.20
ETA* 1.00
-
UUL1
4.5121
4.8696
-0.079Q
0.0762
-4.3206
4.59L2
IU*LI
-3.2306
3,366 1
3.3458
0. 1050
-0.0999
-3.3356
J.«.2fcLl
(U.Dl
3-2931
-3.3100
0.9019
-3.1847
-0.0999
0. 1050
3.3930
-3.2101
_1U*0J L^...
— ■ - +~
-0.6859
0.8955
0.0266
-0.0233
-0.9125
0.^753
chi«?o*oq
... .GAMMA- 1.5
ZETA* 0.60 X/H*
0. Y/H* 0.
Z/H* 0.20
ETA* 1.00
'
(U.L)
-4.3925
4.5837
4.8988
-0.0765
0.0765
-4.3160
4.6601
(U.U
-4*3045
4.3776
4.3641
0.0765
-0.0765
-4.3810
4 ,_30J 1
(U.Dl
4.3182
-4.3650
-4.3252
-0.0765
0.0765
4.3947
-4.2885
IUcDI ...
-o.oooo
O.OOOC
0.0000
-0.0000
0.0000
-0,0000
... . 0.Q0QQ
L-1549
189
TABLE 30
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR > = 1.5, ? = 0.70, AND tj = 1.00
(a) z/H = -0.20
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
_
open
floor
only
closed
closed
on bottom
only
to free air
' t- 1
to grour
id effect
CHI—3.00
GAMMA* 1.5
ZETA-
0.70
X/H* 0.
Y/H=
6.
Z/H— 0.20
CTA = I.OO”
- - '
UUJU
-0.71Q9
2.3517
-1* 1231
U ?T7?
f U*L 1
tM, 01
-0.0741
-U1479
-Q .7 10 1
-Q. 0854
-1.2733
-1.0564
-0.0745
TU73I6
-0.03C2
- 1.2876
- 1. 2276
-0.0802
C. 006 1
0.1397
Q.4 122
-0*0052
0.014?
-0,6900
0. 315C
CHI* 3.00
GAMMA- 1.5
Z£ TA*
0.70
X/H* 0.
Y/H =
0.
Z/H— 0 .20
ETA= 1.00
.
—
IU.L1
-U49I1
-0.7109
2 .0 1 18
-0.979e
0.0745
0.7316
-0. 3680
0.4122
fu.u
IN.D)
HUM.
0.Q74 1
-1.073*
-0. *989
0.0854
-1.2259
0.0802
-1.2290
0.1412
-1. 2290
0.0802
0.5594
-0.006 !
0. 1555
-O. 64n?
0.0052
0.0032
' • • - - - * - -
ZE TA*
0.70
X/H= 0.
Y/H=
0 .
Z/H=-0.20
E T A = 1.00
—
.-HULL..,.
tu.u
MUD)
IU.01
-0*5477
1.4776
-0.9686
0.5C10
-0.3753
0.4210
0.3232
-0.B01 1
—0^1 92 6
0.3824
-1.0019
0.5971
-0, 7040
0.3253
J2. 6.10.1 .....
0.3552
-0.9842
-0 . 3432
-0.9842
0. 5552
0.4364
-0.0320
0. 1231
-0.5358
0.0271
-0.D177
0.254 1
CHI-30.00
_ 1 W.L 1
1 GAMA* 1.5
- 1 . 620 a
ZETA- 0.70
=0.1/26
"x7h-~o^
Y/H* 0.
Z/H— 0.20
-0. 6222
ET A= U00
( U«L)
IM.D1
lil.DI
0.4221
-0-4084
^0,Q51A
0.5544
-0.6693
. - O.STM
-0.3129
0-4266
0.3526
0.4938
-0.6240
- Q.3692
-0, 6240
0.4938
0.1 736
-0.0718
0.2156
0.0605
-0. 0453
t .
... . ;
(U.LI
GAMMA* 1-5
— 1U7613
ZETA* 0.70
. . ... 0 . L742
X/H» 0.
Y/H* 0.
1 . 0252
Z/H— 0.?^
OTA* 1.00
0.1293
-O . 4 3 7 R
(U»L1
iw .01
UUU
0-2919
-0.1180
-0.0645
0.53 IQ
-0.4534
Q-J *2 i_Q_
-Q.Q292
0.3002
0.162 1
0.4225
-0.3715
-0.3715
0.4225
-0.0207
-0.1306
0.2535
~°t JIB 1
0. 1035
-Q.081C
CHl-io. QQ
— u*li
ga^mX-us
-!U6636_
zeta- d.re
0.-39.41
X /H* 0.
Y/H- W
1.0L51 .
/ Z/H*- 0.20
— -fl- 1774
ETA*! UOb
0.1299
-0.486 1
1 U»L 1
IU.D]
— xium -
D.U59Z 0-4656
0-0673 -0.3820
-IU 112 0.2558
0.1396
0.072B
0.09S5
0.2843
-0.2414
0-1295 .
-0.2414
0.2843
-Q.075 1
-0.2252
0-3087 .
-D. 2207
wiiLJa
0.1812
-0.1406
■ ' - '
CHW5-00
tH*ll
GAMMA* US
-fl.65%n
ZETA* 0.70
Q-SIAO
X/H* 0.
Y/H- 0-
-J.0261
Z/H— 0.20
-n „ 1 ^Rn
ET A = 1.00
0.1
—
(U*U
UUW--
tu.oi
-0.1865
0.2l9i
-0-0721
0.4627
-0.4191
JL- 1238
0.2595
-0. 1690
0-0659
0.184 1
-0. 1765
0.0471
-0.1765
0.1841
-0.0435
-cl 3706 ~
0.3957
-—0—11 93 w
Q-A542
Q. 2786
-^8*2426 ....
Q-P767
CHl*90.00 )
- - -
' i- -
”* 8 AIIMA* 1.S
ZETA* 0.70
X/H- oT
Y/H* D-
Z/H— 0.20
El A* 1 * QQ
— ~r —
tM> L )
_ -n.Akik
0.5873
I.03RD
-0_ 1353
0. 1353
■ IU*L 1
v
-0.3940
0-3803
-o.onon
0-5258
0.3819
0.1353
-Q. 1353
— U-m Jtua 1 _
-0.5292
pi 3906
-P.AGj2
~ Q • S 38k .
Q^QQQQ
—
0.4208
fl.QQQQ
-0.1353
.. 0.0000
Q. 1353
Q-5155
- 0.0000
190
TABLE 30. - Concluded
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR V = 1.5, C - 0.70, AND n* 1-00
(b) z/H = 0.20
0. 2752
-0 - 0 5 1 i _
-0.7770
0.5666
2.3130
-0*4142
-0.0203
0.7115
-0.6156
-0.0357
-0.7339
0.017 1
C . 6857
-0.7339
-0.0357
0.3067
CH1»I5.00
GAMMA- 1.5
ZETA-
0.70
X/H«
0.
Y/H* 0.
Z/H- 0.20
E T A = 1.00
(Wf L 1
(U«L1
f u ni
-1.3972
0.0828
-0.2402
0.3426
0.2466
-0.7363
1.8515
-0.1569
0. OP 74
-0.5631
0.1670
-0.5938
0.3331
-C. 5938
0.1670
-0.334 1
-0.034?
0.35 36
O.0796
-C. 1425
1 N « V J
1U,0)
-0.6027
0.6522
0.6692
0.1759
0.26 30
-C.7787
0 . 4763
CHI-30.00
. GAMMA- 1,5
ZETA-
0.70
X/H-
0.
Y/H* 0.
Z/H^ 0.20
ET A= 1-00
(Hall
IU.L1
ru n i
-1,2956
0.0849
0.0147
0.5294
0.4442
-0.64B2
1.6239
0.0976
0.0953
-0.4228
0.2698
-0.4253
0.1736
-0.4253
0.269C
-0.3729
-0. 1P49
0.4400
0.9522
0.1744
-0.2229
J1UE1 —
(U.01
-0,4380
0,6289
0.5594
0. 2033
0.1439
-C.6463 '
r.Hl-45.00
gamma- 1.5
ZETA-
0.70
X/H-
0.
Y/H= 0.
Z/H= 0.20
ET A= 1-00
Uf*U
-1.1934
0.7677
“"1.5293
-0.2606
C . 1090
-0.2734
-C.9320
-0.3223
0.3022
(U.L1
-0,0457
0.2584
0.5738
-0.5973
0.3376
-0.0265
0. 2767
-0.2784
0^2767
0.5367
-0.3189
LMtP 1 —
IU, 0)
-0.3578
0.5315
0.4330
0. 1655
0.0276
-0 .5233
0.3660
r_m »60.00 GAM MA- 1,5 ZETA- 0.70 X/H* o, Y/H>
IM.L1 - 1.1439~ 0.9790 " T7T2 0 7
IU.H ' -0 -307 3 0.6918 Q.5502
If H= 0,20 CT 1.00
-0.1 46S
0.21 18
GiiCT-T.
L-1^9
191
192
TABLE 31.- Concluded
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, = 0.80, AND x\ = 1.00
(b) z/H = 0.20
a
Correction factors for correcting from
a wind tunnel
which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free olr
to ground effect
” CHI— 3. 00
GA
NNA- 1.5 ZETA
- 0* 00 X/H =
—
0. Y/H = 0.
—
Z/H= 0.20
—
ETA= 1.00
r — i 11 ■ 1
ItffH
-1.1368
-0.3695
1 .9407
-0.7746
0.8614
-0.3622
0.4051
lUmLl
-Q.Q384
-0.0497
-0.6429
-0.0443
-0.9258
0.0059
-O^QQSI
iy.Pl
-0.7305
-0.9422
-0.0309
-0.9258
-0.0443
0. 1954
-0.0164
__ (11*01
—
-0. 6278
0.3271
0.5597
0,0220
0.3873
-0.6498
CHI- 3.00
GANNA- 1.5 ZETA
* 0.80 X /H —
0. Y/H= 0.
Z/H= 0.20
£T A= 1.00
r
IW,L>
-1.1368
-0.3695
1.7437
-0.7746
0 . 69 7 1
-C. 3522
0.4051
tU*L 1
0.0384
0.0497
-0.5043
0.0443
-0 . 8P54
-0.0059
0. 0053
IM.DJ
-0.6735
-0.9141
0.0389
-0.8854
0.0443
0.2117
-0.0287
(U.D)
-0.4927
0.3888
0.5597
0. 1030
0.3873
-0.5965
0.2850
CHl-15.00 6 WU«L5 ZETA* 0.80 X/H* 0. Y/H* 0. Z/H= 0.20 E T A = 1.00
(W.L)
-1.0803
-0.2962
1.4205
-0.7 104
0.4300
-0.3699
0.4 142
IU,U
0. 1773
0.2355
-0.4198
0.2031
-0.7512
-0.0307
0.0275
1W.D)
-0.5109
-0.8021
0.1799
-0.7512
0.20M
C. 2402
-0.C5O9
IUiO)
-0.2792
0.4674
0.5078
0.2207
0.3324
-0.4999
0.2467
CHI- 30*00
GANNA- 1.5
ZETA- 0.80 X/H* 0.
Y/H= 0.
Z/H= 0.20 .
El A= 1.00
*
IN. LI
CUfU
CM.Dl
-0.9322
0.2693
-0.2694
-0.0937
0.4005
-0.6196
1. 1634
-0. 1781
0.2753
-0.5376
0. 3387
-0.5414
0.2235
-0.54 14
0. 3387
-0. 3946
-C. 0694
0.2720
0.4439
0.C£ 18
-G.C782
(U, 01
-0. 1342
0.4687
0.3734
0.5622
0. 1712
-0.3964
0.2C64
CHI -45.00
GANNA- 1.5
ZETA- 0.80 X/H*
0. Y/H = 0.
Z/H* 0.20
ETA* 1.00
( W.L )
(U*L1
-0.7710
0.2233
-0.0489
0. 1625
0.4636
-0.4687
1.0507
0.0393
0.2346
-0.3346
0. 3509
-0. 3564
0.1407
-0.3564
0.3509
-0.4372
-0.1277
0.3075
0.4972
0.1127
-0.1123
(U, D 1
-0.0953
0.3808
0.2280
0.2100
0.0383
-0.3053
0. 1700
CHI-60. 00
GANNA- 1.5
ZETA- 0.80 X/H= 0,
Y/H* 0.
Z/H* 0.20
ETA* 1.00
(W*L1_ _
-0.6823
0,3869
1.0298
-0.1039
0. 1273
-0.4934
0.5750
IU. L 1
0.0463
0.4650
0.2017
0.2710
-0.2361
-0.2247
0. 194 0
iw.oi
0. 1224
-0.4022
0.0671
-0.236 1
0.2710
0.3585
-0.1661
(U.D)
-0.0982
0.2552
0.1376
0. 1203
-0.0459
-0.2185
0. 1349
CHI-75.00 GAMNA- 1.5 ZITA- 0.80 X/H* 0. Y/H= 0. Z/H= 0.20 ETA* 1.00
(N.L)
-0,6731
0.5362
1. 0469
-O. 1 356
0 . 1 30 4
-0.5375
0.671P
(Util
-ft.1990
0,4907
0. 3295
0. 1801
-0.1711
-0.3791
0.3107
UtiP)
sum 5_
-0,4343
-0. 1655
-0. 171 1
0.1801
0.4421
-0.2632
(U.D) .
-0.0769
0.1313
0.0875
0.0456
-0.0395
-0. 1224
0. 0858
CHI- 90.00
GANNA- 1,5
ZETA* 0.80
X/H=* 0. Y/H- 0.
11 H* 0.20
ETA* 1.00
-----
1 M.l 1
.-0.6704
0.6323
1.0719-
. -0,1.310
0.1310
-0.5394
0.7633
III.LI
-CLA21Q
Q *57.10
0, 46_L2 ....
0.13J0 ...
-0.1310
-0.5520
Q.44QQ
|y T ni
_ 0-4348
-0. 5584
-0.4224
-0. 1310
0. 1 310
0.5650
-0.4274
(U.D)
-0.0000
0.0000
0.0000
-D ,QQQ_Q
0.0000
-0.0000
Q.JJJJQQ
13S
193
TABLE 32
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 1-00, V= 100
(a) z/H = -0.20
Correction foctors for correcting from a wind tunnel which Is
close d
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CHI — 3.00
GAMMA* 1.5
ZETA- 1.00 X/H-
0. Y/H= 0.
Z/H--0.2C
ETA- l.rn
_ 11UL1
tL.7545
-2.5765
1.8118
- 2 . 6 7 C 3
i . 0' 1 : ’9
-0 . C "42
0. 0939
(U.Ll
-0.2012
-0.2024
-2. CP 24
-0.2019
-’.0346
0.0007
-0. 0004
4W.O)
-2.9635
-3.0C24
-0.201 1
-3.0346
-C .20 1?
C.C^l 1
0. C 322
uuni
-0.4517
0. 1018
1.3611
-0.C524
1 . 3“ 7 5
-C. 199*1
C. 1542
CHI- 3,00 GAMMA* 1-5
ZE T A = 1.00 X/H- 0.
Y/H = 0.
Z/H = -0.20 E.T A = 1.0C
(U.L)
-2.7545
-2.5765
3.0130
-2.6703
(U.Ll
0-2012
0.2024
-2.7397
0.201?
(tf.DI
-2.8222
-2.8640
0.201 1
-2.0955
(U.D1
-0.0250
0.4758
1.3611
0.3361
2. *133
-?.r?55
".20 1 ?
1.32T3
-P.0242
-o. cocr
0.0733
-0. 36 n
0 .0939
G. C00»*
C . 03 1 9
Q, 13?T
CHI-15.00 GAMMA- 1.5 ZETA- 1.00 X/H* 0. Y/H= C.
<y.L 1 -2.3*13 -2. 16Q2 1.7919
1 U.L 1 0.8731 0.8792 -2.111*0
(U.0) -2. 198*1 -2.2452 0.8725
IU.D1 0.5399 0.9451 1.0387
Z/H=-0. 20
ETA- 1.00
-2.2568.
0.8770
1 . 1141
-C.0066
0.0966
-2.2753
-0.0C39
0.0022
-2.2753
0.9770
0.076?
0.0301
0.2326
1.0037
- 0 .23271
O. 1127
CHI-30.00
GAMMA* 1.5
ZETA- 1.00
X/H* 0.
Y/H* 0.
Z/M — 0.20
ETA* 1 . C 0
(W.L)
-1.4748
-1.2742
1.0518
- 1 . 3^0?
n .4200
-C.0947
0. 1059
(U.Ll
1 * 1528
1.166?
-1.2229
1 . 16 1C
- 1 . 7 9
-0.009(1
0.0051
(U.Ol
-1.3080
-1.3610
1.1513
- 1 . 7 *r:9
1 . 16 IP
0.C3G9
0.C27C
LU.01
0.6442
Q.948Q
0.387? __
0.964 1
C. _5C.j
-0.219?
9. 083?
CHI-45.00
GAMMA- 1.5
ZETA- 1.00
X/H- 0.
Y/H= 0.
Z / -0 . 2 0
E T \- 1.C0
1M»L1
... rO-BQ26
-0.5684
0.8768
-0 . 6?.3.Q__
0.2741
-g. 1 106
. 0. 1246
(U.Ll
0.9283
0.9563
-0.6392
0.9464
-0.ecr*5
-C.0190
0.0100
(U.Ol
-0.7227
-0.7845
0.9253
-0. B0C5
0.9464
0.0057
0.023?
IU.O)
0.4129
0.6278
-0. 0388
0.5697
-0.C31C . .
. -0.1558
CHI-60.00
GAMMA- 1.5
ZETA* 1.00 X/H =
0. Y/H= 0.
z/H— 0.20
E T A= 1.00
(y.Li
-Q.516?
-0.2201
0.8624
-0.3785.
-o. 1 383
0. 1 5°4
(U.L)
0.5822
0.6392
-0.3530
0*6197
-0.E248
-0.0375
0.C 195
(W.D)
-0.4306
-0.5095
0.5760
-0.5240
0.6197
C . 0943
O.C 154
(U.Ol
0.1866
0.3103
-0. 12?Q
0.2841
-0. 1 76C
-0.0975
0.0342
CHI-75.00
GAMMA- 1.5
ZETA*
1.00
X/H =
0. Y/H* 0.
Z /H- -0 . 20
E T A = 1.00
IK. LI
(U.Ll
(W.D)
1U.D1
. _ -8.4764
0.3134
-0.2700
0.0581
-0.0856
0.4375
-0.391G
0. 1163
0.0575
-0.2099
0.2996
-C.0560
-0. xnoi
0.4004
-0.3846
0. 1 P2P
0.2937
-0.2846
0, **004
-0*0967
-0. 1 763
-0.0870
C . 1 145
-C.04.4i_
0. 2 145
0.0371
-0.0072
0.0136
CHI-90.00
GAMMA- 1.5
ZETA*
1.00
X/H*
0. Y/H= 0.
Z/H--C1.20
ETA* 1.00
(U.Ll
(U.L)
. (M.D1
(U.01_ ...
-0.4062
0. 1247
-0.1384
-0.0000
-0.0156
0.3440
-0.3566
0.0000
0*0459
-0. 1151
0.0762
0.0000
~G *. ? ? 4 7 _
0.2947
-0. 2947
0,0000.
0.2947 .
-0. 1914
0.2791
-0.2947
C.2947
-0.C0QC
-0.1701
0. 156 3
-o.ccon
0.0493
-0.0619
0. OOOC
194
TABLE 32. - Concluded
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y - 1.5, { = 1.00, AND tj = 1.00
(b) z/H = 0.20
Correction foctors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
[(ground effect)
open
floor
only
to free air
r
CHI— 3.00
1
GAMMA* 1.5
r~
ZETA-
— r
1.00 X/H= 0
Y/H= D.
IM.U
fU*L)
UUOl
- 1.264?
-0.0614
-1-2130
-0.9666
-0.0642
- 1.1338
2.0276
-1. 1209
-0.0616
tU*D)
-0.3946
0.2130
0.6231
CHI* 3.00
GAMMA- 1.5
ZETA*
1.00 X/H* 0.
. Y/H= 0.
_ 1H.U
III. L }
-1.2649
0.0614
- 1. 1492
-0.9668
0.0642
-1.2830
0.3136
1. 7739
-1.0557
IU.01
-0.2388
0 . 6231
CHI-15.00
GAMMA- 1.5
ZETA =
1.00 X/H= 0.
y/H= 0.
1U.L)
IU.U
IU.DI
-1.1807
0.2804
-0-9502
-0.8744
0. 3032
-1.0974
0.4510
1.3563
-0.8548
.0.2691
0.5505
(U.D1
-0.0045
CHI-30. 00
GAMMA* 1.5
ZETA*
1.00 X/H* 0.
Y/H= 0.
( W.L J
<M*LJ
_ t¥.Dl
-0.9528
0.4704
-0.6428
-0.6189
0.5040
-0.8052
1.0207
-0. 5467
0.4721
(U*D)
0. 1339
6.4346
0.3566
CHI-45. 00
GAMMA- 1.5
ZETA*
I. 00 X/H= o.
Y/H* 0.
IW«L 1
1U,L)
tu*oi
-0.6859
0.4800
-0.3645
0. 1280
-6. 2983
0. 5467
-0. 5449
0.3382
0.8689
-0.2698
0.4P33
0.1416 — "
CHI-60.00
GAMMA- 1.5
ZETA*
1.00 X/H= 0.
Y fit- 0.
1 W. L )
t U*L1
(W.D)
-0.5083
0.3323
-0. 1700
-0. 029 3 -
0.4629
-0.3811
""6". 0309
-0. OP 08
0. 3389
( U, D )
0.0589
6.2 355
0.0105
CHI-T5.00
GAMMA- 1.5
ZETA*
1.00 X/H= o.
Y/H* 0.
tM.L)
tU.Ll
' IH.D1
-0.4750
0. 1171
-0.0394
0.1330
0.3777
-0.3200
C • C 34 3
0.0332
C. 1 301
0.0089
iu.dj
0.0057
0^ 1006
chi - 9o.ee
GAMMA- 1.5
ZETA*
1.00 X/H= 0.
Y/H* 0.
IM.LJ
tu.u
1M.01
-0.4854
-0.0700
11.0837
0.2319
0.3566
-0.3440
6.8450”
0.1200
0.08 11
-0.0000
0.0000
0.0000
closed
closed
on bottom
only
to ground effect
- 1.1252
-0.0630
-1. 3513
c . cm 5
If H= o.
-1.1252
0.0650
-X .2932
0. 1550
If H= 0 .
-1.0372
0.2966
-l*JU 22 £
0. 3136
= 1.0C
1.2*J 7 7
- 1. 3510
-0.0630
0.5603
! . 0 1 6 **
-I .29 32
£_.Q6 30
9. 56C3
CTA = 1.00
0 . 6372
- 1 . 1C 25
0.2966
-C, 13?6
C.OC'16
C. 130?
-C.4341
-C. 1 39 6
-C.001 6
C.± 44 C_
-C. 3939
Z /H = 0.20 ETA- 1 .00
-0.7967
0. 4896
-0. °040
0. 30 11
Z/H- 0.20
ft. 3392
-0 . 3040
0.4296
" 0 . 2334 "
-C. 1434
-0. 0083
C . I52i_
-0.323?
-C. 156?
-0.0192
C . I 6 J_2
-0.247?
-0.5054
0.51Z4
-0.5 353
0 . 3 T 99
-0.2275
0.4066
-0. 3559
C. 1 ° 0 1
" . ? 1 4 5
-0.5 353
0.5 174
0.0660
0. 1922
-C. 3559
_ 0 . 4 C 66
-0.2203
-C.0743
C. I 860
-6. 1212
7 /H= 0.20 ETA* I. CO
0. 1504
-C.0C 12
0.013 1
C. 1 735
). 1534
O.C012
0. CL1CJ
0 . J 5 F 6
-0.2046
0 • ? 7 1 5
-0.257a
0.0636
n . 1964
-C.2G7C
C ±2 7 1 5
-0.0539
-C.2703
-0.1544
0.2124
Z/H* 0.20 ETA* 1.00
-0. 1973
0. 1973
-0. 1973
0. 1973
-0. 1973
0. 1973
0.0GCC
-C.2C31
-C.267J
0. 2P10
-c.oooc
C. 162 r
0.CC66
0.1778
C. 0151
- 0.0C 12
0.1035
C .207 I
0.029?
-0.0096
0.258?
0.0565
-0.02 51
0.0555
0.4292
0. 1593
-0. 1467
6 -^ 1- 1
L- 15^9
195
TABLE 33
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y= 1.5, T = 1.50, AND 1.00
(a) z/H = -0.20
Correction foctors for correcting from a wind tunnel which is
closed
closed
on bottom
! only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
• only
1
to ground effect
CHI »-3. 00 GAMWA- 1.5 ZCTA* 1.5Q X/H =
Y/H =
C.
ETA =
l . r 0
U.L)
-7.9750
-7.9295
(U.L)
-0.6703
-0.6705
U.D)
-8.B686
-8.0774
(U.D)
-0.5541
-0.2006
CHI- 3.00
GAMMA- 1.5
ZETA-
1.50 X/H *
ty.L)
-7.9750
-7.9295
(U.L)
0.6703
0.6705
U.D)
-8.4543
-B.4634
IU.D1
0.7732
1.0919
CHI *15. 00
GAMMA* 1.5
ZETA*
1.50 X/H=
- IW.L)
-6.4492
-6.4022
(U.L 1
2.7876
2.7B82
u.di
-6.3645
-6. 3740
(U.DI
2.3898
2.6459
CH I *30. 00
GAMMA- 1.5
ZE TA =
1 - 5 a X/H*
_ U.L)
-3.5802
-1.5282
1 U.L 1
3.3421
3.3435
U * D )
-3.5821
-3.5923
ILUOL . .
2.5223
~C HI -45. 00
GAMMA*” 1. 5
ZETA =
1.50 X/H*
U.L)
_ . -U 6919
-1.6293
(U.L )
2.4854
2. 4863
t W.D1
-1.9913
-2.0025
1U.D1
1-4 116
1.5452
CHI-60.00
GAMMA- 1.S
ZE TA =
1.50 X/H =
IW.L) .
-0.9605
-0,8763
(U*U
1,5534
1.560 1
U.D)
-1.2603
-1.2930
IU.D)
0,6634
0,7440
CHI-75.00
GAMMA- 1.5
ZE TA =
1.50 X/H* '
-0*8157
-0,6840
(U.L)
0.9666
1.0072
u.di
-0.9270
-0.9492
1U.D1
0.2340
0.2646
CHI-90. 00
GAMMA* 1.S
ZETA-
1.50 X/H= (
U.L)
-Q* 8282
-0.62Q6
(U.L)
0.6728
0.7284
U.D)
-0.6665
-0.74 10
— IU*D)
-Q.QQQQ
0,0000
10,0122
-8.8137
-C. 6702
3.95 77
7.1B72
-P.3980
0.6702
3.9577
3.i»869
-6.3083
2.787!
2.7822
1.5252
-3.5254
7. 340e
0.7157
1-^225
-1.9342
2.4827
-0-1618
Y/H*
1,2557
- 1.2247
1.5475
-0,48 15
1,2667
-0.0765
0. 9700
0,2274
1.2473
-0.6528
0.6139
- 0,0000
-7.9532
7.36 r'. ’
- C . P ? 1 7
0.0237
-0.6704
- n . 90 !5
0.CCC 1
-C.CCCC '
-8.7035
-0 . 67'’4
C. 034?
*0.0261
-0.29 ? 2
T . 94 >(,
-C.254?
0.0906
Z /?*= -0 . 2 0
E T \ - 1 . C "
-7.7532
6.75’^t
0.0219
0.0217
0.6704
-0.4895
-C.OCC1
0.0000
-8 . 4°95
0.67(4
C.0353
0.C262
1 .0Q3C
3.94V6
-0*2270
0,0889
Z/H=-0.20
-6,4267
ETA- 1 . 0 0
2.8776
-C • 0226
0,0245
2.7PS2
-6.40C 3
-0.0005
O.QOC1
-6.4003
2. 7QE2
0.0350
0. 0262
2.5749
2,7740
-0.185 ]
Q-Q7LS... _
Z/H--0.20
ETA- 1.C0
-3. 5553
0.94 j 6
.. -0.0250
Si 0^71
3. 3434
-3. 6104
- C . 0 C 1 3
0.0001
-3.6184
3.34 34
n . 0 36 3
0.0261
2.47CC
Q.7C67
-C. 1 325 _
-S,0524_._. .
Z/H--C.2Q
ETA- I. 00
-1,661?
C . 65. >2
-0.0300
0. 0326
2.4*00
-2.0223
-r.0027
0, 000 3
2. 4 0*0
r.0370
0.0258
1.5094
-0. 3744
-C.0977
0.0358
Z/H =-0.20
ETA-' i . )C
-0. 9203
" . 7 11 5
-0. 0402
0.C44C
1.5595
-1.3135
-b.oq£?'
0. 0006
-l.*1P5
1 . 559 >
0.038?
0.0247
0.7238
-0.494
-0.0604
0,p_202_
Z/H=-0.20
LTA= 1 . i ; f !
-0.7542
0 . 74 1 (1
-0.0615
0.0694
1.0065
-3.969?'
-C.0198
O, 0008
-0,?69E
1 . 00 6’i
0,0420
0.0206
0. 2593
-0,2451
- Q *.02 5 4
D. 005 3
Z/H--0.20
ETA = 1.00
~
-0.7435
0.7435
-C.0C47
0. 1 146
0, 7435
-0.7435
-0.0707
-0.0151
-0.7435
0. 7435
0,0569
0.0025
0.0000
-o.oooc
-r.oooo
0,0000
196
TABLE 33. - Concluded
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, \ = 1-50, AND V= 10O
(b) a/H = 0.20
Correction factors for correcting from a wind tunnel which is
closed
on bottom
only
closed floor
only
(ground effect)
to free air
to ground effect
-2. 1701
-0.1127
_r.2*511Q
-0.1675
-2.0863
- 0. 1 no
-2.5612
0.1925
2.98 27
-2,4260
-0, 1127
1 . C p 24
-2. 1 3C4
-0.1129
-2.59 21
0.C74C
-2.0863
0.1130
-2*»l5Q1
0.3874
2.5598
-2.3132
0,1127
1.0024
-2.0263
0.5363
-7.054 I
0.4042
- 1,9399
0.5382
_ -2*MZ3
0.6687
1.2606
-2.1376
0.5375
0.9377
GAMMA- 1.S ZETA =
GAMMA- W5 ZETA*
IM.L)
tU.Ll
-1.0975
1,0042
-I.Q0A9
-0.9828
1.0134
-J.Q644
1.0088
-0.9195
1 .0036 ...
-1.0433
1.0101
-1,0932
0.454 1
- 1.0932
1,0)01
(U, D )
0.50 37
0.6452
0.1938
0.6066
0.1729
CHl-60.00
GAMMA- 1.5
ZETA-
1.50
X/H = 0.
Y/H =
0.
Z /H~ C.20
ETA = 1.0C
( U, L 1
tU.Lt
(U.D)
-0.6790
0.8148
-0.6456
-0.5257
0.8352
-0.7075
0.9362
-0.5595
0.8134
-0.6068
0. "279
-0. 7343
p .3979
-0.7343
0.8279
IU.OI
0*2*91
0.3884
-0.0802
0 . 3646
- 0 . 1 C 6 4
CHI-75.00
GAMMA* 1,5
ZETA-
1.50
X/H= 0
. Y/H=
0 .
Z f\\~ 0.20
CT A- 1.00
1 WftL )
-0.5318
-0.2977
0.9300
-0.4236
0 . 4043
tu.o
(U.D)
0.5228
-0.4351
0.5789
-0.51 16
-0.3550
0.5185
0. 5605
-0.53C8
0.5605
(U,0)
0. 1106
0. 1509
-0.0875
0.1410
- 0 . 1100
CHI-90.00
GAMMA- 1.5
ZETA-
1.50
X/H = 0
. Y/H=
0 .
Z/H= 0.20
ET A= 1.00
IU*L)
1U.L1
(U.D)
-0.5503
0.2986
-0.2849
-0.2020
0.4319
-0.4193
0.926 1
-0.2296
0.2785
-0.4062
0.406?
-0.4062
0.4062
-0.4062
0.4062
(U*0)
-0.0000
0.0000
0. 0000
-0.0000
0 . 0000
L- 15^9
197
TABLE 34
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5 C - 2-00, AND rj = 1 .00
(a) z/H = -0.20
Correction foctors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
r— 1
to grour
id effect
CHI — 3.00
GAMMA* 1.5
ZETA- 2.00 X/H*
0. Y/H= 0.
7/H— 0.20
EM- 1.00
- -19.4963
-19.4 795
24.12 17
-19.4882
23.5Q3Z
_ -Q.QOfll
—
_ Q.Q087
CU.Ll
-1.8711
-1.8712
-21.4284
-1.8712
-21. 4865
0.0000
-0.0000
(W,01
-21.4654
-21.4681
- 1.871 1
-21.4865
- 1 . E 7 1 2
0.021 l
0.0183
L1UD1-
-U3S5
-U0711
9.6671
-1.145?
9.4645 ..
-Q. 1896
C.Q746
CHI* 3.00
GAMMA* 1.5
ZETA-
2.00
X/H= 0. Y/H* 0.
Z/M=-0 . 2 0
E T A = 1.00
..
_ (M*L 1
-19.4963
-
19.4795
16,7534
-19.4882
16. 1456
-C .008 1
0.0087
(U.L1
1.8711
1.8712
-20.4153
1 . q 7 l 2
-20.47 3°
-n.ooop
0.0000
IM.DI
-20.4525
-
20.4554
1.8711
-20.4738
1 .87 12
0.0212
0.0183
m,oi
2.3483
2. 5864
9.6671
2.5192
9.6645
-0. 1 7C 9
0.0677
CHI-15. 00
GAUM A *" 1.5
ZETA*
2. 00
X/H= 0. Y/H* 0.
7 /H= -0 .20
EM- 1.00
- '
1M.L1
-14.7521
-
14.7347
6.3541
- 1 4 « 7 4 3 7
5.76M
-U 0084
0.0090
(U.L1
7.2970
7.2971
-14.4687
7.2771
- 14.52 75
-G. 0 0C2
-0,0000
IW.D1
-14.5061
-
14.5091
7.2967
- 14.5275
".2971
0,0214
C.01F4
I U f D 1
.6*4360
6.6269
6.0751
6.5736
4.C721
-C. 1376
0.0533
CHI *30. 0Q
GAMMA* 1.5
ZETA=
2.00
X/H* 0. Y/H= 0.
Z/H=-Q« 20
ETA- 1 . C 0
— 1M,L1 —
1. 17Q3_
-7.1530
.. 2*1458
-7.1610
1.5741
-0.C093
Q.GJGC
lU.tl
7.6729
7.6731
-7.3895
7.6732
-7.4477
-C . 0004
-0.0001
( kT.Ol
-7.4262
-7.4293
7.6722
-7.44 77
7.6732
C.0215
0.0184
tli.O)
- 5.5474-
5.6901 .
-.0.0553.
5.6505
. ... 0.8520 _
-0.1C31
0. 039.6. _
CH I *45. 00
GAMMA- 1.5
ZETA- 2.00 X/H= 0.
Y/H* 0. Z /H* -0 . 20
E TA= 1.00
(U,L ) ...
-3.1295
-3.1062
1.8180 -3.1182
_ 1.2424 .
-P.Q113
0,0121
IU * L > 5.1644 5.161*9 -3.9719 5. 1652 -4. CM3 -0.0008 -0.000?’
-4.0096 -11.0129 5. 1630 -4.0313 5. 1 552 0.0216 0.Q1G4
lU.Di 3.Q969 3.LMS.. - 1. 1313 3. IT Q Q - 1.14 12 -Q.GZ3_1_ Q.n 275
CHI-60. 00
GAMMA- 1.5
ZETA-
2.00
X/H*
0. Y/H= 0.
Z/H=-0.20
ETA = 1.00
’
tu T i i
-1-7945
t 1.7624
.1 .9686
-1*7.121 .
J_,4 >73
-0.0154
0.0166
tU.LJ
3.1108
3. 1122
-2.5755
3.1 127
-2.6749
-0.0C19
-0,0005
IW,D)
-2.6130
-2.6168
3. 1075
-2.6349
3. 1127
0.021?
o, cn r i
— iU*01_
1.4190
1.480.9
-1.QB65
.1,4648
“1,0916
CHI*75. 00
GAMMA- 1.5
ZETA-
2.00
X/H*
0. Y/H- 0.
Z/H=-0 . 20
ET A = 1.C0
1M*U_
-1.5145
-1.4804
?ni
- 1 . son?
1^4^77
(U,U
2.0058
2.0108
- 1.8867
2.0127
- 1 .9460
-C.0C6?
-0.001?
(U,D )
-1.9230
-1.9289
1.9950
-1.9460
2.C 127
0.0229
o .Din
iu f m
0.5011
__ 0.52S5
_ -0.49 14
0.5707
-0.4987
-0.0196
n nnii o
;
— u * y ^
chi * 90. oo :
GAMMA* 1.5
ZETA-
2.00
X/H*
O. Y/H= 0.
Z/H--0.20
E T A = M00
,UUW .
..... -1,5 3 A0
-1.434^
1.9937
-1.4921
1.492 1
-0.0439
0.0576
tu.u
1.4491
1.4698
-1,4345
1.4921
- 1.4921
-0.0430
-0.0222
IWaDl
- 1.4626
- 1.4824
1.3956
-1.4921
1 .492 1
0.0293
0.0096
— - 1U.D1
tQ.QPQO
0.0000
. -0,00.00
-0.
Q.
-0.0000
0.0000
198
TABLE 34. - Concluded
LATERAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, K = 2.00, AND tj = 1.00
(b) z/H = 0.20
Correction foctors for correcting from o wind tunnel which is
closed
closed floor
open
closed
closed
on bottom
open
only
floor
closed
on bottom
only
(ground effect)
only
only
to free air
to ground effect
CM [*-3,00
GAMMA- 1.5
ZETA* 2.00 X/H= 0. Y/H* 0.
Z/H- 0.20
ETA- 1.00
-3.2264
-0.1632
-3.97 36
3.5336
-3.9736
-n.1632
1.6077
-0.C 1 2 1
0.C001
C .0593
-C. 192 1
0.C 19"
-a.ocoo
2.031?
0.0726
t«,U
(U.U
tu.m
-3.2445
-0.1431
-3.9143
-3.2065 4.1340
-0.1632 -3.8391
-3.9417 -0.1631
<u,0>
-0.0097
0.2550 1.6156
6. 1P24
CHI- 3.00
GAMMA* 1.5
ZETA- 2.00 X/H- 0. Y/H* 0.
Z/H* 0 . 20
ETA- 1.00
2. 9508
-3.GC 54
0. 1632
1.6077
-C.01C1
-0.OCC1
C . 0597
-0.1771
0 . C 1 9 °
0. OOCC
0.0319
0.0654
IH.L)
(UtU
1 W.D)
IU.D1
-3.2445
0.1631
-3.7457
0.3005
-3.2065 3.5420
0.1632 -3.6701
-3.7735 0.1631
0.5389 1.6156
-3.2264
0.1632
-3.0054
0.4736
CHI-15.00
GAMMA- 1.5
ZETA- 2.00 X/H- 0. 3C/H* 0.
Z/H* 0.20
ETA- 1.00
(U.Ll
IU.L1
-3.0520
0.7817
-3.0128 2.5550
0.7822 -3.1708
-3.2 75 2 Q. 78 1.6 _ _
-3.0333
0.7821
-3.3071
1.9812
-3.3071
0.7821
-0.0127
-C.0CC4
0.0602
0.0205
0.00C 1
0. 03 1 9
lUi Ol
0.7544
0.9400 1.4470
0.8947
1 .4399
-0.1403
C. 0533
CHI-30. 00
" GAMMA- 1.5
ZETA- 2.00 X/H* 0. Y/H = 0.
Z/H= 0.20
ETA- 1.00
nuu
11ULI
-2.4924 -2.4438 1.7187
1.3625 1.3636 -2.3904
kATn -?.495fl 1.3621
-2 . 4 7 1 6
1.3633
-2,5276
1.1631
-2.5276
Lt 2*3 3 .......
-^.0207
-0.0008
_CLtD.6Q-6-
0.0220
0.0003
imljj:
IU.D)
0.9860
1.1312 0.9638
1.0913
0.956C
-0. 1 05 3
0.0399
CHI-45. 00
GAMMA- 1.5
ZETA- 2.00 X/H- 0. Y/ H- 0.
Z/H- 0.20
ETA- 1.00
IMmLl
(U.U
-1.7260
1.5630
-1,7077
-1.6732 1,2992
1,5654 -1.6310
-1.7 ILL 1.5623 ....
-1,7003
1.5647
-1.7688
0 .7590
-1.7688
1.5647
-0.0252
-C.0C1"
0.0610
0, 0276
0.0007
HI.D)
0.0663
0.9714 0-3407
0.9434
0.2314
-r.orsi
0.C221
CHI -&0. 00
GAMMA- 1.5
ZETA- 2.00 X/H* 0. Y/H* 0.
Z/H= 0.20
ETA- 1.00
tu.u
CU.Ll
-1.0473
1.33Q3
-0.9750 1.1802
1.3361 -1.0627
- 1 - 1 A 77 1.3288
-1.0129
1.3344
-1.2007
0.6576
-1.2007
1.3344
-0.0344
-0.0C4 1
0.0617
Q*03??_
0,0016
Q.0311
mi .
(U, D1
0.5375
0.6023 -0.1220
0.5851
-0. 1343
-C .0477
q 4 _o U2
CHI-75. QQ
GAMMA- 1.5
ZETA- 2.00 X/H- 0. Y/H* 0.
Z/H= 0.20
CTA= 1.00
■■■■"' -
(M.U
UljLl
-Q*T52fr
0.9036
-0.6316 1.1750
0.9223 -0.7238
0.8984
-0 ^6956
0.9175
-0.8670
0.6600
-0.8670
0,9175.
-0.0570
-0.013?
C. 0640
0.0640
o.oo4e
JJURI
1U* 01 , r .
.. . . 0.2083
0.2365 -0.1698
0.2300
-0.1071
-0.0216
0,0066
CHI -90. 00
GAMMA- 1.5
ZETA- 2.00 X/H- 0. Y/H- 0.
Z/H= 0.20
ETA- 1.00
. _a
iw*L»
IU.U
(U.D)
-0.7570
0.5993
-0.5855
-0.5352 1.1678
0.6637 -0.5265
-0.6511 0.5654
-0.6631
0.6631
-0.6631
0.6631
-0.6631
0.6631
-0.0939
-0.0639
0.0776
0.1279
0.0005
0.0121
iu*Pi
-0.0000
-0.0000 0.0000
-0.0000
0.0000
-0.0000
0. 0000
L-15^9
199
TABLE 35
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND tj = 1.00
(a) z/H = -0.20
8
Correction factors for correcting from a wind tunnel which Is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
to grour
id effect
CHI— 3.00
GAM* A* 1.5
ZETA* 4.00 X/H- 0
1 U.L 1
-680.9501
— 680. 94 94 1
(U.U
nr, di
IUlDI
-181.3685
-708.4083
-182.9465
-181.3686
-708.4084
-182.81 *3
CHI* 3.00
GAHHA- 1.5
ZETA- 4,00 X / H - 0,
JM.L 1
_ - -680.4501
-680.9494
IIUA1
181.3685
-674.6072
179.4684
181.3606 -<
-674.6073
t70.5PftA
*. T
----- * ~
turn Aw 1.5
ZETA- 4. 00 X/H* 0.
iM-iV
-159.1240
- 159. 1233
1U,L1
(JUOJ
218.7700
-166.6452
189. 117?
218.7700 -1
-166.6453 ,1
1 R9.2126
CHI-30. DO
GAHHA* 1.5
ZETA* 4.00 X/H- 0.
” t«.L 1
-31.0349
-11.Q2JU -
01.5815
-48. 1787
63.9816
-
:r:-jnuto"v
81.56)5
-48. 1786
. 63,9099.
CHI -45.00
CA8HA- 1,5 T
ZETA* 4,00 X/H* 0.
IW.LI
-13.9702 -13.9691
IU.U
1M,0>
IU,DJ
37,2543
-26.5847
,25.2533
37.2543
-26,5848
- — 25,3344
CHI-60.00
GAHHA- 1.5
ZETA- 4.00 X/H* 6 .
IM.t I
-11.0625
- 1 1,0611
tU.L)
1 W.DJ
tu.Pi
21.0283
-18.4565
10.5724
21.0283
-18.4567 ,
10,6050 _
CHI-75.00
GAHHA- 1.5
ZETA- 4. OF X/H= 0.
IUmUl
-10.4346
— . - 1 0.63 19 |
14.1141 -1
-13.8265 1
3.7QB8 . :
tU.LJ
IM.D1
tU,Pl
14. 1 140
-13.8263
3.6939
CHI-90.00
CAM HA- 1.5
ZETA- 4.00 X/H- C,
|y.l i
-10.6143
-10.6053 |
IU,L 1 "
— tM.D)
-4 IU.D1
10.5929
-10.6066
-Q.QOOO
10.5949 -l
-10.6075 1
_ .-Q» QOCD.
-6°0 . 9 50 1__
-151. 3606
-708. 4120
-182.. PS 1 5
-708.4120
-131.3686
322 . 547 4
0.0000
0.0033
-0.0951
- D. 0000
0.0032
0. 0361
Z /H=-0«20 ET A* 1.00
388.5U37
181.3685
322.i476__
19*1144
110. 7699
1U.I&49.
Q. 14 ! T
40.1722
81.5814
37.0483
8.8140
26.5793
37.2541
_-680. 950JL
181.3666'
-674. 6109
— 1Z5« 554J
387.976 3
-674.6109
181.3606
J22.5474 _
-0.0000
0.0034
- 0.0050
0.0000
0.003?
0. 0344
Z/H=-0.20 ETA- 1.00
-152. 123L __
218.7701
- 166. 64e6
1S9* 1058 __
-19,6732
- 1 66. 6486
210.7701
_ril,7fe51
-0.0000
0.0034
- 0.0635
- 0 . 0000
0.0032
0.0269
Z/H=-0.20 ETA- 1 - DO
-31_.8345
81. 5516
-48. 1820
63.9614
Z/H*-0.20
-13.9697
37.2544
-26.5801
25. 3201
-0.407 ?
-49.1820 ‘
31.5816
-37,048'*
8.2725
-26. 588 1
37.2544
-20.8257
■0. 0004
-0.0000
0.0034
-0.0515
_-Q jS _0005
- 0.000 I
0.0034
-0.03 68
0.Q0C4
-O.OCO'-
0. 0032
0. 0202
Z/H=-0.20 ETA* I.C'O
18.4501
21.0278
-9.9919
rl 1.06 18
21.0285
- 1 R . 4599
_ 10^5960
_J 0. 25_P_7
- 1 0. 4*599
21.0285
-9.992L
-0.000 7_
- 0.0002
0.0034
-0.0236
0.0 0Q 7
-0.00C1
0.0032
0.0090
Y/H= 0.
Z/H=-0. 20 ETA= 1.0C
I 1. 1138
13.9199
14.1 120
-10 t 6JJ3
14. 1146
-13,8297
3. 7D49„
10^9 15 _
-13.8297
14,1146
-C . 000 7
0.0034
- 0.0 110
- 0.0006
0.0032
o.oo?a
10.6006
10.56 12
Z/H=-0« 20
10.6103
-10.61C3
ETA= 1.00
10.6103
-10.6103
10.6103
-Q.0JQOO
-0.0175
0,0037
-Q.0000
-0.0155
Q. 0029
0. 0000
200
TABLE 35. - Concluded
VERTICAL DISTRIBUTION OF INTERFERENCE FACTORS FOR y = 1.5, C = 4.00, AND t? = 1.00
(b) z/H * 0.20
8
Correction factors for correcting from a wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
1 — i
to ground effect
CHI— 5.00
GAMMA* US
ZETA*
*.00
X/H* 0.
Y/H- 0.
Z/H= 0.20
ETA* 1.00
-0.0030
c. ooco
0 . C 736
-0.0950
(U,L)
(U,L)
— ^r.V?3T
-0.3257
-9.5807
-7. *67*
-0.3257
-9.5888
8.6066
-9.5272
-0.3257
-7.4706
-0. 3257
-9.6143
2 . 04 57
-9.6143
-C. 3257
-o.cooo
0.0255
tu.oi
0.6033
0.7354
5.72 18
0.6983
CHI* 3.00
GAMMA- 1-5V
zeta-
4.00
X/H* 0.
Y/H= 0.
Z/H* 0.20
-7.4706
0. 3257
-9.2246
EM* 1.00
6. 94*2
-^>.2246
0.3257
b". 0C32
Oft L )
UJtO
IWfDl
tU,D)
-7.1*737
0.3257
-9. 1909
1.1612
-7.467*
0.3257
-9. 1 991
7.5C41
-9. 1374
0.3257
-C.00C0
0.0336
-C..0P56
Q.O00C
0.0255
0.0335
1.2802
3.7218
1 . 2*68
3. 7202
CHI-15-00
GAUM A- 1,5
ZETA*
4.00
X/H* 0.
Y/H* 0.
Z/H= 0.20
ETA* 1.00
-7.1828
1.5918
-8.2010
5.0931
- U 20 1 0
U 5918
-0 . OC 3 1
0.0034
w.u>
IU.U
(U.0)
-7.1859
1-5918
-8.1673
-7.1794
1.5918
-8.1755
5.6403
-R . 11 37
1.5918
-C.0000
0.0337
0.0000
0.0255
0.0267
3.4547
2.0503
3.4536
-0.0689
CU*DI
1.901*
2.0770
•.
CHI* SO » 00
GAMMA* 1-5
ZETA-
4.00
X/H* 0. Y/H* 0.
If H* 0.20
ET A = 1.00
3 . 394 B
-6.6374
2.9552
2.6077
-0.0035
-C.00C1
0.0337
-0.0512
0 .0037
(MiU
tUtU
Of.DI
IU%D1
-6.2866
2.9551
-6.6037
2. *5*8
-6.279*
2.9552
-6.6119
2.5267
3.9329
-6.5499
2.9550 _
2.6090
-6 . 2831
2.9552
-6.6 374
2.5067
-0.0000
0.C255
0.0200
CHI AS- 00 GAMMA* US Z£T*- *«0Q X/H= 0. Y^H= 0.
(U.L)
(U.U
-*.6*22
3.7769
-4.9SQT
-4.6334
3.7770
-*.9589
2.9022
-4.8969
UXL6&
-4 ,8380
3.7770
-4.9 5*5_
2.372C
-4.9845
3. 7 7 7C
-0. 0C4 3
-0.00C1
0.C338
C. 0046
-0.0000
0.0255
0.0142
A Islil — ~
_ .1U.DI
2.2902
2.3415
1.3171
2.3273
1 .3 156
— 0 .0371
CHI-60.00
GAMMA- 1.5
zeta* u.oo
X/H*
0.
Y/H*
0.
Z/H* 0.20
ETA* 1.00
1M.L1
IU.L1
-3.1750
3.6773
-3.1626“
3.6776
3,5085.
2.4916
-3.4465
3,6769
-3. 1690
3.6776
-U33JU
1.9605
-3.5341
3.6776
-G. 0060
-C.0003
0.0338
0.0064
-o.oobo
0.0255 .
1.11*01
1.57*2
U 6070
-0.00 10
1. 5980
-0.0031
-0.0238
CHI-75. 00
GAMMA- 1.5
ZETA* 4.00
X/H =
0.
Y/H*
0.
Z/H* 0.20
eta= uco
. liULI
WiU
-2.106*
2.71*7
-2.5178
-2,0834
2.7159
-2.5264
2.4559
-2.4642
2^7132
-2.0954
2.7159
-2.5518
1.9394
-2.5510
2.7159
-0.0111
-0.0012
0 »0_339
0.1 0119
-0. 0000
0.0254
1M. D1 —
tu.oi
1 0.6599
0.6751
-0.4729
0.671?
-0.4766
-0.0112
0. C 03 9
CHI -90. GO
GAMMA- 1.5
ZETA* 4.00
X/H =
0.
Y/H*
0.
Z/H= 0.20
CT A* 1.00
_ AMiLl_
(U«L1
- 1.982*
1.9260
_ 1 0199
-1.9052
1.9392
- 1.9266
0.0000
2.4577
-1.8619
1.9000
-1.9488
1.9*88
-1.94DG
1.9488
-1.9480
1.9488
-C. 0336
-0.0229
0.0366
0.0*37
-0.0096
lUfP)
. -I.Tl
-0.0000
o.odoo
-0.
0.
-0.0000
0. 0000
L-15^9
1
201
TABLE 38
Hum III DISTRIBUTION OF interference factors for y = 1.5, ? - 10.00, I) ■= 1.00, AND i/H - o.»
*
Correction foctors for correcting from o wind tunnel which is
closed
closed
on bottom
only
open
closed floor
only
(ground effect)
open
floor
only
closed
closed
on bottom
only
to free air
: — i — » ~
to ground effect
CHI—J.OO 1.5 «»*- 10.00
Z/H* 0.20 E T A = 1.00
null
ssu u
<H,P>
-15.242?
■ -P.52J5
-21.593?
lU.Dl
2. **696
-15.2422
-0.521*1
-21.5968
275212
" 16-5495
-21.5569
-0. 5? 1 5
7.7043
-15.2425
-0. 5214
-21.6151
2 .5068
GJOT*« 1.5" KW* 10.M
X/H* 0.
2/H- 0.20 ETA = 1.00 _
(H*U
<U t U
1M.01
tU.OI
- 15.2429
0.5215
-20.78S6
3.2144
-15.2422
0.5214
-20.7885
15.0651
-20.7485
0.5? 15
7.7043
CHl-15. 00 6WWl» 1.5 ZETA- 10.00 X/H* 0.
l/H- 0.20 ETA 3 1-00
IM,l»
~ — 1U?L 1
(W,P1
tU* 0)
-1575056
2.6263
-18.9893
-15. 0049
2.6263
-18.9922
12.5159
- 1 6 .9523
-15.0053
2.6263
1 1.9848
-19.0105
2.6263
4.4106
4.4487
CHI* 30.00 GAHHA- 1.5 ZETA* 10.00 X/H= 0.
(W,L)
IU* L 1
(U*01
-16.2059
5.1934
-16.4260
5.1074
-14.2051
5.1934
-16.4289
5.1361
CH1-43.00 GA**A- 1.5 ZETA* 10.00 X/H-
Uf.W
IU.U
j*.ei
-12.6634
7.5216
-13.5TT3
-12.6625
7.5216
-13.5802
t.U,D»
5.0257
CH|*60.00 GAAHA-
ZE TA* 10.00
L¥.U
IUaWI
(W.0)
iUsO)
-10.0907
9.0239
-10.5636
3-9693
-10.0893
9.0239
-10.5665
3.9826
CHI *7 3.00 GAWM* 1.5
ZETA- 10,00
IM.Ll
uum
(UaDl
-6.9066
8.2600
-LJ23B
1.9796
-6.9040
8,2601
-J^ZhL
1.9861
7.3101
4.4380
7.3100
. Y/H= 0.
Z/H = 0.20
ETA= 1.00
9.9775
-16.3889
5. 1934
-14.2055
5. 1934
-16.4472
9.4500 \
-16.4472 \
5. 19 34 t
6.3167
5. 1281
6.3165
. Y/H* 0.
Z/H = 0.20
ETA= 1.00
P.0760
-13.5402
7.5215
4.5202
-12.6630
7.5216
-13. 5985
7.5S17
-13.5985
7.5216
5.0199
4.5200
Y/H* 0.
Z/H= 0.20
ETA= 1.00
" 6 .”86 73
-10.5265
9. 0238
1.6468
7j0~. 0900
9.0239
-10. 5848
3.9789
6.3458
-10.5P48
9.0239
1 . 3466
]. Y / M= 0 .
Z /H = 0.20
ETA = 1.00
6.4751
-7.7867
a._2329
-6.9053
8.260 1
-7.8450
5.9562
-7.3450
8.260 1
-0.7033
-o/oool
- 0.0000
0.0211
~ 07 S 004
0.0000
0.0183
- 0.0373
0.0143
, .. •
: -o.ooo 3
0.0000
0 . 021 2
0.0004
-o.ooob
0.0183
- 0.0335
0.0129
- 0.0003
- 0.0000
C .02 12
- 0.0275
0.0004
- 0.0000
0 . C 183
0.0107
- C . 0004
- C .0000
0.0212
0.0004
- 0.0000
0.0103
- 0.0207
3.008 1
-r.ooo’5
- 0.0000
0.0212
" o rooo 5
- 0.0000
0 . 01 F 3
- 0.0143
0.0658
-oToobT
- 0.0000
0.0212
- 0.0096
0.0007
- 0.0000
0.0183
0.0037
—
.
- 0.0013
- 0.0001
0.0212
0.0013
- 9 , Q 000
0.0183
- 0.0047
0 . 001 C
“cm-90^00; GAWA* U5 «TA» 10.00
X/H* 0.
Y/H 1 0.
Z/H = 0.20 ETA- 1.00
l ' -
y —
LMeIU
(U.U
jjUflj
-5*9777
5.9606
- 5-9468
0.0000
-5.9563
5.9629
- 5.9504
0.0000
6.4842
-5.9101
5 .949Q
-0.0000
'75.9683
5. 9683
- 5.9663
0.0000
5.9683
-5.9683
5.9683
-0.0000
-0.0094
-0.0078
0.0215
0. dl 20
-0.0054
0.0180
0. oo&o
NASA-Lanpley, 1962
L-15^9
Live Music Archive
Librivox Free Audio
Metropolitan Museum
Cleveland Museum of Art
Internet Arcade
Console Living Room
Books to Borrow
Open Library
TV News
Understanding 9/11