Title from cover
Topics: EXHAUST PLUMES., SUPERSONIC FLOW.
125
125
Oct 7, 2015
10/15
by
Falcovitz, Joseph.
texts
eye 125
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Title from cover
Topic: EXHAUST PLUMES.,SUPERSONIC FLOW.
225
225
May 6, 2010
05/10
by
Gonor, A. L
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eye 225
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Exact solution of supersonic gas flow problem for spatial bodies of star-like structure
Topics: GAS FLOW, MACH NUMBER, STARS, SUPERSONIC FLOW, GAS FLOW, STAR, SUPERSONIC FLOW
291
291
May 6, 2010
05/10
by
Westphal, W. R
texts
eye 291
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Supersonic flow of two turbine blade sections with turning angle of 160-degrees
Topics: CASCADES, MACH NUMBER, SUPERHARMONICS, SUPERSONIC FLOW, TURBINE BLADES, CASCADE, SUPERSONIC FLOW,...
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224
Jun 19, 2010
06/10
by
Belotserkovskiy, O. M.; Sedova, Ye. S.; Shugayev, R. V
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eye 224
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Supersonic flow around blunt body of revolution with generatrix discontinuity
Topics: BLUNT BODIES, BODIES OF REVOLUTION, DISCONTINUITY, SUPERSONIC FLOW, SYMMETRY, BLUNT BODY,...
379
379
May 6, 2010
05/10
by
Dugan, J. F
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eye 379
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Rotating-stall limits in supersonic turbofan engine
Topics: MACH NUMBER, ROTATING STALLS, SUPERSONIC FLOW, TURBOFAN ENGINES, ROTATING STALL, SUPERSONIC FLOW,...
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232
Jun 17, 2010
06/10
by
Khodyko, Yu. V
texts
eye 232
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Supersonic flow around thin bodies of revolution by gas
Topics: BODIES OF REVOLUTION, GAS FLOW, SUPERSONIC FLOW, THIN BODIES, GAS FLOW, REVOLUTION, SUPERSONIC...
561
561
Jun 19, 2010
06/10
by
Enselme, M
texts
eye 561
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Aerodynamic characteristics of wing-fuselage combination in supersonic flow
Topics: AERODYNAMIC CHARACTERISTICS, BODY-WING CONFIGURATIONS, CONFERENCES, FUSELAGES, SUPERSONIC FLOW,...
233
233
Jun 18, 2010
06/10
by
Shvets, A. P
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eye 233
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Supersonic flow around ellipsoids and detached shock wave positions from wind tunnel tests
Topics: AERODYNAMICS, SUPERSONIC FLOW, WIND TUNNEL, DETACHMENT, ELLIPSOIDS, SHOCK WAVES, SUPERSONIC FLOW,...
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217
Jun 18, 2010
06/10
by
Bolotin, V. V.; Novichkov, Yu. N
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eye 217
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Buckling and steady flutter of heat compressed panels in supersonic flow
Topics: BUCKLING, THERMAL BUCKLING, COMPRESSING, FLUTTER ANALYSIS, PANEL FLUTTER, SUPERSONIC FLOW, THERMAL...
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229
Jul 9, 2010
07/10
by
Fedors, R. F.; Landel, R. F
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eye 229
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No Abstract Available
Topics: MISSILES, RAMJET ENGINES, PROPULSION SYSTEM PERFORMANCE, SUPERSONIC FLOW
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237
May 30, 2011
05/11
by
Marscher, Alan P
texts
eye 237
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Research supported by this grant involved theoretical investigations of the multifrequency nonthermal emission from the relativistic jets in blazars, which are quasars and related objects with highly variable brightness. In the initial stage of the project, one-dimensional, conical (i.e., spherical symmetry between the jet axis and surface is assumed) jet models were used to explain the multi-waveband spectra and variability of blazars. The results were applied to two flares observed in the...
Topics: SUPERSONIC FLOW, VISCOUS FLOW, COMPUTERIZED SIMULATION, SHOCK WAVES
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424
Jun 19, 2010
06/10
by
Gogish, L. V.; Stepanov, G. YU
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eye 424
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Approximation method for calculating base pressure in two-dimensional supersonic flows
Topics: APPROXIMATION, BASE PRESSURE, ISENTROPIC PROCESSES, SUPERSONIC FLOW, TWO DIMENSIONAL FLOW,...
434
434
May 6, 2010
05/10
by
Savin, R. C
texts
eye 434
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Approximate solution for flow about flat-top wing body configuration at supersonic speeds
Topics: AIRSPEED, WING BODY, ANGLE OF ATTACK, APPROXIMATION, BODY-WING CONFIGURATIONS, SUPERSONIC FLOW,...
214
214
Jun 19, 2010
06/10
by
Golubinskiy, A. I.; Ivanov, A. N
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eye 214
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Exact solutions to problem of hypersonic or supersonic gas flow past slipping or delta wing with stall fence
Topics: AERODYNAMIC STALLING, SUPERSONIC FLOW, WING STALL, DELTA WINGS, GAS FLOW, HYPERSONIC FLOW,...
384
384
May 6, 2010
05/10
by
Church, J. D.; Taylor, N. L
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eye 384
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Force study of scale model xsm-64a navaho missile and booster at supersonic speeds
Topics: AERODYNAMIC FORCES, BOOSTER, NAVAHO MISSILE, SCALE MODEL, SUPERSONIC FLOW, BOOSTERS, NAVAHO...
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157
Jun 19, 2010
06/10
by
Borisov, V. M
texts
eye 157
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Variational problems of supersonic gas dynamics in determining shape of minimum drag axisymmetric bodies
Topics: AXISYMMETRIC BODIES, DRAG, GAS DYNAMICS, SUPERSONIC FLOW, VARIATION METHOD, GAS DYNAMICS, MINIMUM...
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444
Jul 5, 2010
07/10
by
Laugwitz, D.; Schmieden, C
texts
eye 444
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No Abstract Available
Topics: LINEAR EQUATIONS, SUPERSONIC FLOW, WINGS, PROBLEM SOLVING, THREE DIMENSIONAL FLOW
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957
Jun 21, 2010
06/10
by
NON
texts
eye 957
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No Abstract Available
Topics: ELECTRON PLASMA, SHOCK WAVES, SUPERSONIC FLOW, ELECTROSTATIC WAVES, PLASMA HEATING
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192
May 31, 2011
05/11
by
NON
texts
eye 192
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Hi-Tech Inc., a company which manufactures water jetting equipment, needed a high pressure rotating swivel, but found that available hardware for the system was unsatisfactory. They were assisted by Marshall, which had developed water jetting technology to clean the Space Shuttles. The result was a completely automatic water jetting system which cuts rock and granite and removes concrete. Labor costs have been reduced; dust is suppressed and production has been increased.
Topics: JET FLOW, AEROACOUSTICS, SUPERSONIC FLOW, JET IMPINGEMENT, PRESSURE RATIO, JET NOZZLES
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356
Jun 17, 2010
06/10
by
Ivanov, A. V
texts
eye 356
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Rarefied gas density near forward stagnation point of blunt body in supersonic flow
Topics: BLUNT BODIES, GAS DENSITY, RAREFIED GAS, STAGNATION POINT, SUPERSONIC FLOW, DECELERATION, GAS...
1,369
1.4K
Jun 20, 2010
06/10
by
Belotserkovskiy, O. M
texts
eye 1,369
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Supersonic gas flow around blunt bodies, and numerical algorithms constructed for calculating two-dimensional and three-dimensional bodies of various shapes
Topics: ALGORITHMS, BLUNT BODY, NUMERICAL ANALYSIS, SUPERSONIC FLOW, TWO-DIMENSIONAL BODY, BLUNT BODIES,...
555
555
Jun 2, 2011
06/11
by
Gates, Thomas S.; Odegard, Gregory M.; Herring, Helen M
texts
eye 555
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The next generation of space transportation vehicles will require advances in lightweight structural materials and related design concepts to meet the increased demands on performance. One potential source for significant structural weight reduction is the replacement of traditional metallic cryogenic fuel tanks with new designs for polymeric matrix composite tanks. These new tank designs may take the form of thin-walled sandwich constructed with lightweight core and composite facesheets....
Topics: AIRCRAFT CONFIGURATIONS, AERODYNAMIC DRAG, SUPERSONIC FLOW, DRAG REDUCTION, SINGULARITY...
Mendeley Climate Change Library
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43
Jul 5, 2019
07/19
by
Chuang Wen; Nikolas Karvounis; Jens Honore Walther; Yuying Yan; Yuqing Feng; Yan Yang
texts
eye 43
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The mitigation of CO 2 emissions is an effective measure to solve the climate change issue. In the present study, we propose an alternative approach for CO 2 capture by employing supersonic flows. For this purpose, we first develop a computational fluid dynamics (CFD) model to predict the CO 2 condensing flow in a supersonic nozzle. Adding two transport equations to describe the liquid fraction and droplet number, the detailed numerical model can describe the heat and mass transfer...
Topics: CO 2 emission, CO 2 separation, Carbon capture and storage, Supersonic flow
911
911
Jun 21, 2010
06/10
by
TITOVA, L. K
texts
eye 911
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EMBRYONAL DEVELOPMENT OF RECEPTOR STRUCTURES OF VESTIBULAR APPARATUS AND CORTI ORGAN IN VERTEBRATES
Topics: LEADING EDGES, SUPERSONIC FLOW, TRAILING EDGES, WINGS, COMPUTER PROGRAMMING, UNIVAC 1108 COMPUTER
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170
Jun 18, 2010
06/10
by
Chiccine, B. G.; Mitchell, G. A
texts
eye 170
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Internal flow performance of fixed 14 deg ramp inlet from zero to 20 deg angle of attack at supersonic free stream
Topics: ANGLE OF ATTACK, THROATS, ANGLE OF ATTACK, FREE STREAM, INLET FLOW, SUPERSONIC FLOW, BOUNDARY...
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349
Jun 26, 2010
06/10
by
Herbell, T. P.; Quatinetz, M.; Weeton, J. W
texts
eye 349
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Production of high strength refractory compounds and microconstituents into refractory metal matrix
Topics: COMBUSTION PHYSICS, HYDROGEN, SUPERSONIC COMBUSTION, IGNITION, RARE GASES, SUPERSONIC FLOW,...
840
840
May 6, 2010
05/10
by
Robins, A. W
texts
eye 840
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Force and pressure measurements on several canopy- fuselage configurations at low supersonic speeds
Topics: AERODYNAMIC FORCES, SUPERHARMONICS, SUPERSONIC FLOW, SUPERSONIC SPEED, WINDSHIELDS, AERODYNAMIC...
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194
Jun 18, 2010
06/10
by
Chushkin, P. I.; Katskova, O. N
texts
eye 194
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Three-dimensional supersonic flow of gas in thermodynamic equilibrium around body at angle of attack
Topics: ANGLE OF ATTACK, GAS FLOW, SUPERSONIC FLOW, THERMODYNAMIC EQUILIBRIUM, THREE-DIMENSIONAL FLOW,...
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547
Jul 12, 2010
07/10
by
NON
texts
eye 547
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The SIR-A experiment was conducted in order to acquire radar data over a variety of regions to further understanding of the radar signatures of various geologic features. The capability of the Shuttle as a scientific platform for observation of the Earth's resources was assessed. The SIR-A sensor operated nominally and the full data acquisition capacity of the optical recorder was used.
Topics: CHANNEL FLOW, SUPERSONIC FLOW, TRANSONIC FLOW, PRESSURE MEASUREMENT, TRANSONIC WIND TUNNELS,...
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268
Jul 11, 2010
07/10
by
TANKHELSON, A.; ZAYNUTDINOV, S
texts
eye 268
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AN ACCOUNT OF THE FIFTH CONFERENCE OF THE JOINT SOVIET-AMERICAN WORKING GROUP ON SPACE BIOLOGY AND MEDICINE, HELD AT TASHKENT, IS PRESENTED. TOPICS DISCUSSED THE SPACEFLIGHT RESULTS OF SOVIET RESEARCH METHODS, AND EXCHANGE OF RESEARCH REPORTS.
Topics: CENTRIFUGAL COMPRESSORS, FLUID FLOW, SUPERSONIC DIFFUSERS, SUPERSONIC FLOW, FLOW DISTRIBUTION,...
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251
May 28, 2011
05/11
by
Bansal, Narottam P.; Eldridge, Jeffrey I
texts
eye 251
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Unidirectional celsian matrix composites having 42-45 vol % of uncoated or BN-SIC coated Hi-Nicalon fibers were tested in three-point bend at room temperature. The uncoated fiber-reinforced composites showed catastrophic failure with strength of 210 35 MPa and a flat fracture surface. In contrast, composites reinforced with coated fibers exhibited graceful failure with extensive fiber pullout. Values of first matrix cracking stress and strain were 435 /- 35 MPa and 0.27 /- 0.01%, respectively,...
Topics: HYDROGEN, SUPERSONIC FLOW, KEROSENE, GAS STREAMS, COMBUSTION EFFICIENCY, ENERGY LEVELS,...
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236
Jun 1, 2011
06/11
by
Krebs, Richard P.; Hensley, Reece V
texts
eye 236
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Performance characteristics of the turbine of a 4000-pound-thrust axial-flow turbojet engine was determined in investigations of the complete engine in the NACA Cleveland altitude wind tunnel. Characteristics are presented as functions of the total-pressure ratio across the turbine and of turbine speed and gas flow corrected to sea-level conditions. Three turbine nozzles of different areas were used to determine the area that gave optimum performance. Inasmuch as tail-pipe nozzles of different...
Topics: COMPRESSIBILITY, VANES, WINGS, SUPERSONIC FLOW, COMPRESSIBLE FLOW, FLOW VELOCITY, FLOW...
This research showed the bow shock formation in a complex plasma, where plasma particles and charged dust particles form a complex entity. The formation was visible by naked eyes through the illumination of laser light on dust particles. The supersonic flow was possible to make in a complex plasma since dust acoustic wave is characterized by a sound speed of a few cm per second. This observation is important as it is a good representation of bow shocks commonly observed in planetary...
Topics: DTIC Archive, YOKOHAMA NATIONAL UNIV (JAPAN), *PLASMAS(PHYSICS), DUST, JAPAN, LASERS, SUPERSONIC...
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623
Jun 1, 2011
06/11
by
Mukhopadhyay, Vive
texts
eye 623
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An interactive computer program was developed for wing flutter analysis in the conceptual design stage. The objective was to estimate flutter instability boundaries of a typical wing, when detailed structural and aerodynamic data are not available. Effects of change in key flutter parameters can also be estimated in order to guide the conceptual design. This userfriendly software was developed using MathCad and Matlab codes. The analysis method was based on non-dimensional parametric plots of...
Topics: SUPERSONIC FLOW, AIRCRAFT DESIGN, SUBSONIC FLOW, AERODYNAMICS, COMPUTATION, FLOW VELOCITY,...
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273
May 31, 2011
05/11
by
Curtis, Scott; Adler, Robert F
texts
eye 273
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This study uses a twenty-three year (1979-2001) satellite-gauge merged community data set to further describe the relationship between El Nino Southern Oscillation (ENSO) and precipitation. The globally complete precipitation fields reveal coherent bands of anomalies that extend from the tropics to the polar regions. Also, ENSO-precipitation relationships were analyzed during the six strongest El Ninos from 1979 to 2001. Seasons of evolution, Pre-onset, Onset, Peak, Decay, and Post-decay, were...
Topics: SHAPE OPTIMIZATION, COMPUTER PROGRAMMING, AERODYNAMICS, SUPERSONIC FLOW, FUNCTIONS (MATHEMATICS),...
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258
Jun 1, 2011
06/11
by
Encke, W
texts
eye 258
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A selection of measurements obtained on experimental impellers for axial blowers will be reported. In addition to characteristic curves plotted for low and for high peripheral velocities, proportions and blade sections for six different blower models and remarks on the design of blowers will be presented.
Topics: CONICAL FLOW, SUPERSONIC FLOW, AIRCRAFT DESIGN, DIFFERENTIAL EQUATIONS, MACH CONES, GAS FLOW,...
The Transonic Turbine Test Rig at the Naval Postgraduate School, Monterey, California, uses a super sonic jet exhauster to lower the turbine exit static pressure and thus increase pressure ratios available for turbine testing. Exhauster operation results in inter action between two co-flowing streams of air. The primary air is supersonic and the secondary air, subsonic. This thesis is an experimental study of the mixing process that occurs between the two streams in a cylindrical mixing...
Topics: Aeronautics, Exhauster, Ejector, Mixing of co-flowing streams, Turbulent jet, Compressible mixing,...
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327
May 28, 2011
05/11
by
Lind, Rick; Brenner, Marty; Freudinger, Lawrence C
texts
eye 327
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Wavelets present a method for signal processing that may be useful for analyzing responses of dynamical systems. This paper describes several wavelet-based tools that have been developed to improve the efficiency of flight flutter testing. One of the tools uses correlation filtering to identify properties of several modes throughout a flight test for envelope expansion. Another tool uses features in time-frequency representations of responses to characterize nonlinearities in the system...
Topics: BOUNDARY LAYER TRANSITION, VISCOUS FLOW, SHARP LEADING EDGES, LEADING EDGES, SUPERSONIC FLOW,...
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155
Jun 19, 2010
06/10
by
Shipilin, A. V
texts
eye 155
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Optimum form of two-dimensional and axisymmetric bodies in supersonic ideal gas flow with associated shock waves
Topics: AXISYMMETRIC BODIES, GAS FLOW, IDEAL GAS, SHOCK WAVES, SUPERSONIC FLOW, SYMMETRY, TWO DIMENSIONAL...
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285
May 21, 2011
05/11
by
Gambles, Jody W.; Winkert, To
texts
eye 285
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This paper reports a Class S CCSDS recommendation Reed Solomon encoder circuit baselined for several NASA programs. The chip is fabricated using United Technologies Microelectronics Center's UTE-R radiation-hardened gate array family, contains 64,000 p-n transistor pairs, and operates at a sustained output data rate of 200 MBits/s. The chip features a pin selectable message interleave depth of from 1 to 8 and supports output block lengths of 33 to 255 bytes. The UTE-R process is reported to...
Topics: METHOD OF CHARACTERISTICS, NOZZLE DESIGN, NOZZLE GEOMETRY, SUPERSONIC NOZZLES, RADII, SUBSONIC...
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477
Jun 27, 2010
06/10
by
Denery, D. G
texts
eye 477
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Algorithm for identification of system parameters from input-output data with application to air vehicles
Topics: AERODYNAMICS, GAS DYNAMICS, ROCKET ENGINE DESIGN, SUPERSONIC FLOW, AERODYNAMIC CHARACTERISTICS,...
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211
Jul 23, 2010
07/10
by
Kulikovskii, A. G
texts
eye 211
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No Abstract Available
Topics: REATTACHED FLOW, SUPERSONIC FLOW, TWO DIMENSIONAL FLOW, BACKWARD FACING STEPS, BOUNDARY LAYERS,...
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219
Jul 6, 2010
07/10
by
Schuster, B.; Stanley, E
texts
eye 219
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Long term effects of physical exercise and conditioning in the prevention and treatment of coronary heart disease are studied. Some aspects of the problem are outlined and difficulties encountered in a group of middle aged business executives using a carefully prescribed, but non-regimented and loosely supervised conditioning program employing commonly used forms of exercise (bicycling and jogging), are described.
Topics: BOLTZMANN TRANSPORT EQUATION, LASERS, MATHEMATICAL MODELS, SUPERSONIC FLOW, CARBON MONOXIDE,...
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340
May 23, 2011
05/11
by
Nerney, Steven; Suess, S. T
texts
eye 340
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We have solved for the potential flow downstream of the terminal shock of the solar wind in the limit of small departures from a spherical shock due to a latitudinal ram pressure variation in the supersonic solar wind. The solution connects anisotropic streamlines at the shock to uniform streamlines down the heliotail because we use a non-slip boundary condition on the heliopause at large radii. The rotational velocity about the heliotail in the near-field solution decays as the fourth power of...
Topics: CONVERGENCE, SUPERSONIC FLOW, TRANSONIC FLOW, OPTIMIZATION, DESIGN ANALYSIS, AERODYNAMIC...
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270
May 6, 2010
05/10
by
Fohrman, M. J
texts
eye 270
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Static aerodynamic characteristics of short blunt 10-deg semivertex angle cone in helium at supersonic speed
Topics: AFTERBODIES, REYNOLDS NUMBER, STATIC AERODYNAMIC CHARACTERISTICS, SUPERSONIC FLOW, SUPERSONIC...
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Jun 20, 2010
06/10
by
VAUCHERET, X
texts
eye 214
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DEFINITION OF LOCATION AND HEIGHT OF ROUGHNESS INITIATING TRANSITION WITHOUT ADDITIONAL DRAG FOR SUPERSONIC FLOW
Topics: SUPERSONIC FLOW, SURFACE ROUGHNESS, TRANSITION FLOW, AERODYNAMIC DRAG, FLOW GEOMETRY,...
Topics: DTIC Archive, BOGDNOFF, SEYMOUR M., PRINCETON UNIV NJ DEPT OF AERONAUTICAL ENGINEERING, *SUPERSONIC...
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427
Jun 21, 2010
06/10
by
NON
texts
eye 427
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Plans for detailed design, development, fabrication, and astronaut training for lunar flying vehicle
Topics: SEPARATED FLOW, STATISTICAL ANALYSIS, TURBULENT BOUNDARY LAYER, PHASE SHIFT, SPATIAL DISTRIBUTION,...
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364
May 31, 2011
05/11
by
NON
texts
eye 364
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Tensegritoy, inspired by the tensegrity concepts of R. Buckminster Fuller, is an erector set like toy designed to give students an understanding of structural stability. It is used by children, architects, engineers, and teachers. The manufacturer, Tensegrity Systems Corporation, also offers a collapsible point of purchase display which incorporates technology developed for space station trusses described in ''NASA Tech Briefs.'' The tech brief described deployable trusses that can be collapsed...
Topics: COMPUTATIONAL FLUID DYNAMICS, BOUNDARY CONDITIONS, SUPERSONIC INLETS, SUPERSONIC FLOW, UNSTEADY...
