1 p. L., iv, 5-262 p. incl. illus., tables, diagrs. 23 cm
Topic: Gas-turbines
California Digital Library
1,025
1.0K
Feb 1, 2007
02/07
by
Moss, Sanford A. (Sanford Alexander)
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Thesis (PH.D.)--Cornell University
Topic: Gas-turbines
Caption title
Topic: Gas turbines
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21
Jan 30, 2020
01/20
by
Dusinberre, George Merrick
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256 pages 25 cm
Topic: Gas-turbines
284
284
Dec 10, 2009
12/09
by
Wegner von Dallwitz, Richard Maximilian Ferdinand Albert, 1873-
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Book digitized by Google from the library of University of California and uploaded to the Internet Archive by user tpb.
Topic: Gas-turbines
Source: http://books.google.com/books?id=mVxDAAAAIAAJ&oe=UTF-8
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2.0
Mar 10, 2022
03/22
by
ASME Turbo Expo (2004 : Vienna, Austria)
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7 volumes in 8 : 28 cm
Topics: Gas-turbines -- Congresses, Gas-turbines -- Aerodynamics -- Congresses, Engineering design --...
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Oct 28, 2020
10/20
by
ASME Turbo Expo (2003 : Atlanta, Ga.)
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6 volumes in 8 : 28 cm
Topics: Gas-turbines -- Congresses, Gas-turbines -- Aerodynamics -- Congresses, Engineering design --...
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2.0
Apr 12, 2022
04/22
by
Frutschi, Hans Ulrich
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x, 283 p. : 24 cm
Topic: Gas-turbines
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92
Dec 19, 2019
12/19
by
Boyce, Meherwan P
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xv, 799 pages : 25 cm
Topics: Gas-turbines -- Handbooks, manuals, etc, Gas-turbines, Gasturbine
Topic: Marine gas-turbines
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10.0
Nov 8, 2021
11/21
by
Lefebvre, Arthur H. (Arthur Henry), 1923-2003
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xvii, 531 p. : 25 cm
Topic: Gas-turbines -- Combustion
Naval Postgraduate School
234
234
Jan 14, 2013
01/13
by
Young, Mark F;Grafton, Thomas A;Conner, H;Netzer, David W
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Title from cover
Topics: COMBUSTORS, GAS TURBINES
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804235&ix=nu&I=0&V=D&pm=1
Topics: Aerodynamics, Gas-turbines.
A computer program was written for use in sizing gas turbine counterflow regenerators. The program simulates the semi-open gas turbine regenerative cycle under constant load conditions. Inputs to the program include compressive ratio, turbine inlet temperature, component efficiencies, horsepower output and regenerator core geometry. External regenerator core dimensions are varied and various supports are computed such as thermal efficiency, mass flow rate, total relative pressure drop,...
Topics: Gas turbines, Regenerator
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59
May 24, 2013
05/13
by
Woodward, John B
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"A Wiley-Interscience publication."
Topic: Marine gas-turbines
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83
Oct 7, 2015
10/15
by
Young, Mark F;Grafton, Thomas A;Conner, H;Netzer, David W
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Title from cover
Topic: COMBUSTORS,GAS TURBINES
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25
Jun 10, 2019
06/19
by
O'Brien, John Patrick, 1925-
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ix, 342 p. : 25 cm. --
Topic: Automotive gas turbines
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3.0
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xiv, 262 p. : 25 cm
Topic: Gas-turbines -- Ceramic materials
A preliminary design study was conducted to determine the geometry for an enhanced mixing eductor system for the Landing, Helicopter Assault Ship Replacement (LHA R) program gas turbine exhaust. A one-dimensional analytical model, with a correction factor applied to the secondary mass flow, was developed to predict the secondary air mass flow rate and the exhaust temperature at the mixing tube exit plane. The resultant design consisted of a high aspect ratio lobed nozzle and a mixing tube. The...
Topics: Ejector pumps, Gas-turbines
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71
Oct 7, 2015
10/15
by
Stammettii, Vincent A.
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Title from cover
Topic: GAS TURBINES.,MARINE ENGINES.
Title from cover
Topics: GAS TURBINES., MARINE ENGINES.
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3.0
Mar 31, 2022
03/22
by
ASM Materials Week '93 (1993 : Pittsburgh, Pa.)
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iv, 143 pages : 28 cm
Topic: Gas-turbines -- Coatings -- Congresses
This thesis presents an analysis of data taken from several stall initiation events for an LM-2500 gas turbine engine. Specifically, the time series of three separate pressure signals located at stages 3, 6, and 15 were analyzed utilizing fast Fourier transform, power spectral density, and an autocorrelation technique to determine the best and most reliable indicator to stall. The spectral analyses performed showed that rotating precursor waves that travel at approximately half rotor speed were...
Topics: Gas-turbines, Stalling (Aerodynamics)
Sponsored by the Bureau of Ships
Topics: Gas-turbines--Incrustations, Heat exchangers
A hardware model of the Gas Turbine Generator (GTG) in use on the US Navy's DDG-51 Class Destroyer is constructed for use as a lab apparatus at the Massachusetts Institute of Technology's Laboratory for Electromagnetic and Electronic Systems (LEES). The components of the hardware model include a 5 kilowatt three-phase generator; DC power supplies and motors that function as the prime mover; computer software to implement speed and voltage control; and an input-output interface board that passes...
Topics: Gas-turbines, Computer programs, Speed
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76
Oct 8, 2015
10/15
by
Kohler, Henry L. ; Miller, J.A.
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Sponsored by the Bureau of Ships
Topic: Gas-turbines--Incrustations,Heat exchangers
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Jun 18, 2021
06/21
by
McMahon, Patrick Joseph
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xi, 379 p. 23 cm
Topics: Airplanes -- Motors, Aircraft gas-turbines
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70
Sep 28, 2020
09/20
by
Mattingly, Jack D
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xxx, 582 pages : 24 cm
Topics: Aircraft gas-turbines -- Design and construction, Flugtriebwerk, Aircraft gas-turbines Design and...
215
215
Nov 30, 2018
11/18
by
Otis, Charles E. (Charles Edward), 1932-
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xix, 466 pages : 28 cm
Topic: Aircraft gas-turbines -- Design and construction
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810529&ix=nu&I=0&V=D&pm=1
Topics: Aircraft gas-turbines--Blades, Aerodynamics--Research.
This thesis presents a simple, meanline analysis of the impact of blade roughness on the mass flow, work coefficient, and efficiency of a three-stage axial compressor as a function of the location of fouling. First, an extensive review is presented on the state-of-the-art of measuring compressor degradation and on the impact of roughness on loss and deviation in a compressor cascade. The performance of a baseline, three-stage compressor, which has hydrodynamically smooth blades, is predicted....
Topics: Gas-turbines, Compressors, Blades, Performance, Fouling
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95
Oct 7, 2015
10/15
by
Stammetti, Vincent A.;Smith, David L.
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Cover title
Topic: Marine gas-turbines,Design and construction
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4.0
Apr 22, 2022
04/22
by
Saarlas, Maido
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x, 239 p., [1] leaf of plates : 27 cm
Topics: Steam-turbines, Marine, Marine gas-turbines
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208
Aug 5, 2011
08/11
by
Bent, Ralph D; McKinley, James L
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Includes index
Topics: Airplanes, Propellers, Aerial, Aircraft gas-turbines
http://uf.catalog.fcla.edu/uf.jsp?st=UF023036446&ix=pm&I=0&V=D&pm=1
Topics: Jet propulsion, Airplanes--Motors, Gas-turbines.
As part of an on going High Cycle Fatigue program related to gas turbine engines, which is sponsored jointly by the Naval Air Systems Command and the Air Force, unsteady strain gauge measurements were made on a 37.5 inch diameter titanium rotor in the Naval Postgraduate School, Turbopropulsion Laboratory vacuum spin pit. Vibratory excitation was produced by a number of evenly spaced magnets positioned around the rotor perimeter, which generated eddy currents in the blades and associated...
Topics: Strain gages, Calibration, Gas-turbines, Blades
206
206
Jan 6, 2014
01/14
by
Montana. Renewable Energy and Conservation Program; Eagle Energy Systems
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"Grant Agreement Number 467-811."
Topics: Gas-turbines, Electric power, Wood waste
Naval Postgraduate School
358
358
Oct 16, 2012
10/12
by
Stammetti, Vincent A.;Smith, David L.
texts
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Cover title
Topics: Marine gas-turbines, Design and construction
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16
Jan 15, 2020
01/20
by
Carroll, William, 1915- editor
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120 pages 28 cm
Topics: Automobiles, Gas-turbine, Automotive gas turbines
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61
Jun 29, 2020
06/20
by
Norbye, Jan P
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xvi, 570 pages : 24 cm
Topics: Automotive gas turbines, Automobiles, Gas-turbine
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66
Oct 6, 2015
10/15
by
Franke, Richard H.
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Technical report for period October 1984 - March 1985--Cover.
Topic: ENTHALPY.,FLUID MECHANICS.,GAS-TURBINES.,JET ENGINES.
Technical report for period October 1984 - March 1985--Cover.
Topics: ENTHALPY., FLUID MECHANICS., GAS-TURBINES., JET ENGINES.
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Apr 18, 2022
04/22
by
Giampaolo, Tony, 1939-
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1 online resource (xv, 405 pages) :
Topics: Gas-turbines -- Handbooks, manuals, etc, Turbines à gaz -- Guides, manuels, etc, TECHNOLOGY &...
This thesis contains an analysis of the failure of the instrumentation ring for measuring the combustor exit temperature and total pressure in the T63-A-700 gas turbine engine. An improved ring design has been constructed and installed. Extensions to the exhaust stacks have been installed to keep the cell temperature reasonable. A water-cooled heat exchanger was installed in place of an air-cooled heat exchanger that was not adequately cooling the oil temperature while running the engine. In...
Topics: Gas-turbines., Compressor map, GASTURB, Heat exchanger, SMOOTHC, Thermocouple
http://uf.catalog.fcla.edu/uf.jsp?st=UF002324692&ix=pm&I=0&V=D&pm=1
Topics: Gas-turbines--Vibration, Vibration--Measurement, Neural networks (Computer science.
Operational experience indicates that steam escaping from carrier catapults has the potential to induce stall or surge in the compressors of jet aircraft during takeoff. As the carrier fleet ages and the Navy transitions to the single engine F-35C variant of the Joint Strike Fighter, further investigation of steaminduced surge phenomena is necessary to avert undue risks to pilots and to obviate stall related damage to Navy aircraft. This study investigated the effects of both throttle-induced...
Topics: Airplanes, Jet propulsion, Aircraft gas-turbines, Compressors, Fluid dynamics
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xi, 306 pages : 23 cm
Topics: Gas-turbines -- Materials, Instalacoes Hidraulicas, Motores De Combustao Interna
Topics: NOx control, gas turbine combustors, gas turbine fuel additives, soot control, pollution control,...
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177
Sep 25, 2017
09/17
by
Fiock, Ernest F.; Halpern, Carl
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Topics: Gas-turbines -- Bibliography., Jet propulsion -- Bibliography., Rockets (Aeronautics) --...
Progress report for period October 1984 - September 1985.
Topics: CONTROL SYSTEMS., DIGITAL SYSTEMS., GAS TURBINES., MARINE ENGINES., MARINE PROPULSION.
