Books on the topic 'Aeronautical turbine'

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1

Rogo, C. Variable area radial turbine fabrication and test program. [Cleveland, Ohio: Army Aviation Research & Technology Activity, Propulsion Directorate, 1986.

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2

Bill, Gunston. The development of jet and turbine aero engines. Yeovil: Patrick Stephens, 1995.

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3

Center), NASA-Chinese Aeronautical Establishment (CAE) Symposium (1985 NASA Lewis Research. Combustion fundamentals: NASA-Chinese Aeronautical Establishment (CAE) Symposium. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

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4

Aerothermodynamics of gas turbine and rocket propulsion. 3rd ed. Reston, VA: American Institute of Aeronautics and Astronautics, 1997.

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5

Aerothermodynamics of gas turbine and rocket propulsion. Washington, DC: American Institute of Aeronautics and Astronautics, 1988.

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6

L, Braslow Albert, Butterfield A. J, and Langley Research Center, eds. Circulation control propellers for general aviation, including a BASIC computer program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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7

1959-, Pierre Christophe, and United States. National Aeronautics and Space Administration., eds. Stochastic sensitivity measure for mistuned high-performance turbines. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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8

J, Holt Mark, ed. The turbine pilot's flight manual. Ames: Iowa State University Press, 1995.

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9

J, Holt Mark, ed. The turbine pilot's flight manual. 2nd ed. Ames: Iowa State University Press, 2001.

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10

C, Smith Steven. Airflow calibration of a bellmouth inlet for measurement of compressor airflow in turbine-powered propulsion simulators. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1985.

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11

United States. National Aeronautics and Space Administration., ed. PROBABILISTIC ANALYSIS OF GAS TURBINE FIELD PERFORMANCE... NASA/TM--2002-211699... NATIONAL AERONAUTICS AND SPACE ADMINISTRATION... NOVEMBER. [S.l: s.n., 2003.

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12

United States. National Aeronautics and Space Administration., ed. Space shuttle main engine: NASA has not evaluated the alternate fuel turbopump costs and benefits : report to the Administrator, National Aeronautics and Space Administration. Washington, D.C: The Office, 1993.

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13

United States. National Aeronautics and Space Administration, ed. Space shuttle main engine: NASA has not evaluated the alternate fuel turbopump costs and benefits : report to the Administrator, National Aeronautics and Space Administration. Washington, D.C: The Office, 1993.

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14

United States. National Aeronautics and Space Administration., ed. Space shuttle main engine: NASA has not evaluated the alternate fuel turbopump costs and benefits : report to the Administrator, National Aeronautics and Space Administration. Washington, D.C: The Office, 1993.

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15

Walter, Blanchard, and Royal Institute of Navigation (Great Britain), eds. Air navigation from balloons to Concorde: Selected essays from the archives of the Royal Institute of Navigation. Bognor Regis: Woodfield Pub., 2005.

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16

C, Oates Gordon, ed. Aerothermodynamics of aircraft engine components. New York, N.Y: American Institute of Aeronautics and Astronautics, 1985.

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17

C, Oates Gordon, ed. Aircraft propulsion systems technology and design. Washington, DC: American Institute of Aeronautics and Astronautics, 1989.

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18

Werding, Hans. So flogen schon die Pharaonen: Schiffsantriebe, Dusen, Turbinen, Propeller, Flugzeuge, Fliegende Untertassen u.v.a. ; Gebaut nach den Hieroglyphen Amenophis IV. Lohne: LITprivat-Verlag, 1990.

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19

Cunningham, Robert E. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. Cleveland, Ohio: Lewis Research Center, 1986.

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20

Cunningham, Robert E. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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21

E, Cunningham Robert. Passive eddy-current damping as a means of vibration control in cryogenic turbomachinery. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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22

Conner, Margaret. Hans Von Ohain: Elegance in Flight (General Publication). AIAA (American Institute of Aeronautics & Ast, 2002.

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23

Grafton, Thomas A. III. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. 1987.

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24

(Editor), Timothy C. Lieuwen, and Vigor Yang (Editor), eds. Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, And Modeling (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Ast, 2005.

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25

Investigation of the Influence of Supersonic Rotor Velocities on Turbine Performance and Design. Creative Media Partners, LLC, 2021.

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26

Fuel Vaporization in the Pre-Ignition Zone of a Gas Turbine Combustion Chamber. Creative Media Partners, LLC, 2021.

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27

Turbine Pilots Flight Manual. Iowa State Press, 1998.

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28

Manning, Walter William. Study of electrostatic modulation of fuel sprays to enhance combustion performance in an aviation gas turbine. 1987.

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29

Urich, Dave J. An experimental investigation of soot size and flow fields in a gas turbine engine augmentor tube. 1986.

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30

Jway, Ching Hua. An investigation into the effects of fuel additives and fuel composition on soot particle size in a T63 gas turbine combustor using light transmittance and scattering techniques. 1986.

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31

Smith, I. E. Combustion in Advanced Gas Turbine Systems: Proceedings of an International Propulsion Symposium Held at the College of Aeronautics, Cranfield, April 1967. Elsevier Science & Technology Books, 2014.

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32

Blanchard, Walter. Air Navigation from Balloons to Concorde. Woodfield Publishing, 2006.

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33

Sieverding, C. H., G. Cicatelli, J. M. Desse, M. Meinke, and P. Zunino. Experimental and Numerical Investigation of Time Varying Wakes behind Turbine Blades: Results of the Industrial and Material Technology Aeronautics ... and Multidisciplinary Design). Springer, 2001.

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34

Probabilistics Analysis Of Solid Oxide Fuel Cell Based Hybrid Gas Turbine System... NASA/TM-2003-211995... National Aeronautics And Space Administration... April 2003. [S.l: s.n., 2003.

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35

Norster, E. R. Combustion and Heat Transfer in Gas Turbine Systems: Proceedings of an International Propulsion Symposium Held at the College of Aeronautics, Cranfield, April 1969. Elsevier Science & Technology Books, 2013.

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36

1939-, Sieverding C. H., and European Commission. Directorate-General XII, Science, Research, and Development., eds. Experimental and numerical investigation of time varying wakes behind turbine blades: Results of the Industrial and Material Technology Aeronautics Research Project AER2-CT92-0048, 1992-1996. Braunschweig/Wiesbaden: Vieweg, 1999.

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37

Royce, Rolls Rolls. Jet Engine. Wiley & Sons, Limited, John, 2022.

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38

Jet Engine. Wiley & Sons, Limited, John, 2015.

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39

Radar Micro-Doppler Signatures: Processing and applications. The Institution of Engineering and Technology, 2014.

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40

Chen, Victor C., William J. Miceli, and David Tahmoush. Radar Micro-Doppler Signatures: Processing and Applications. Institution of Engineering & Technology, 2014.

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