Books on the topic 'Hypersonic propulsion and hypersonic aerothermodynamics'

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1

T, Pratt David, ed. Hypersonic airbreathing propulsion. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.

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2

Heiser, William H. Hypersonic airbreathing propulsion: With Daniel H. Daley and Unmeel B. Mehta. Washington, D.C: American Institute of Aeronautics and Astronautics, 1994.

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3

Hypersonic aerothermodynamics. Washington, DC: American Institute of Aeronautics and Astronautics, 1994.

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4

Park, Chul. Nonequilibrium hypersonic aerothermodynamics. New York: Wiley, 1990.

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5

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.

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6

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Hypersonic combined cycle propulsion. Neuilly sur Seine, France: AGARD, 1990.

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7

Coons, L. L. Propulsion challenges of hypersonic flight. New York: AIAA, 1986.

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8

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Special course on aerothermodynamics of hypersonic vehicles. Neuilly sur Seine, France: AGARD, 1989.

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9

Kors, David L. Combined cycle propulsion for hypersonic flight. New York: AIAA, 1987.

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10

Ahuja, J. K. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

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11

Utyuzhnikov, Sergey V. Hypersonic aerodynamics and heat transfer. New York: Begell, 2014.

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12

Armengaud, F. One-dimensional modeling of hypersonic flight propulsion engines. Washington, D. C: AIAA, 1989.

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13

Flandro, G. A. Dynamic interactions between hypersonic vehicle aerodynamics and propulsion system performance: Final report to Aircraft Guidance and Controls Branch, Guidance and Control Division ... [Washington, DC: National Aeronautics and Space Administration, 1992.

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14

Yamamoto, Yukimitsu. Numerical simulation of hypersonic flow around a space plane. III Analysis of aerothermodynamic heating. Tokyo: National Aerospace Laboratory, 1989.

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15

Harloff, G. J. Viscous three-dimensional analyses for nozzles for hypersonic propulsion. Cleveland, Ohio: Sverdrup Technology, Inc., NASA Lewis Research Center Group, 1990.

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16

Harloff, G. J. Viscous three-dimensional analyses for nozzles for hypersonic propulsion. Cleveland, Ohio: Sverdrup Technology, Inc., NASA Lewis Research Center Group, 1990.

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17

IUTAM Symposium on Aerothermochemistry of Spacecraft and Associated Hypersonic Flows (1992 Marseille, France). Aerothermochemistry of spacecraft and associated hypersonic flows: Proceedings of the IUTAM Symposium held in Marseille, France, Le Palais du Pharo, September 1-4, 1992. [France: s.n.], 1994.

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18

Bruckner, A. P. Investigation of hypersonic ramjet propulsion cycles using a ram accelerator test facility. Paris, France: International Astronautical Federation, 1991.

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19

Dinkelmann, Michael. Reduzierung der thermischen Belastung eines Hyperschallflugzeugs durch optimale Bahnsteuerung. München: Utz, Wissenschaft, 1997.

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20

Salemann, Victor. Propulsion system integration for Mach 4 to 6 vehicles. [New York]: American Institute of Aeronautics and Astronautics, 1988.

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21

Mehta, Unmeel B. Air-breathing aerospace plane development essential: Hypersonic propulsion flight tests. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1994.

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22

Claus, Weiland, and American Institute of Aeronautics and Astronautics, eds. Selected aerothermodynamic design problems of hypersonic flight vehicles. Berlin: Springer, 2009.

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23

Mekkes, Gregory L. Fuel plume image mixing analysis formulation with proper treatment of non-constant velocity flowfields. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

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24

Prabhu, Dinesh Kumble. A new parabolized Navier-Stokes code for chemically reacting flow fields. Ames, Iowa: Iowa State University, 1987.

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25

1936-, Thornton Earl A., ed. Aerospace thermal structures and materials for a new era. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

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26

Harloff, G. J. Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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27

Harloff, G. J. Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off design conditions. [Washington, DC]: National Aeronautics and Space Administration, 1988.

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28

Sinha, N. Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications. New York: AIAA, 1987.

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29

Hollis, Brian R. User's manual for the One-Dimensional Hypersonic Experimental Aero-Thermodynamic (1DHEAT) data reduction code. Hampton, Va: Langley Research Center, 1995.

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30

Hollis, Brian R. User's manual for the One-Dimensional Hypersonic Experimental Aero-Thermodynamic (1DHEAT) data reduction code. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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31

Arrighi, Robert S. PSL: The Propulsion Systems Laboratory, No. 1 & 2. Washington, DC: National Aeronautics and Space Administration, NASA History Division, Office of External Relations, 2012.

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32

Rüggeberg, Thomas. Experimentelle Untersuchungen des Betriebsverhaltens eines Triebwerkseinlaufs bei Überschall-Anström-Machzahlen. Aachen: Shaker Verlag, 1996.

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33

Symposium, Advisory Group for Aerospace Research and Development Propulsion and Energetics Panel. Hypersonic combined cycle propulsion: Papers presented at the Propulsion and Energetics Panel 75th Symposium, held in Madrid, Spain, 28th May to 1st June 1990. Neuilly sur Seine: Agard, 1990.

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34

Palumbo, Giuseppe. Investigation of aerothermodynamics and optical radiation in the hypersonic flow field: Final technical report ... for the period December 11, 1989-January 31, 1993. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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35

Palumbo, G. G. C. Investigation of aerothermodynamics and optical radiation in the hypersonic flow field: Final technical report ... for the period December 11, 1989-January 31, 1993. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

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36

Carty, Atherton A. Development and validation of a supersonic helium-air coannular jet facility. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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37

Ko, William L. Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1999.

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38

Pratt, David T., Daniel H. Daley, Unmeel B. Mehta, and William H. Heiser. Hypersonic Airbreathing Propulsion/Book and Disk (Aiaa Education). AIAA (American Institute of Aeronautics & Ast, 1993.

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39

National Aeronautics and Space Administration (NASA) Staff. Hypersonic Airbreathing Propulsion: An Aerodynamics, Aerothermodynamics, and Acoustics Competency White Paper. Independently Published, 2018.

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40

Park, C. Nonequilibrium hypersonic aerothermodynamics. New York a.o., 1990.

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41

Center, Lewis Research, ed. CFD for hypersonic propulsion. [Cleveland, Ohio: Lewis Research Center, 1991.

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42

CFD for hypersonic propulsion. [Cleveland, Ohio: Lewis Research Center, 1991.

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43

Basics of Aerothermodynamics. Springer, 2004.

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44

Museliak, Dora. Hypersonic Air Breathing Propulsion Technologies. Wiley & Sons, Incorporated, John, 2022.

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45

Museliak, Dora. Hypersonic Air Breathing Propulsion Technologies. Wiley & Sons, Incorporated, John, 2022.

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46

Bruno, Claudio. Airbreathing Hypersonic Propulsion: An Introduction. Springer, 2023.

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47

Museliak, Dora. Hypersonic Air Breathing Propulsion Technologies. Wiley & Sons, Incorporated, John, 2022.

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48

Museliak, Dora. Hypersonic Air Breathing Propulsion Technologies. Wiley & Sons, Incorporated, John, 2022.

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49

United States. National Aeronautics and Space Administration., ed. Advanced computational techniques for hypersonic propulsion. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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50

N, Tiwari S., Singh D. J, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics., eds. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Norfolk, Va: Old Dominion University Research Foundation, 1992.

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