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Boeing Scientific Research Labs., Seattle, WA; University of Washington, Seattle
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Thayer, W. J., III; Corlett, R. C.
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Ignition and Combustion of a Transverse Hydrogen Jet in a Mach 2.5 Airstream.
Boeing Scientific Research Labs., Seattle, WA; University of Washington, Seattle
WSS/CI Paper 71-15,
Combustion Institute/Western States Section. Spring Meeting. April 26-27, 1971,
Denver, CO,
1-17 p.,
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Linan, A.
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Diffusion flames and Supersonic Combustion.
Instituto Nacionale de Tecnica Aeroespacial, Madrid, Spain
Office of Scientific Research, Arlington, VA,
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Experimental Investigation on Flameholding Mechanism and Combustion Performance in Hydrogen-Fueled Supersonic Combustors.
Chinese Academy of Sciences, Beijing, People's Republic of China; Case Western Reserve Univ., Cleveland, OH
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March 2002
Brailovsky, I.; Sivashinsky, G.
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On Propagation Limits in Porous Media Combustion.
Tel Aviv University, Ramat Aviv, Tel Aviv 69978, Israel
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Tien, J. H.; Stalker, R. J.
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Release of Chemical Energy by Combustion in a Supersonic Mixing Layer of Hydrogen and Air.
University of Queensland, Brisbane, Australis
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Mobus, H.; Gerlinger, P.; Bruggemann, D.
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Scalar and Joint Scalar-Velocity-Frequency Monte Carlo PDF Simulation of Supersonic Combustion.
Universitat Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany; Deutsches Zentrum fur Luft- und Raumfahrt, Stuttgart, Germany; Universitat Bayreuth, Germany
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Mitani, T.; Kouchi, T.
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Flame Structures and Combustion Efficiency Computed for a Mach 6 Scramjet Engine.
Japan Aerospace Exploration Agency, Japan; Tohoku Univ., Japan
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Numerical Study on Combustion of H2-O2 in a Supersonic Reactive Expansion in a Nozzle.
Amirkabir University of Technology, Hafez Ave, Tehran, Iran
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