Combustor data bases for hypersonic airbreathing propulsion systems

Author:

McDaniel, Jr. James1

Affiliation:

1. Virginia, Univ., Charlottesville

Publisher

American Institute of Aeronautics and Astronautics

Reference48 articles.

1. Computational Investigation of Shock-Enhanced Mixing and Combustion

2. Billig,F.S."Propulsion Systemsfrom TakeofftoHigh-SpeedFlight,"Progressin AstronauticsandAeronautics.Vol. 137, 1991, A.Richard Seebass,Editor-in-Chief, p. 69.

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2. Irregular Phenomena of Shock Reflection Transition in a Conventional Supersonic Wind Tunnel;AIAA Journal;2003-06

3. Effects of Ramp Side Angle in Supersonic Mixing;AIAA Journal;2003-06

4. Dual-mode flowfield in scramjet combustor;35th AIAA Thermophysics Conference;2001-06-11

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