A study of recessed cavity flowfields for supersonic combustion applications
Author:
Affiliation:
1. Taitech, Inc., Beavercreek, OH
2. USAF, Research Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-938
Reference38 articles.
1. Vinogradov, V., Grachev, M., Petrov, M., and Sheechman, J. "Experimental Investigation of 2-D Dual Mode Scramjet with Hydrogen Fuel at Mach 4 . 6". AIAA Paper 90-5269, Oct. 1990.
2. Vinogradov, V., Kobigsky, S., and Petrov, M. "Experimental Investigation of Liquid Carbonhydrogen Fuel Combustion in Channel at Supersonic Velocities". AIAA Paper 92-3429, July 1992.
3. Romankov, O. N. and Starostin, F. I. "Design and Investigation of the Stand and Flying Scramjet Model Conceptions and Results ofExperiments". AIAA Paper 93-2447, June 1993.
4. McClinton, C., Roudakov, A., Semenov, V., and Kopehenov, V. "Comparative Flow Path Analysis and Design Assessment of an Axisymmetric Hydorgen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5". AIAA Paper 96-4571, Nov. 1996.
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