Comparison of Supersonic Combustion Tests with Shock Tunnels, Flight and CFD-Reference-Cited by-同舟云学术

Comparison of Supersonic Combustion Tests with Shock Tunnels, Flight and CFD

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Steelant Johan,Mack Andreas,Hannemann Klaus,Gardner Anthony

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. 3Paull,A.,Alesi,H.,Anderson,S.,HyShotflightprogramandhowitwasdeveloped,AIAA2002-4939,2002

2. 5Gardner, A.D., Hannemann, K., Steelant, J., Paull, A. Ground Testing of the HyShot Supersonic Combustion Flight Experiment inHEG and Comparisonwith FlightData, AIAA 2004-3345, 2004

3. 7Adeli, R., Flow Filed Study due to a Supersonic Jet Exiting into a Supersonic Stream. Proceedings of 14thSTAB Symposium, Bremen, Germany,November16-18,2004

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