Development of a double-oblique-shock Scramjet model in a shock tunnel
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (4) , 258-263
- https://doi.org/10.2514/3.44265
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- DEVELOPMENT OF A DOUBLE-OBLIQUE-SHOCK SCRAMJET MODEL IN A SHOCK TUNNELPublished by Defense Technical Information Center (DTIC) ,1969
- Flat plate turbulent heat transfer at hypervelocities.Journal of Spacecraft and Rockets, 1966
- CALIBRATION OF THE SHOCK TUNNEL COMPONENT OF COUNTERFLOW RANGE (I) AT MACH 7.5Published by Defense Technical Information Center (DTIC) ,1966
- A THEORETICAL ANALYSIS OF NON-EQUILIBRIUM HYDROGEN-AIR REACTIONS IN FLOW SYSTEMSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963