Shock Impingement Caused by Boundary-Layer Separation Ahead of Blunt Fins
- 1 October 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (10) , 1363-1364
- https://doi.org/10.2514/3.50590
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Shock Interference Bell Aerospace, Heating in Hypersonic FlowsAIAA Journal, 1972
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- Fluctuating Pressures Induced by Three-Dimensional ProtuberancesThe Journal of the Acoustical Society of America, 1970