On the Structure of Three-Dimensional Shock-Induced Separated Flow Regions
- 1 May 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (5) , 597-600
- https://doi.org/10.2514/3.61401
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Effect of Transition on Three-Dimensional Shock- Wave/Boundary-Layer InteractionAIAA Journal, 1972
- A Study of Hypersonic Corner Flow InteractionsAIAA Journal, 1971
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- Supersonic interference flow along the corner of intersecting wedges.AIAA Journal, 1967
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966