Regimes and properties of three-dimensional separation flows initiated by skewed compression shocks
- 1 January 1982
- journal article
- Published by Springer Nature in Journal of Applied Mechanics and Technical Physics
- Vol. 23 (3) , 413-418
- https://doi.org/10.1007/bf00910085
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Properties of two- and three-dimensional separation flows at supersonic velocitiesFluid Dynamics, 1979
- Expressions for predicting 3-D shock wave-turbulent boundary layer interaction pressures and heating ratesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Mach 3 oblique shock wave/turbulent boundary layer interactions in three dimensionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- On the Structure of Three-Dimensional Shock-Induced Separated Flow RegionsAIAA Journal, 1976
- A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock WaveAIAA Journal, 1973