A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flow
- 10 July 1978
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Boundary-layer displacement and leading edge bluntness effects on attached and separated laminar boundary layers in a compression corner.I - Theoretical studyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Supersonic separated and reattaching laminar flows- i - general theory and application to adiabatic boundary layer-shock wave interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952