Shock-wave-induced turbulent boundary-layer separation at hypersonicspeeds
- 20 January 1975
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- New Diagnostic Technique for the Study of Turbulent Boundary-Layer SeparationAIAA Journal, 1974
- Flowfield Measurements Using a Total Temperature Probe at Hypersonic SpeedsAIAA Journal, 1972
- Comparison of characteristics and shock capturing methods with application to the space shuttle vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Viscous interaction effects on a static pressure probe at m equals 6AIAA Journal, 1963