An examination of blunt fin-induced shock wave turbulent boundary layer interactions
- 15 January 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A detailed study of attached and separated compression corner flowfields in high Reynolds number supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Three dimensional shock wave turbulent boundary layer interactions -A parametric study of blunted fin-induced flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Reynolds Number Effects on Shock-Wave Turbulent Boundary-Layer InteractionsAIAA Journal, 1977
- A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock WaveAIAA Journal, 1973
- ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK.Published by Office of Scientific and Technical Information (OSTI) ,1968
- Hypersonic turbulent boundary-layer interference heat transfer in vicinity of protuberancesAIAA Journal, 1965