Correlations of Peak Heating in Shock Interference Regions at Hypersonic Speeds
- 1 August 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 9 (8) , 621-623
- https://doi.org/10.2514/3.61760
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Transition in Compressible Free Shear LayersJournal of Spacecraft and Rockets, 1972
- Shock wave-turbulent boundary layer interaction in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- Changes in heat transfer from turbulent boundary layers interacting with shock waves and expansion wavesAIAA Journal, 1970
- Correlation of peak heating for reattachment of separated flows.Journal of Spacecraft and Rockets, 1968
- Correlation of turbulent heat flux to deceleration flaps in supersonic flow.Journal of Spacecraft and Rockets, 1968