Flap turbulent heating characteristics obtained from a hypersonic shock tunnel
- 21 June 1971
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- A REVIEW OF HEAT TRANSFER IN SEPARATED AND REATTACHED FLOWSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Hypersonic turbulent boundary-layer separations at high Reynolds numbers.Journal of Spacecraft and Rockets, 1969
- Correlation of peak heating for reattachment of separated flows.Journal of Spacecraft and Rockets, 1968
- Turbulent heat transfer associated with control surface at Mach 6.AIAA Journal, 1968
- Correlation of turbulent heat flux to deceleration flaps in supersonic flow.Journal of Spacecraft and Rockets, 1968
- Heat-transfer measurements of entry cones with maneuvering surfacesAIAA Journal, 1965
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964