A REVIEW OF HEAT TRANSFER IN SEPARATED AND REATTACHED FLOWS
- 29 June 1970
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 52 references indexed in Scilit:
- Heat-transfer measurements in the shock-induced flow separation region in a supersonic nozzle.AIAA Journal, 1968
- Free-flight base pressure and heating measurements on sharp and blunt cones in a shock tunnel.AIAA Journal, 1967
- A review of separated and reattaching flows with heat transferInternational Journal of Heat and Mass Transfer, 1967
- Heat transfer in supersonic separated flow over a two-dimensional backward-facing stepInternational Journal of Heat and Mass Transfer, 1966
- Momentum Transfer in Turbulent Separated Flow Past a Rectangular CavityJournal of Applied Mechanics, 1966
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- The Effect of Suction and Injection on the Heat Transfer and Flow in a Turbulent Separated AirflowJournal of Heat Transfer, 1966
- Separated flow behind a rearward-facing step with and without combustionAIAA Journal, 1965
- A study of laminar hypersonic cavity flowsAIAA Journal, 1964
- Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tubeAIAA Journal, 1964