Prediction of skin-friction and heat transfer from compressible turbulent boundary layers in rocket nozzles
- 1 November 1978
- journal article
- Published by Elsevier in International Journal of Heat and Mass Transfer
- Vol. 21 (11) , 1403-1410
- https://doi.org/10.1016/0017-9310(78)90204-1
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Relationship between temperature and velocity profiles in a turbulent boundary layer along a supersonic nozzle with heat transferAIAA Journal, 1970
- Laminarization of a Turbulent Boundary Layer in Nozzle Flow—Boundary Layer and Heat Transfer Measurements With Wall CoolingJournal of Heat Transfer, 1970
- Heat transfer from boundary layers undergoing an acceleration induced reverse transitionAIChE Journal, 1970
- Approximate calculation of Reynolds analogy for turbulent boundary layer with pressure gradient.AIAA Journal, 1969
- An Aspect of Heat Transfer in Accelerating Turbulent Boundary LayersJournal of Heat Transfer, 1969
- Heat transfer to a turbulent boundary layer with varying free-stream velocity and varying surface temperature—an experimental studyInternational Journal of Heat and Mass Transfer, 1965
- A Comparison of Analytical and Experimental Local Heat Fluxes in Liquid-Propellant Rocket Thrust ChambersJournal of Heat Transfer, 1962