A theory for two-dimensional supersonic turbulent base flows
- 20 January 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
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- Another estimate of the similarity parameter for turbulent mixing.AIAA Journal, 1968
- Experimental studies on the lip shock.AIAA Journal, 1968
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- Comments on "Review of Recent Developments in Turbulent Supersonic Base Flow"AIAA Journal, 1966
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- An Experimental Investigation of Base Flows at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1961
- An Investigation of Separated Flows - Part I: The Pressure FieldJournal of the Aerospace Sciences, 1961
- A Theory for Base Pressures in Transonic and Supersonic FlowJournal of Applied Mechanics, 1956