Transformation theory for the adiabatic compressible turbulent boundary layer with pressure gradient
- 20 January 1969
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- NOL HYPERSONIC TUNNEL NO. 4, RESULTS 7: EXPERIMENTAL INVESTIGATION OF TURBULENT BOUNDARY LAYERS IN HYPERSONIC FLOWPublished by Defense Technical Information Center (DTIC) ,1955
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