A two-layer calculation for the initial interaction region of an unseparated supersonic turbulent boundary layer with a ramp
- 14 January 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Turbulent hypersonic flow at a wedge-compression cornerJournal of Fluid Mechanics, 1972
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959