Induced boundary-layer transition at supersonic speeds - Combined effects of roughness and free-stream disturbances
- 4 May 1970
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Boundary-layer transition at supersonic speeds - Roughness effects with heat transfer.AIAA Journal, 1968
- Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flowsJournal of Fluid Mechanics, 1962