Supersonic boundary-layer transition - Effects of roughness and freestream disturbances
- 1 May 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (5) , 797-803
- https://doi.org/10.2514/3.6278
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Measurements and correlations of transition Reynolds numbers on sharp slender cones at high speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Experiments on roughness effects on cone boundary-layer transition up to Mach 16.AIAA Journal, 1969
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- Boundary-layer transition at supersonic speeds - Roughness effects with heat transfer.AIAA Journal, 1968
- Hypersonic laminar boundary-layer transition on 8-foot-long, 10 deg cone, M sub 1 equals 9.1-16.AIAA Journal, 1967
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flowsJournal of Fluid Mechanics, 1962