Experimental observation of transition of the hypersonic boundary layer.
- 1 February 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (2) , 257-263
- https://doi.org/10.2514/3.5083
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Use of a pulse heated fine wire probe for the measurement of total temperature in shock driven facilitiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Roughness, bluntness, and angle-of-attack effects on hypersonic boundary-layer transitionJournal of Fluid Mechanics, 1966
- Hypersonic boundary-layer transition data for a cold-wall slender coneAIAA Journal, 1965
- Flat plate boundary layer transition at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flowsJournal of Fluid Mechanics, 1962