Some effects of roughness and variable entropy on transition at a Mach number of 8
- 23 January 1967
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Hypersonic boundary-layer transition data for a cold-wall slender coneAIAA Journal, 1965
- Shock curvature effect on the outer edge conditions of a laminar boundary layerAIAA Journal, 1963
- MEASUREMENTS OF PRESSURE DISTRIBUTION AND BOUNDARY-LAYER TRANSITION ON A HOLLOW-CYLINDER MODELPublished by Defense Technical Information Center (DTIC) ,1953
- MEASUREMENT OF BOUNDARY-LAYER TRANSITION ON A STANDARD MODEL TO DETERMINE THE RELATIVE DISTURBANCE LEVEL IN TWO SUPERSONIC WIND TUNNELSPublished by Defense Technical Information Center (DTIC) ,1953