An investigation of the effect of suction on hypersonic laminar boundary-layer separation.
- 1 February 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (2) , 239-243
- https://doi.org/10.2514/3.4484
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.AIAA Journal, 1968
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964
- Some Experiments on Hypersonic Separated FlowsARS Journal, 1962