A second-order weak interaction expansion for moderately hypersonic flow past a flat plate.
- 1 October 1967
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (10) , 1915-1917
- https://doi.org/10.2514/3.4338
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)Journal of the Aerospace Sciences, 1962
- The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aerospace Sciences, 1960
- An Experimental Investigation of Leading-Edge Shock-Wave - Boundary-Layer Interaction at Mach 5.8Journal of the Aeronautical Sciences, 1957