Boundary layer separation in hypersonic flow
- 24 January 1966
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- INVESTIGATION OF FLOW SEPARATION ON A TWO-DIMENSIONAL FLAT PLATE HAVING A VARIABLE-SPAN TRAILING-EDGE FLAP AT M INFINITY EQUAL TO 3 AND 5Published by Defense Technical Information Center (DTIC) ,1964
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964
- Some Experiments on Hypersonic Separated FlowsARS Journal, 1962
- Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic FlowJournal of the Aerospace Sciences, 1961
- A Semiempirical Relation for Laminar SeparationJournal of the Aerospace Sciences, 1959
- A Theoretical Investigation of Laminar Separation in Supersonic FlowJournal of the Aeronautical Sciences, 1957