An Experimental Model for the Sharp Flat Plate in Rarefied Hvnersonic Flow
- 1 September 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (9), 1580-1587
- https://doi.org/10.2514/3.55283
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Aerodynamic properties of some simple bodies in the hypersonic transition regime.AIAA Journal, 1966
- Structure of the boundary layer at the leading edge of a flat plate in hypersonic slip flowAIAA Journal, 1964
- Slip flow and hypersonic boundary layersAIAA Journal, 1964
- CRITERION FOR SLIP NEAR THE LEADING EDGE OF A FLAT PLATE IN HYPERSONIC FLOWAIAA Journal, 1963
- Structure of a Plane Shock LayerPhysics of Fluids, 1962
- Heat Transfer to Flat Plate in High Temperature Rarefied Ultrahigh Mach Number FlowARS Journal, 1962
- Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic FlowJournal of the Aerospace Sciences, 1961
- Hypersonic Shock Wave-Boundary Layer Interaction and Leading Edge SlipARS Journal, 1960