Angle of attack and leading edge effects on the flow about a flat plate at Mach number 18.
- 1 May 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (5) , 848-852
- https://doi.org/10.2514/3.4608
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- An Experimental Model for the Sharp Flat Plate in Rarefied Hvnersonic FlowAIAA Journal, 1966
- Condensation studies in hotshot tunnelsAIAA Journal, 1964
- AIR CONDENSATION IN A HYPERSONIC WIND TUNNELAIAA Journal, 1963
- Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic FlowJournal of the Aerospace Sciences, 1961