Nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flow
- 12 July 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Artificially Induced Boundary-Layer Transition on Blunt-Slender Cones at Hypersonic SpeedsJournal of Spacecraft and Rockets, 1979
- Real-Gas Scale Effects on Shuttle Orbiter Laminar Boundary-Layer ParametersJournal of Spacecraft and Rockets, 1977
- Boundary-Layer Stability and TransitionAnnual Review of Fluid Mechanics, 1976
- Shock tunnel investigation of boundary-layer transition at M equals 5.5.AIAA Journal, 1967