Unusual boundary-layer transition results on cones in hypersonic flow.
- 1 April 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (4) , 660-664
- https://doi.org/10.2514/3.5183
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Unit Reynolds number effects on boundary-layer transition at Mach 6.AIAA Journal, 1968
- Some effects of roughness and variable entropy on transition at a Mach number of 8Published by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Hypersonic boundary-layer transition data for a cold-wall slender coneAIAA Journal, 1965
- JET NOISEAIAA Journal, 1963
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- Recent Studies on the Effect of Cooling on Boundary-Layer Transition at Mach 4Journal of the Aerospace Sciences, 1961