Experiments on roughness effects on cone boundary-layer transition up to Mach 16.
Authors:
- 1 March 1969
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (3) , 465-470
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Observations on the influence of ambient pressure on boundary-layer transition.AIAA Journal, 1968
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Laminar heat transfer to spherically blunted cones at hypersonic conditionsAIAA Journal, 1964
- Status of Development of Hotshot Tunnels at the Aedc1964
- Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)Journal of the Aerospace Sciences, 1962
- Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flowsJournal of Fluid Mechanics, 1962
- The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aerospace Sciences, 1960
- Transition-Point Fluctuations in Supersonic FlowJournal of the Aeronautical Sciences, 1954