Influence of measured freestream disturbances on hypersonic boundary-layer transition
- 1 September 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (9), 1664-1670
- https://doi.org/10.2514/3.5962
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Discussion: “On Supersonic Wind Tunnels With Low Free-Stream Disturbances” (Morkovin, M. V., 1959, ASME J. Appl. Mech., 26, pp. 319–324)Journal of Applied Mechanics, 1960
- Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind TunnelsJournal of the Aeronautical Sciences, 1954
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950