Hypersonic boundary-layer transition in the presence of wind-tunnel noise.
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (12) , 2475-2476
- https://doi.org/10.2514/3.6541
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Hot wire measurements of freestream and shock layer disturbances.AIAA Journal, 1971
- Influence of measured freestream disturbances on hypersonic boundary-layer transitionAIAA Journal, 1970
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- Effects of freestream disturbances on boundary-layer transition.AIAA Journal, 1968
- Effects of freestream turbulence on boundary- layer transition.AIAA Journal, 1967
- Factors Affecting Transition Reynolds Numbers on Models in Supersonic Wind TunnelsJournal of the Aeronautical Sciences, 1954