Observations on the influence of ambient pressure on boundary-layer transition.
- 1 October 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (10) , 1907-1911
- https://doi.org/10.2514/3.4899
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- An investigation of radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Shock tunnel investigation of boundary-layer transition at M equals 5.5.AIAA Journal, 1967
- Hypersonic boundary-layer transition data for a cold-wall slender coneAIAA Journal, 1965
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961