Boundary-Layer Transition on Supersonic Cones in an Aeroballistic Range
- 1 March 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (3) , 270-277
- https://doi.org/10.2514/3.49692
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
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- Three-dimensional laminar boundary-layer transition on a sharp 8 degcone at Mach 10AIAA Journal, 1970
- Effect of uncooled leading edge on cooled-wall hypersonic flat-plateboundary-layer transitionAIAA Journal, 1970
- Stability theory as a guide to the evaluation of transition data.AIAA Journal, 1969
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- On the Many Faces of TransitionPublished by Springer Nature ,1969
- Observations on the influence of ambient pressure on boundary-layer transition.AIAA Journal, 1968
- Effects of slight nose bluntness and roughness on boundary-layer transition in supersonic flowsJournal of Fluid Mechanics, 1962
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961