Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds
- 1 June 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (6) , 1082-1090
- https://doi.org/10.2514/3.49919
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- Experiments on roughness effects on cone boundary-layer transition up to Mach 16.AIAA Journal, 1969
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- Observations on the influence of ambient pressure on boundary-layer transition.AIAA Journal, 1968
- Further experiments on transition reversal at hypersonic speeds.AIAA Journal, 1966
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- Stability and transition of a supersonic laminar boundary layer on an insulated flat plateJournal of Fluid Mechanics, 1960
- Experiments on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- On the Stability of the Boundary Layer Over a ConeJournal of the Aeronautical Sciences, 1950