Measurements and correlations of transition Reynolds numbers on sharp slender cones at high speeds
- 29 June 1970
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- Transition experiments on a flat plate at subsonic and supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Observations on the influence of ambient pressure on boundary-layer transition.AIAA Journal, 1968
- Contoured nozzle design and evaluation for hotshot wind tunnelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Some effects of roughness and variable entropy on transition at a Mach number of 8Published by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Effect of spherical roughness on hypersonic boundary-layer transition.AIAA Journal, 1966
- Flat plate boundary layer transition at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- BOUNDARY LAYER TRANSITION- FREESTREAM TURBULENCE AND PRESSURE GRADIENT EFFECTSAIAA Journal, 1963
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aerospace Sciences, 1960