Wind tunnel experiments relating to supersonic and hypersonic boundary layer transition
- 30 January 1974
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Turbulent bursts and rings on a cone in helium at Me = 7.6.AIAA Journal, 1972
- Cone Transitional Boundary-Layer Structure at Me = 14AIAA Journal, 1972
- 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
- Use of moderate-length hot wires to survey a hypersonic boundary layer.AIAA Journal, 1967
- Solution of the Boltzmann equation for expanding flows.AIAA Journal, 1967
- 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
- Stability and transition of a supersonic laminar boundary layer on an insulated flat plateJournal of Fluid Mechanics, 1960
- An experiment on the stability of hypersonic laminar boundary layersJournal of Fluid Mechanics, 1960