A Program for Transition Research
- 1 March 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (3) , 261-265
- https://doi.org/10.2514/3.49690
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Wind tunnel experiments relating to supersonic and hypersonic boundary layer transitionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Development of a high Reynolds number quiet tunnel for transition researchPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- On the application of linear stability theory to the problem of supersonic boundary-layer transitionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Influence of measured freestream disturbances on hypersonic boundary-layer transitionAIAA Journal, 1970
- Effect of boundary-layer transition on vehicle dynamicsJournal of Spacecraft and Rockets, 1969
- 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
- Observations on the influence of ambient pressure on boundary-layer transition.AIAA Journal, 1968
- Stability and transition of a supersonic laminar boundary layer on an insulated flat plateJournal of Fluid Mechanics, 1960
- Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic FlowJournal of the Aeronautical Sciences, 1954