A comparison of planar and conical boundary layer stability and transition at a Mach number of 8
- 24 June 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Prediction and control of transition in supersonic and hypersonic boundary layersAIAA Journal, 1989
- Boundary-layer transition on a cone and flat plate at Mach 3.5AIAA Journal, 1989
- Growth of disturbances in a laminar boundary layer at Mach 3Physics of Fluids A: Fluid Dynamics, 1989
- On nonlinear aspects of hypersonic boundary-layer stabilityAIAA Journal, 1988
- Linear Stability Theory and the Problem of Supersonic Boundary- Layer TransitionAIAA Journal, 1975
- Boundary-Layer Transition on Supersonic Cones in an Aeroballistic RangeAIAA Journal, 1975
- Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High SpeedsAIAA Journal, 1971
- Stability and transition of a supersonic laminar boundary layer on an insulated flat plateJournal of Fluid Mechanics, 1960
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949