Use of Rouse's stability parameter in determining the critical layerheight of a laminar boundary layer
- 1 January 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (1) , 173-175
- https://doi.org/10.2514/3.5632
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Experimental observation of transition of the hypersonic boundary layer.AIAA Journal, 1969
- Boundary-layer transition on sharp cones at hypersonic Mach numbers.AIAA Journal, 1968
- Hypersonic boundary-layer transition data for a cold-wall slender coneAIAA Journal, 1965
- 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
- Stability and transition of a supersonic laminar boundary layer on an insulated flat plateJournal of Fluid Mechanics, 1960
- A General Stability Index for Flow Near Plane BoundariesJournal of the Aeronautical Sciences, 1945