Calculations of turbulent shear stress in supersonic turbulent boundary layer zero and adverse pressure gradient flow
- 10 January 1973
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Supersonic Turbulent Boundary Layer in Adverse Pressure Gradient. Part I: The ExperimentAIAA Journal, 1972
- Experimental and theoretical investigations of temperature distributions in supersonic boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- Mixing length and kinematic eddy viscosity in a compressible boundary layer.AIAA Journal, 1968