A modified wall wake velocity profile for turbulent compressible boundary layers.
- 1 June 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 10 (6), 381-383
- https://doi.org/10.2514/3.44376
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Turbulence measurements in a compressible boundary layer subjected to a shock-wave-induced adverse pressure gradientPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Turbulent properties of a compressible boundary layer.AIAA Journal, 1972
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- Use of Coles' universal wake function for compressible turbulent boundary layersJournal of Aircraft, 1970
- Mixing length and kinematic eddy viscosity in a compressible boundary layer.AIAA Journal, 1968
- The law of the wake in the turbulent boundary layerJournal of Fluid Mechanics, 1956
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951