Turbulent Boundary-La yer Shear Stress Distributions for Compressible Adverse Pressure Gradient Flow
- 1 March 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (3) , 375-376
- https://doi.org/10.2514/3.49236
Abstract
No abstract availableKeywords
This publication has 2 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
- Supersonic Turbulent Boundary Layer in Adverse Pressure Gradient. Part I: The ExperimentAIAA Journal, 1972