Two-stream, supersonic, wake flowfield behind a thick base. I - General features
- 1 August 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (8) , 2039-2046
- https://doi.org/10.2514/3.11177
Abstract
No abstract availableThis publication has 29 references indexed in Scilit:
- Turbulent boundary-layer properties downstream of the shock-wave/boundary-layer interactionAIAA Journal, 1987
- Compressible separated flowsAIAA Journal, 1986
- Interaction between two compressible, turbulent free shear layersAIAA Journal, 1986
- A study of compressible turbulent reattaching free shear layersAIAA Journal, 1986
- A Review of Research on Subsonic Turbulent Flow ReattachmentAIAA Journal, 1981
- Effect of finite-size probe volume upon laser Doppler anemometer measurementsAIAA Journal, 1976
- A modified wall wake velocity profile for turbulent compressible boundary layers.Journal of Aircraft, 1973
- Supersonic Turbulent Boundary Layer in Adverse Pressure Gradient. Part 11: Data AnalysisAIAA Journal, 1972
- Correlation between turbulent shear stress and turbulent kinetic energyAIAA Journal, 1970
- Use of turbulent kinetic energy in free mixing studiesAIAA Journal, 1970