Three-dimensional shock wave turbulent boundary layer interaction for a 20 deg sharp fin at Mach 3
- 24 March 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The flowfield structure of the 3-D shock wave - Boundary layer interaction generated by a 20 deg sharp fin at Mach 3Published by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Thin-layer approximation and algebraic model for separated turbulentflowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A modified wall wake velocity profile for turbulent compressible boundary layers.Journal of Aircraft, 1973
- The prediction of laminarization with a two-equation model of turbulenceInternational Journal of Heat and Mass Transfer, 1972