Calculation of 3-D Shock Wave-Turbulent Boundary Layer Interactions Generated by Sharp Fins
- 1 January 1991
- book chapter
- Published by Springer Nature
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Laser skin friction measurements and CFD comparison of weak-to-strong swept shock/boundary-layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Skin friction measurements by laser interferometry in swept shock wave/turbulent boundary-layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Structure of supersonic turbulent flow past a sharp finAIAA Journal, 1987
- Three-dimensional shock wave turbulent boundary layer interaction for a 20 deg sharp fin at Mach 3Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Calculation of three-dimensional shock/turbulent boundary-layer interaction generated by sharp finAIAA Journal, 1985
- A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equationsAIAA Journal, 1984
- An experimental study of the interaction between a glancing shock wave and a turbulent boundary layerJournal of Fluid Mechanics, 1982
- Computation of three-dimensional turbulent separated flows at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- An experimental study of three-dimensional flow fields in an axial corner at Mach 3Published by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Mach 3 oblique shock wave/turbulent boundary layer interactions in three dimensionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976