Direct measurements of wall shear stress by buried wire gages in a shock-wave boundary-layer interaction region
- 27 June 1977
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Experiments on transonic and supersonic turbulent boundary-layer separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Modifications of the law of the wall and algebraic turbulence modelling for separated boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- A normal shock-wave turbulent boundary-layer interaction at transonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Shock wave-turbulent boundary layer interaction at a high Reynolds number, including separation and flowfield measurementsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Shock-wave-induced turbulent boundary-layer separation at hypersonicspeedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Wall Shear in Strongly Retarded and Separated Compressible Turbulent Boundary LayersAIAA Journal, 1974
- Shock wave-turbulent boundary layer interactions in rectangular channelsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Flow Angle and Shear Stress Measurements Using Heated Films and WiresJournal of Basic Engineering, 1972