Effect of Mach number and Reynolds number on a normal shock-wave/turbulent boundary-layer interaction
Authors:
- 23 July 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Comparison of multiequation turbulence models for several shock-separated boundary-layer interaction flows1978
- Numerical Investigation of Turbulence Models for Shock-Separated Boundary-Layer FlowsAIAA Journal, 1978
- A normal shock-wave turbulent boundary-layer interaction at transonic speeds1976
- Transonic flow about a thick circular-arc airfoil1975