Expressions for predicting 3-D shock wave-turbulent boundary layer interaction pressures and heating rates
- 16 January 1978
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An experimental study of three-dimensional flow fields in an axial corner at Mach 3Published by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Three-Dimensional Separation for Interaction of Shock Waves with Turbulent Boundary LayersAIAA Journal, 1973
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966