On the structure of three-dimensional shock-induced separated flow regions
- 26 January 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Flowfield Measurements in an Asymmetric Axial Corner at M -12.5AIAA Journal, 1974
- Supersonic Interaction in the Corner of Intersecting Wedges at High Reynolds NumbersAIAA Journal, 1972
- Effect of Transition on Three-Dimensional Shock- Wave/Boundary-Layer InteractionAIAA Journal, 1972
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966