Flow characteristics about concave conic forebodies at high Mach number
- 20 January 1975
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Turbulent boundary-layer separation in front of a forward-facing step.AIAA Journal, 1967
- Leading-Edge Separation of Laminar Boundary Layers in Supersonic FlowJournal of the Aerospace Sciences, 1961