Experimental studies on the lip shock
- 23 January 1967
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Observations of turbulent reattachment behind an axisymmetric downstream-facing step in supersonic flow.AIAA Journal, 1966
- Estimation of the strength of lip shock.AIAA Journal, 1966
- Theory of laminar near wake of blunt bodies in hypersonic flow.AIAA Journal, 1965
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965