Turbulent boundary-layer separation in front of a forward-facing step.
- 1 October 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (10) , 1746-1753
- https://doi.org/10.2514/3.4299
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Boundary layer separation in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Fluctuating Wall Pressure under a Separated Supersonic FlowThe Journal of the Acoustical Society of America, 1964
- SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLESAIAA Journal, 1963