Incipient separation pressure rise for a Mach 3.8 turbulent boundarylayer.
- 1 May 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (5) , 761-763
- https://doi.org/10.2514/3.6829
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Turbulence measurements in a compressible boundary layer subjected to a shock-wave-induced adverse pressure gradientPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973