Unit Reynolds number effects on boundary-layer transition at Mach 6.
- 1 May 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (5) , 956
- https://doi.org/10.2514/3.4644
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Flat plate boundary layer transition at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965