Experimental investigations of the compressible turbulent boundary layer at very high reynolds numbers
- 1 April 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (4) , 631-638
- https://doi.org/10.2514/3.2939
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- SKIN FRICTION EXERTED BY A COMPRESSIBLE FLUID STREAM ON A FLAT PLATEAIAA Journal, 1963
- Turbulent Boundary-Layer Characteristics at Supersonic Speeds-Theory and ExperimentJournal of the Aeronautical Sciences, 1950