Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of Attack
- 1 January 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (1) , 55-57
- https://doi.org/10.2514/8.2149
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- Das Umströmungsproblem bei inkompressiblen PotentialströmungenArchive of Applied Mechanics, 1948