Characteristics of the Turbulent Boundary Layer on a Flat Plate in Compressible Flow from Measurements of Friction in Pipes
- 1 September 1950
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 17 (9) , 573-584
- https://doi.org/10.2514/8.1726
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Extended Applications of the Hot-Wire AnemometerReview of Scientific Instruments, 1947
- Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1938
- Widerstand von Platte und Rohr bei hohen Reynoldsschen ZahlenArchive of Applied Mechanics, 1930