Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic Velocities
- 1 July 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (7) , 441-448
- https://doi.org/10.2514/8.2688
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Direct Measurement of Supersonic Skin FrictionJournal of the Aeronautical Sciences, 1952
- The Compressible Boundary LayerJournal of the Aeronautical Sciences, 1952
- Simplified Treatment of the Turbulent Boundary Layer Along a Cylinder in Compressible FlowJournal of the Aeronautical Sciences, 1952
- The structure of the turbulent boundary layerMathematical Proceedings of the Cambridge Philosophical Society, 1951
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- Characteristics of the Turbulent Boundary Layer on a Flat Plate in Compressible Flow from Measurements of Friction in PipesJournal of the Aeronautical Sciences, 1950