The Effect of Mass Transfer on the Compressible Turbulent Boundary-Layer Skin Friction and Heat Transfer
- 1 June 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (6) , 404-410
- https://doi.org/10.2514/8.3050
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic VelocitiesJournal of the Aeronautical Sciences, 1953
- On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure GradientJournal of the Aeronautical Sciences, 1952
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- Heat Transfer in Laminar Compressible Boundary Layer on a Porous Flat Plate with Fluid InjectionJournal of the Aeronautical Sciences, 1949
- The Mechanics of Viscous FluidsPublished by Springer Nature ,1935