A Provisional Analysis of Turbulent Boundary Layers with Injection
- 1 April 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (4), 255-260
- https://doi.org/10.2514/8.3322
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure GradientJournal of the Aeronautical Sciences, 1952
- Heat Transfer in Laminar Compressible Boundary Layer on a Porous Flat Plate with Fluid InjectionJournal of the Aeronautical Sciences, 1949
- Experimental Study of Cooling by Injection of a Fluid Through a Porous MaterialJournal of the Aeronautical Sciences, 1948