On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure Gradient
- 1 October 1952
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 19 (10) , 705-712
- https://doi.org/10.2514/8.2432
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- The Laminar Boundary Layer on a Rotating BladeJournal 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