On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure Gradient
Author:
Affiliation:
1. Polytechnic Institute of Brooklyn,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.2432
Reference9 articles.
1. The Laminar Boundary Layer on a Rotating Blade
2. Yuan, S. W., A Theoretical Investigation of the Temperature Field in the Laminar Boundary Layer on a Porous Flat Plate with Fluid Injection, Project Squid, Tech. Rep. No. 4, September5,1947.
3. Heat Transfer in Laminar Compressible Boundary Layer on a Porous Flat Plate with Fluid Injection
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