The Effect of Mass Transfer on the Compressible Turbulent Boundary-Layer Skin Friction and Heat Transfer
Author:
Affiliation:
1. Consolidated Vultee Aircraft Corporation,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3050
Reference11 articles.
1. Heat Transfer in Laminar Compressible Boundary Layer on a Porous Flat Plate with Fluid Injection
2. On Heat Transfer over a Sweat-Cooled Surface in Laminar Compressible Flow with a Pressure Gradient
3. Turbulent Boundary Layer in Compressible Fluids
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