Turbulent heat-transfer and skin-friction measurements on a porous cone with air injection at high Mach numbers.
Author:
Affiliation:
1. General Electric Company, King of Prussia, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3627
Reference12 articles.
1. Bartle, E. R. and Leadon, B. M. "The effectiveness as a universal measure of mass transfer cooling for a turbulent boundary layer/' Proceedings of the 1962 Heat Transfer and Fluid Mechanics Institute (Stanford University Press, Stanford, Calif. 1962), pp.27-41.
2. Measurements of Skin Friction of the Compressible Turbulent Boundary Layer on a Cone with Foreign Gas Injection
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