Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent Flow
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50348
Reference15 articles.
1. Active cooling heat protection.
2. A comparison between film cooling and transpiration cooling systems in high speed flow
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