Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion
Authors:
- 10 January 2005
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent FlowAIAA Journal, 1972