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Aerodynamic heating on a flared cone at Mach 6 is studied. The Stanton number and recovery factor are calculated using the experimentally measured wall temperature.
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This page is a summary of: Heat Transfer and Recovery Factor of Aerodynamic Heating on a Flared Cone, AIAA Journal, November 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060937.
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