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Aerodynamic heating is a large concern for high-speed flight vehicles. We use computational methods to analyze and predict the levels of heat transfer on a high-speed generic missile in order to facilitate future design of flight vehicles at hypersonic speeds.
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This page is a summary of: Aerodynamic Heating in the Gap Between a Missile Body and a Control Fin, Journal of Spacecraft and Rockets, July 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a35183.
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