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We proposed a better configration for hypersonic reentry aircraft in order for smaller drag and heat transfer. We also optimized it using the Kriging model.
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This page is a summary of: Multiobjective Design Optimization of Hypersonic Combinational Novel Cavity and Opposing Jet Concept, Journal of Spacecraft and Rockets, May 2017, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a33801.
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