RELIABLE MULTIDISCIPLINARY DESIGN OF A SUPERSONIC NOZZLE USING MULTIFIDELITY SURROGATES (AIAA 2017-3826)
AIAA/ISSMO multidisciplinary analysis and optimization (Conference)
2017-01-01
21 pages
Conference paper
English
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FRAMEWORK FOR MULTIFIDELITY AEROELASTIC VEHICLE DESIGN OPTIMIZATION (AIAA 2017-4322)
British Library Conference Proceedings | 2017
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