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Multidisciplinary design optimization for aircraft wing using response surface method, genetic algorithm, and simulated annealing

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In terms of optimization algorithms, Response Surface Method, Genetic Algorithm, and Simulated Annealing are utilized to get global optimum. The optimization objective functions are minimizing weight and maximizing lift/drag. The design variables are aspect ratio, tapper ratio, sweepback angle. The optimization results demonstrate successful and desiable construction of MDO framework. |

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Multidisciplinary design optimization for aircraft wing using response surface method, genetic algorithm, and simulated annealing

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