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VDI Wing Optimization Exercise - Student Version

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Weight is one of the most critical parameters in aircraft design. In this exercise, you will be provided with a baseline design of an aluminum aircraft wing. Your objective is to reduce the weight of the wing without exceeding the yield stress and maximum allowable deflection

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  • AnnaFless

    AnnaFless created this project

  • andres2203

    andres2203 copied this project