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AeroExplore TLS Wing Optimization Challenge

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AlejandroEA
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Weight is one of the most critical parameters in aircraft design. In this challenge, 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 maximum allowable deflection (+ y direction) of .90 meters.

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Project History

  • AnnaFless

    AnnaFless created this project

  • AlejandroEA

    AlejandroEA copied this project