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AeroExplore TLS Wing Optimization Challenge
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3 Geometries
2 Meshes
2 Simulation setups
2 Results
3 Geometries 2 Meshes 2 Simulation setups 2 ResultsAbout this project
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 created this project
Milad_Mafi copied this project