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AeroExplore TLS Wing Optimization Challenge
536
40
Statistics
5 Geometries
5 Meshes
6 Simulation setups
12 Results
5 Geometries 5 Meshes 6 Simulation setups 12 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.
