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AeroExplore TLS Wing Optimization Challenge
Statistics
4 Geometries
4 Meshes
3 Simulation setups
3 Results
About 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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by simscalesimscale
Project History
vourname createdthis project
almost 9 years ago
pcid_escobar copied this project
almost 9 years ago