Set up your own cloud-native simulation in minutes.Start Simulating Now
AeroExplore TLS Wing Optimization Challenge
517 40
Statistics
5 Geometries 5 Meshes 6 Simulation setups 12 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.
Related Projects
Project History
AnnaFless created this project