AeroExplore TLS Wing Optimization Challenge

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Baseline Design - Geometry
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dbusetto
dbusetto
Created

almost 9 years ago

Last modified

over 5 years ago

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geometries 3 Geometries
meshes 3 Meshes
simulations 3 Simulation setups
runs 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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Project History

AeroExplore TLS Wing Optimization Challenge by dbusetto | SimScale