AeroExplore TLS Wing Optimization Challenge

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Post-Processor Screenshot - PostProcessorScreenshot
Post-Processor Screenshot - PostProcessorScreenshot
PostProcessorScreenshot
2D
hollow - Geometry
Geometry
3D
final version - Geometry
Geometry
3D
wing thick first section and small rib - Geometry
Geometry
3D
Baseline Design - Geometry
Geometry
3D
Baseline Design V1 - Geometry
Geometry
3D
Baseline Design - Geometry
Geometry
3D
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janvanbaelen
janvanbaelen
Created

almost 9 years ago

Last modified

over 5 years ago

Statistics
geometries 6 Geometries
meshes 6 Meshes
simulations 5 Simulation setups
runs 6 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 janvanbaelen | SimScale