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Airplane Wing Design Optimization with Stress Analysis

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Airplane Wing Design Optimization with Stress Analysis image
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4uad
4uad
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geometries 3 Geometriesmeshes 3 Meshessimulations 6 Simulation setupsruns 6 Results
About this project

This project involves the simulation of stress analysis of an aircraft wing. There are total 6 comparison configurations with 3 different models and two different load definition.

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Project History

  • ahmedhussain18

    ahmedhussain18 created this project

  • 4uad

    4uad copied this project