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Airplane Wing Design Optimization – Stress Analysis

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jourada
jourada
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geometries 3 Geometriesmeshes 0 Meshessimulations 0 Simulation setupsruns 0 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

  • jourada

    jourada copied this project