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Airplane Wing Design Optimization with Stress Analysis

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Garva
Garva
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geometries 3 Geometriesmeshes 3 Meshessimulations 2 Simulation setupsruns 2 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

  • simscale

    simscale created this project

  • Garva

    Garva copied this project