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NACA0012 - Angle of Attack - Parametric Study - Copy

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siahyongchun88
siahyongchun88
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geometries 2 Geometriesmeshes 3 Meshessimulations 2 Simulation setupsruns 7 Results
About this project

Simple project studying NACA0012 symmetric airfoil under an angle of attack (aoa) range. The workflow utilizes the parametric capabilities of SimScale to study multiple design points/multiple aoa. Please check the following forum post for more information https://www.simscale.com/forum/t/parametric-angle-of-attack-aoa-study-for-airfoil-lift-and-drag-calculation/96408 - Copy

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Project History

  • itsavlidis

    itsavlidis created this project

  • siahyongchun88

    siahyongchun88 copied this project