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Boundary Conditions for Incomp flow at various aoa

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Old   January 17, 2020, 16:00
Default Boundary Conditions for Incomp flow at various aoa
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Pierce
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I have a rectangular block with an airfoil solving for viscous in-compressible flow, it solves nicely when velocity is boundary normal, where I have a velocity inlet walls and a pressure outlet. However, I now want to solve it for several angles of attack and was wondering how to set appropriate boundary conditions here. Thanks, Pierce
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