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is sharp trailing edge a stagnation point?

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Old   May 31, 2011, 16:35
Default is sharp trailing edge a stagnation point?
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Shenren Xu
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For example, a NACA0012 airfoil with sharp trailing edge of finite angle (not a cusp). If incoming flow is subsonic (isentropic), can the trailing edge be assumed to be a stagnation point?

If I use a node-based, instead of cell-centered, finite volume Euler solver, how to impose weak boundary condition then?

Thanks.
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