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Shenren Xu
Join Date: Jan 2011
Location: London, U.K.
Posts: 67
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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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