is sharp trailing edge a stagnation point? -- CFD Online Discussion Forums

May 31, 2011, 16:35	is sharp trailing edge a stagnation point?	#1
Shenren_CN Member Shenren Xu Join Date: Jan 2011 Location: London, U.K. Posts: 67 Rep Power: 15	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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