Which trailing edge is correct for meshing of aerofoils for CFX -- CFD Online Discussion Forums

May 10, 2009, 13:45	Which trailing edge is correct for meshing of aerofoils for CFX	#1
LSC Member LSC Join Date: May 2009 Posts: 58 Rep Power: 17	pls shed some light as to which trailing edge should I use during meshing. I need to run the simulations in CFX. I encountered problem sweeping for the case with a common vertex for Upper and Lower surface at the trailing edge. The error message goes like this: "Error: ACIS error 95034: Attempt to sweep a non-manifold face". Previously I have no problem sweeping for the case of a finite thickness at the Trailing edge. Trailing edge with common vertex. Finite Thickness at trailing edge Please advice..

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