Which trailing edge is correct for meshing of aerofoils for CFX
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. http://i725.photobucket.com/albums/w...hsc/3dEDGE.jpg
Finite Thickness at trailing edge
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