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Far May 15, 2012 12:58

Not getting shell meshing
I am trying to reproduce the wing - body tutorial given in ANSYS ICEM CFD 14 training material. Every things else is fine including density box, volume meshing and smoothing. But I am not able to get the the shell meshing as given in the included file. At leading edge autoblock is used as instructed in tutorial.

My mesh seems like this :

cfd seeker May 17, 2012 14:23

Far you have great experience in Structured meshing and you are facing problem in simple unstructured meshing, feels odd :o
well i exactly dont know the solution but once i came across this problem for another geometry but when i changed my file import from acis to parasolid or vice-versa(as i dont remember exactly), the problem gets solved but it was just a good luck :)

Far May 17, 2012 14:30

Actually this was done to record the youtube tutorials, and finally I solved the problem. Now this problem is solved.

Rigth now I am working on the youtube clip regarding NACA 0015 wing with hexa meshing.

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