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[ICEM] Not getting shell meshing

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Old   May 15, 2012, 12:58
Default Not getting shell meshing
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Sijal Ahmed Memon (turboenginner@gmail.com)
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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 :


Last edited by Far; May 15, 2012 at 13:02. Reason: pics
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Old   May 17, 2012, 14:23
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Far you have great experience in Structured meshing and you are facing problem in simple unstructured meshing, feels odd
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
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Old   May 17, 2012, 14:30
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Actually this was done to record the youtube tutorials, and finally I solved the problem. Now this problem is solved. Wing body tutorial with tetra + prism


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