Prism problem in ICEM CFD at inlet and outlet
Hello,
Relatively new user looking at meshing a case for exterior aerodynamics of streamlined vehicles, in particular a wind tunnel validation study. My problem is prism generation on the floor boundary not running to the inlet and outlets correctly. This causes the prisms to decrease to a small point which ultimately leads to terrible quality cells. Please see the attached picture that I hope explains my issue. I am aware that the mesh appears quite coarse - I am just trying to eliminate the prism problem. Any help or advice welcome. http://i62.tinypic.com/295siac.jpg Cheers! Ben |
If your geometry is not very complex, try using blocking...then you will have easy time with the prism layer
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Hi,
check the value of Max Prism Angle parameter under Global Prism Mesh Parameters. If you have 90 or less that may cause the error |
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