[ICEM] NACA RM L51E25 Mesh Generation in ICEM 14

sarodesr · August 6, 2013, 07:40

Hi,

I am bit new to ansys and wanted to run simulation for NACA RM L51E25 profile in fluent. I have used solidworks 2010 for geomerty (parasolid) and imported it into ICEM. everything goes fine except wing part. I have tried unstructured mesh but it wont work. Please let me know how to mesh Wing part.

Thanks in advance!

Regards,

Sarang

Far · August 7, 2013, 04:36

Try ICEM Hexa.

diamondx · August 7, 2013, 13:02

or use a smaller size , that is too coarse .

sarodesr · August 14, 2013, 06:14

Thank you very much!
Got it by decreasing size

, and now trying ICEM Hexa.

regards,

Sarang

August 7, 2013, 13:02		#3
diamondx Super Moderator Ghazlani M. Ali Join Date: May 2011 Location: Tokyo, Japan Posts: 1,385 Blog Entries: 23 Rep Power: 29	or use a smaller size , that is too coarse . __________________ Regards, New to ICEM CFD, try this document --> https://goo.gl/KAOIwm Ali

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August 7, 2013, 04:36		#2
Far Senior Member Sijal Join Date: Mar 2009 Location: Islamabad Posts: 4,558 Blog Entries: 6 Rep Power: 54	Try ICEM Hexa.

August 14, 2013, 06:14		#4
sarodesr New Member Sarang Join Date: Jul 2013 Posts: 13 Rep Power: 13	Thank you very much! Got it by decreasing size , and now trying ICEM Hexa. regards, Sarang