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October 19, 2010, 23:14 |
Trimmer and Volume Shapes
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#1 |
New Member
Ji-nam, Kim
Join Date: Oct 2010
Posts: 3
Rep Power: 15 |
Hi,
I'm trying to analyze the flow around NACA0012 airfoil in 2D. The length of freestream field is 15.1m and chord length of airfoil is 1m. I used trimmer and blocks in volume shapes function for generating mesh, but it wasn't good. Cell size is not uniform that I thought. How can I generate a uniform sized mesh? Please teach me. |
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October 20, 2010, 13:56 |
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#2 |
Member
John
Join Date: Aug 2009
Posts: 92
Rep Power: 16 |
It tends to do that when you cut a 2d plane. Make sure your cut plane is exactly in the z=0 plane.
Otherwise, it shouldn't be a problem. Use cell quality remediation when running the simulation. |
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October 21, 2010, 12:04 |
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#3 |
Senior Member
Joern Beilke
Join Date: Mar 2009
Location: Dresden
Posts: 497
Rep Power: 20 |
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March 11, 2011, 22:42 |
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#4 | |
New Member
Mahbub Islam
Join Date: Mar 2010
Location: Bangladesh
Posts: 24
Rep Power: 16 |
JBeilke
Hope you are doing well. I am looking for some help from you. Currently I am working on 3D airfoil (NACA 2412) simulation. I am new in star CCM. Can you please send me any tutorial/ or required steps for VOLUME MESHING around 3D airfoil? I am passing my sleepless nights to get a way, but not found anything yet. It would be a great help for me - if anybody would give me some guidelines on how to mesh upon .IGES geometry imported in star ccm. my mail add: mahbub.me.buet@gmail.com Thank you in advance. Quote:
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