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Old   October 19, 2010, 23:14
Default Trimmer and Volume Shapes
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Ji-nam, Kim
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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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Old   October 20, 2010, 13:56
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John
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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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Old   October 21, 2010, 12:04
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Joern Beilke
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http://www.beilke-cfd.de/naca_0012_5_degree.sim.gz

It needs some rotation and scaling.
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Old   March 11, 2011, 22:42
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Mahbub Islam
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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.


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Originally Posted by JBeilke View Post
http://www.beilke-cfd.de/naca_0012_5_degree.sim.gz

It needs some rotation and scaling.
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