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June 18, 2009, 23:15 |
NACA0012 meshing problem
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#1 |
New Member
parvez
Join Date: Jun 2009
Posts: 8
Rep Power: 17 |
HI friends,
I am new to the gambit. I am trying to mesh NACA0012 with chord length of 2.My farfields are 50C from the airfoil. I have followed the cornell tutorials. Everything goes well except the last part when I am trying to mesh the airfoil face its giving negative area(mesh is going inside the airfoil) and skewness >98. I am using MAP scheme to mesh the face. If you want I can send the dbs file. |
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June 19, 2009, 01:54 |
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#2 |
Super Moderator
Maxime Perelli
Join Date: Mar 2009
Location: Switzerland
Posts: 3,297
Rep Power: 41 |
post a picture of your issue, with a zoom in your issue.
If you enable the shade-option, is the interior of the airfoil also shaded?
__________________
In memory of my friend Hervé: CFD engineer & freerider |
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June 24, 2009, 00:49 |
meshing problem in NACA0012
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#3 |
New Member
parvez
Join Date: Jun 2009
Posts: 8
Rep Power: 17 |
Hi MAX,
I have attached the zoomed in(shaded) file of my problem. After Using shade option it shades only the outer part not the inside of the airfoil. |
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June 24, 2009, 01:46 |
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#4 |
Super Moderator
Maxime Perelli
Join Date: Mar 2009
Location: Switzerland
Posts: 3,297
Rep Power: 41 |
Try to split the outer surface along the x(x<0) axis.
And remesh both surfaces, it should help
__________________
In memory of my friend Hervé: CFD engineer & freerider |
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