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-   -   Question about meshing 2D airfoil in icemcfd (http://www.cfd-online.com/Forums/ansys/76465-question-about-meshing-2d-airfoil-icemcfd.html)

cxcxcx0505 May 26, 2010 09:18

Question about meshing 2D airfoil in icemcfd
 
I am doing the meshing for 2D airfoil naca0012 in icem cfd, the grid came out is not nice in the leading edge because of the lack of formatted point data at the frontal part.I want to build the data using C++,I know the equation,but I dunno how to make the steps for variable-X,the data found from internet is
something like
1.00000 0.00126 0
0.99280 0.00227 0
0.97989 0.00405 0
0.96352 0.00627 0
0.94455 0.00878 0
0.92350 0.01151 0
0.90075 0.01438 0
0.87658 0.01735 0
......
I want to make more precise point,do anyone know how to solve this?
Thanks.

ingmecc May 26, 2010 15:07

Javafoil
 
You can obtain a number of point for a lot of profile that you want downloading JavaFoil at http://darwin.wcupa.edu/webapps/javafoil/
good luck.

cxcxcx0505 May 26, 2010 19:09

Thank you!


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