[Gmsh] Airfoil meshing Naca 0012

[Emanuele T.]

Hi, i wrote a mesh using naca 0012 points taken here
http://www.soton.ac.uk/~jps7/Aircraft%20Design%20Resources/Sydney%20aerodynamics%20for%20students/panel2d/naca0012.dat

I want to intensify the density of points near the leading edge and the
trailing edge. How can i obtain this??
Thanks
-------------- next part --------------
An HTML attachment was scrubbed...
URL: <http://www.geuz.org/pipermail/gmsh/attachments/20100219/195b4cb8/attachment.html>
-------------- next part --------------
A non-text attachment was scrubbed...
Name: parziale_phisical.geo
Type: application/octet-stream
Size: 15385 bytes
Desc: not available
URL: <http://www.geuz.org/pipermail/gmsh/attachments/20100219/195b4cb8/attachment.geo>