[Gmsh] Airfoil meshing Naca 0012

[Emanuele T.]

I attach my current .geo file

2010/2/20 Emanuele T. <nuovodna at gmail.com>

> Thanks for the tip. Now i have another problem. I prepared a .geo file with
> an airfoil in a circular box. I'd like to obtain a mesh like in attached
> picture. How can i realize this?
>
>
> 2010/2/19 Eric Nutsch <ericnutsch at gmail.com>
>
> Emanuele,
>>
>>
>> If by points you mean cells (for more resolution), you can use the
>> gmsh "characteristic length" variable (lots of info in the user
>> guide).
>>
>> If you actually want more points(not sure why) you would have to write
>> an interpolation script outside of gmsh (python for instance)
>>
>>
>> Eric Nutsch
>>
>>
>>
>> On Fri, Feb 19, 2010 at 12:15 PM, Emanuele T. <nuovodna at gmail.com> wrote:
>> > 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
>> > _______________________________________________
>> > gmsh mailing list
>> > gmsh at geuz.org
>> > http://www.geuz.org/mailman/listinfo/gmsh
>> >
>> >
>>
>
>
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