[peter pan]

Hello,
I'm new in this forum and need some help for meshing a naca 0015 airfoil (2D, quad cells only, solver=fluent).
For the first time I used edge sizings and mapped face meshing in a C-Grid. But I need an inflation layer at the edges of the airfoil, so I can use the "same" grid for standart wall function with y+ between 30 and 300 and enhanced wall function with y+<5.
Now I have the problem that there is no possibility to use an inflation layer with a mapped face meshing. I tried a lot of different sizing methods but never got a accurate grid.

Does anybody know how to mesh that airfoil, to get a grid like the picture?

http://imageshack.us/photo/my-images/807/grid.jpg/





My first grid with the mapped face meshing was like the picture but without the inflation layer.