Simple simple airfoil mesher

Hi. I can only create O-meshes. If your airfoil has a very thin (or collapsing) trailing edge, the mesh might end up being really bad (it might work though). Let me know how this works out.

Example is shown below on this page.
Outer radius of domain
Rear angle
Front angle
Normal cell count
Tangent cell count
Rotate geometry
Rotate blocks
Airfoil data file
Send a message to Mads (do you like this tool? Suggest changes )
If you click me without a file I will just use a naca0015 so you can test.



Sorry for this crappy sketch:


EXAMPLE
1.0000 0.00158
0.9500 0.01008
0.9000 0.01810
0.8000 0.03279
0.7000 0.04580
0.6000 0.05704
0.5000 0.06617
0.4000 0.07254
0.3000 0.07502
0.2500 0.07427
0.2000 0.07172
0.1500 0.06682
0.1000 0.05853
0.0750 0.05250
0.0500 0.04443
0.0250 0.03268
0.0125 0.02367
0.0000 0.00000
0.0125 -0.02367
0.0250 -0.03268
0.0500 -0.04443
0.0750 -0.05250
0.1000 -0.05853
0.1500 -0.06682
0.2000 -0.07172
0.2500 -0.07427
0.3000 -0.07502
0.4000 -0.07254
0.5000 -0.06617
0.6000 -0.05704
0.7000 -0.04580
0.8000 -0.03279
0.9000 -0.01810
0.9500 -0.01008
1.0000 -0.00158