Hi,

Myself and my house mate are interested in creating a simple 2D structured mesh generator based upon aerofoil geometry using Fortran. Any exisiting codes or help to get us going in the right direction would be greatly appreciated.

Hi look this link http://www-users.informatik.rwth-aac.../software.html

http://portal.acm.org/citation.cfm?id=201591.201605

I have recently made a hyperbolic (i.e without specified outer boundary) grid generator for O-meshes around an airfoil based on this paper and its references.

You will have some trouble with the trailing edge, I found this could be resolved by taking forward steps close to the boundary and switching to backward steps later on.

Also, it works better to have the volumes determined per level instead of a priori, as is done in the original paper by Steger and Chaussee