[saeed jamshidi]

Hello all,

I am going to create contour of flow over an airfoil in tecplot manually.
I have generated a mesh around the airfoil and extracted the all nodes coordinates. The mesh is structured and non staggered.
You know for a simple geometry we have something like this:

 ZONE,I=         180 ,J=         120 ,C=RED,F=POINT
    0  0.1 1
    0.1 0.1 2
    ....

So, what about complex geometries?