problem in 3d meshing
I am doing 3d analysis of a reactangular wing made from naca 2412 airfoil of chord 300mm and span 400mm. I had made the wing in solidworks. I imported the model in gambit as parasoild .. now i am totally sutcked . I have done 2d analysis of airfoil bt never did 3d .
Please help me out and tell me the steps i need to follow . Its a part of our thesis and i am totally stuck here .
what kind of problem?
*import your geometry
*extract fluid domain if necessary
*divide your geometry if you need full hexa mesh
*check your mesh
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