structured grid generation for airfoils in tandem
may i know what is a more efficient way of generating structured grid for airfoils in tandem? Is it necessary to 've a multiblock approach?
btw, i'm currently using c grid for a single airfoil.
Re: structured grid generation for airfoils in tan
I've also used C-grid for solving N-S equations for flow about airfoil but my code program diverge. Is that because wrong choise of stretching parameters?
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