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structured grid generation for airfoils in tandem

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May 25, 2006, 21:11	structured grid generation for airfoils in tandem	#1
quarkz Guest Posts: n/a	hi, 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. Thanks!

May 27, 2006, 16:24	Re: structured grid generation for airfoils in tan	#2
Bounecer Guest Posts: n/a	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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