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structured grid generation for airfoils in tandem

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Old   May 25, 2006, 20:11
Default structured grid generation for airfoils in tandem
  #1
quarkz
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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!
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Old   May 27, 2006, 15:24
Default Re: structured grid generation for airfoils in tan
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Bounecer
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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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