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December 8, 2005, 03:57 |
stretching coefficients
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#1 |
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Hello all; I'm using structured "C" grid generation for simulating flow about NACA 0012 airfoil in case of 2D, incompressible and laminar flow (Re=2x10**3). Please can you direct me to the grid dimension and the stretching coefficients necessary for this flow.
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