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October 14, 2007, 18:20 |
Drag prediction in Lattice Boltzmann method
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#1 |
Guest
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Hi!
I am wondering how would this method perform in analysis of aicraft wings (airfoils) and similar where drag is very low. FVM methods are known to get it too high and I also found that in them drag vs AOA curve is not similar in shape to experimental. I'm interested in low mach numbers Ma<0.3 Thank you! Daniel |
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