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Drag prediction in Lattice Boltzmann method

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Old   October 14, 2007, 17:20
Default Drag prediction in Lattice Boltzmann method
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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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