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How to use FLUENT to solve the transition airfoil

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Old   January 19, 2007, 03:50
Default How to use FLUENT to solve the transition airfoil
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NACA0012
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How can we use FLUENT to solve the transition happened on the airfoil in the low Re. number? Usually there would be the leading edge vortex generated.

Can we predict the transition position of airfoil using FLUENT?

These problems troubled me for a long time. Could somebody answer me?Thank u!
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