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Reynolds number effect on Lift Coefficient

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Hi, so my question is, what effect does the reynolds number have on the lift coefficient (and anything else for that matter)?

I understand it's a measure of laminar vs turbulent airflow, and that it does effect the maximum lift coefficient. But i haven't found any information on how to incorporate it into an equation.
Any help much appreciated.
Thanks.

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Re effect will vary wildly for different airfoils. As a (very) general rule, higher Re will yield better lift results.

http://www.cfd-online.com/Wiki/NACA0012_airfoil

This shows some plots of how Re effects CL and CD. Of further interest, you may look at XFOIL (a 2D CFD program that will create various lift plots for airfoil shapes), or investigate various NACA airfoils.

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