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Lift and drag coefficients for low reynolds numbers typical of VAWT

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Old   December 17, 2013, 01:19
Default Lift and drag coefficients for low reynolds numbers typical of VAWT
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M. Abdul Akbar
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Dear All,

For the purposes of my research I need data of lift and drag coefficients for asymmetric NACA airfoil's for low Reynolds number's typical of Vertical Axis Wind Turbine's (VAWT). Is there any experimental data for the same ?. I know there is data for symmetrical airfoil brought out by the Sandia National Laboratories but is there a similar experimental result database for non-symmetrical NACA airfoil's ??

Thanks in Advance,
Abdul Akbar
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Old   December 17, 2013, 05:17
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Glenn Horrocks
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Here is zillions of experimental results for squillions of airfoils.

http://aerospace.illinois.edu/m-selig/pd.html
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Old   December 17, 2013, 07:40
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Thank you Glenn Horrocks .....
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airfoil, drag, lift, naca, vawt


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