Lift and drag coefficients for low reynolds numbers typical of VAWT
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 |
Here is zillions of experimental results for squillions of airfoils.
http://aerospace.illinois.edu/m-selig/pd.html |
Thank you Glenn Horrocks .....
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