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Old 04-11-2011, 08:47 AM
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Lnewqban
 
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Default RE: Stall Speed
Pablo,

You need to determine the maximum coefficient of lift (CL) of that airfoil for the worst Reynolds number of your wing (tip if tapered wing).

Then you can use this calculator:

http://adamone.rchomepage.com/calc_stallspeed.htm
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