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Airfoil "Actual Location" of Aerodynamic center...(How to find it)

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clanon

Well-Known Member
Joined
Jun 6, 2007
Messages
1,119
Just found this presentation making (i guess) a relationship between real AC and location of Thickness on the MAC...
For the 23012 and the 64212
Imagen2.jpg
Is it the t/c ratio @30% on the 23012 moving the Actual Ac ahead and viceversa for the 64212 ?
Is there an easy way of calculating this for a novel airfoil ?

Thnkz
 
Last edited:
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