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
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
For the 23012 and the 64212
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: