Hi Guys,
I finally found the formula for creating an Airfoil arc radius. It is:
r = ((25*C) / 2*P)) = ((c*p) / 200)
Where:
C = chord in inches
P = percentage of arc required
Who said I'd give up?? LOL
Ren
Received on Tue Apr 24 2012 - 18:26:05 CEST
This archive was generated by Yannick on Sat Dec 14 2019 - 19:13:47 CET