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Corrected AoA and Cl for AR ...

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clanon

clanon

Well-Known Member
Joined
Jun 6, 2007
Messages
1,119
Hi,guys...I didn't find post about the corrections you're supposed to do for aspect ratio on the angles (from airfoil plot to rigging)
-Induced AoA + section AoA.
-Induced Cl + section Cl
And how 0 lift angle should go (plus or minus)
PS: i know is basic but it is important for me to get it right
Thankz
I have a .21 correction factor for AR 8.4 from a curve ; non tappered (1)
 
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