RE: First Scratchbuild--need help with airfoil
okay:
1-9/16" thickness = 1.5625"
1.5625" thick at the spars--and a 10.5" cord--currently
1.5625/10.5 x 100 = 14.88
I want to change to:
1-5/16" thickness and 12.25" cord
1-5/16" thickness = 1.3125"
1.3125/12.25 x 100 = 10.71
So- If I did that right--then I'm going from a 14.88% thickness too a 10.71% thickness.