In order to properly fill your custom glider or pattern wing order, we need the following information:


Airfoil 1 (choose from Selig's database) ______________ chord in inches
_________
Airfoil 2 (choose from Selig's database) ______________ chord in inches
_________
Panel length from Airfoil 1 to Airfoil 2 ______________
Panel taper (i.e. straight trailing edge or tip leading edge is 1.5"
behind root leading edge) _______________
Airfoil 3 (choose from Selig's database) ______________ chord in inches _________
Panel length from Airfoil 2 to Airfoil 3 ______________
Panel taper (i.e. straight trailing edge or tip leading edge is 1.5"
behind root leading edge) _______________
Airfoil 4 (choose from Selig's database) ______________ chord in inches _________
Panel length from Airfoil 3 to Airfoil 4 ______________
Panel taper (i.e. straight trailing edge or tip leading edge is 1.5"
behind root leading edge) _______________
Wing sheeting thickness ______________
Leading edge allowance ______________
Trailing edge allowance ______________
Washout (in degrees or raise tip trailing edge 1/4") ______________
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