RA Cores Custom wing quote work sheet

Airfoil 1 E214 RG15 S3021 S4083 SD7003 SD7032 SD7037 SD8020 Use other field or chord in inches
Airfoil 2 E214 RG15 S3021 S4083 SD7003 SD7032 SD7037 SD8020 Use other field or 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 E214 RG15 S3021 S4083 SD7003 SD7032 SD7037 SD8020 Not Used Use other field or 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 E214 RG15 S3021 S4083 SD7003 SD7032 SD7037 SD8020 Not Used Use other field or 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 1/16" balsa (0.0625") 1/20" balsa (0.05") 1/32" balsa (0.03125") 1/42" obechi (0.024") none (fiberglass vacuum bagging) Use other field or
Leading edge allowance none (fiberglass vacuum bagging) 1/8" balsa (0.125") 3/16" balsa (0.1875") 1/4" balsa (0.25") 3/8" balsa (0.375") 1/2" balsa (0.5") Use other field or
Trailing edge allowance 1/4" balsa (0.25") 1/2" balsa (0.5") 1" balsa (1.0") feather edge Use other field or

Washout (in degrees or raise tip trailing edge 1/4") None 1 degree 2 degrees 3 degrees Use other field or

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