Y^ = Y^/t • t/c • e = Y-p/T • (0.10) • c 



Yg = Yc^* ■ ^'"''= ■ " " ^c^'' ■ <0025) • c 



WHERE 



fm = CAMBER 

 t = THICKNESS 

 C = CHORD 



AND LEADING EDGE RADIUS = 0.448 (t/c)^ • C 



X/C 



yjir 



Yc/* 















0.025 



0.1466 



0.1586 



0.050 



0.2066 



0.2712 



0.100 



0.2907 



0.4482 



0.200 



0.4000 



0.6993 



0.300 



0.4637 



0.8635 



0.400 



0.4962 



0.9615 



0.500 



0.4962 



1.0000 



0.600 



0.4653 



0.9786 



0.700 



0.4035 



0.8892 



0.800 



0.3110 



0.7027 



0.900 



0.1877 



0.3586 



1.000 



0.0333 



0.0000 



Figure 6 - Nondimensional Section Offets of the Parent Foil 



11 



