Besoh and Liu 



0.2 0.4 0.6 



Spanwise Position y/L 



Figure 19a. Aerodynamic center location 



1.0 



0.2 



0.8 



0.4 0.6 

 Spanwise Position y/L 



Figure 19b. Local lift coefficient slope Cn 



La 



l.o 



i.o 



0.2 



0.4 0.6 

 Spanwise ros'tion y/L 



0.8 



Figure 19c. Noncirculatory modification factor p 



Figure 19. 



Spanwise distributions of loading modification parameters 



388 



