DESIGN Cjh = 0.210 



0.03 - 



0.02 - 



0.01 - 







4488 AND 4489 







/^ 



^-L^^ 



rrr tan j3j 



/ 



/ 



/y^''^ ^ 4486 



\ 







^4487 ^•""^^...^ 



A- 





^^^^.^^^ 







r 



^^\ 







27rRV 



^ 



^ H 



- 5 



X 

 -o < 



_ > 

 O 2 

 o 



- 1.2 



1.0 



0.4 



1.0 



RADIUS — 

 n 



Figure 19 - Lifting Line Circulation and Hydrodynamic Pitch 

 Representing Loading of Propellers 4486, 4487, 

 4488, and 4489 



57 



