





^^^^ 



^ 









7r-^tanj3j(r) 



---""""^ 





S 



0.02 



/ 





-X 



r 



27rRV 



- 



0.01 



/ 







\ 











Cjh 



= 0.370 \ 







/ 



1 



1 



= 1.250 

 1 



\ 



0.2 



0.4 



0.6 



r/R 



0.8 



- 1.2 



— 1.0 



- 0.8 



- 0.6 



- 0.4 



- 0.2 



-< 

 o 



o 



o 



d > 



o 2 

 o 



1.0 



Figure 15 - Design Circulation and Hydrodynamic Pitch 

 Distributions of Propeller 4567A 



46 



