a: to > 



U.b 

 0.4 



--f^^^^ 



BEVERIDGE^ 





/ PRESENT 



\\ 





/ METHOD 



\ \ 





/ (EQUATION 27) 



0.2 



■ / 



\ \ 



0.0 



/ ' ' 



1 



0.2 



0.4 



0.6 

 r/R RADIUS 



0.8 



Figure 10 - Radial Distribution of Propeller Sink Strength 

 Derived From Lifting Line Calculations 



34 



