I4UU 



1 1 1 1 1 1 1 



a = 10° 





1 U = 225 ft/sec 



1200 



— CL z/c ~ 1 - 



w 





0. 





C) 



H 1000 



— 1 



1 



J^ 





I 



Q 





\ 



UJ 





1 



111 





1 



a. 



J /"S 



CO 



-1 



O : ^ O (a = 0) REFERENCE 24 



< 800 



~" f 



h A (C ~ 0.06) REFERENCE 24 " 



o 





I 



1- 





I 



< 





\ 



1- 





1 



o 



T ^^ 



S 600 



jj 9 



UJ 





V 



H 





r\ 



UJ 





w 



S 





\ 



X 





\ 



LU 





\ 



t 400 



" / \ 1 



O 



p v 



> 





\ 1 



200 



— XT 



^^^'^ifV^" 



n 



t:^ocP*i^^"^ 



-3 -2 -1 ~ 1 2 

 SPANWISE DISTANCE FROM WING TIP POSITIVE OUTBOARD (IN.) 



Figure 11 - Variation of Tip Vortex Rotational Velocity as a Function 

 of Wing Outboard Distance for Spanwise Mass Injected Tip 



(Data from Reference 24) 



24 



