Figure 6 - Crossflow Angle versus Axial Distance for Flow Along 

 Streamlines of the Lucy Ashton 



0.1 



0.0 



-0.1 



-0.2 



T r 



1 r 



-1.0 -0.8 -0.6 -0.4 -0.2 0.0 0.2 0.4 0.6 0.8 1.0 



S 



Figure 6a - Streamline 1 



0.1 



0.0 



-0.1 



-0.2 



"I 1 1 1 1 r 



J L 



LEGEND 

 PRESENT THEORY — — . 



VON KERCZEK 



I I I L 



-1.0 -0.8 -0.6 -0.4 -0.2 0.0 0.2 0.4 0.6 0.8 1.0 



S 



Figure 6b - Streamline 6 



0.1 



0.0 - 



-0.1 - 



-0.2 



1 1 r 



J \ I I L 



LEGEND 

 PRESENT THEORY 

 VON KERCZEK — 



I I L 



-1.0 -0.8 -0.6 -0.4 -0.2 



0.0 0.2 0.4 0.6 



S 



0.8 1.0 



Figure 6c - Streamline 10 



41 



