E/E ee 
Figure 22 - Variation of Experimental Total Loads with Angular 
Position for Quasi-Steady Acceleration 
5 KNOTS 
.21 REV/SEC 
3.55 KNOTS 
10.96 REV/SEC 
6 
2 
ee ae 
IS 
V = 5.36 KNOTS \ a 
n = 12.70 REV/SEC S 
V = 6.26 KNOTS 
n = 13.78 REV/SEC eee 
V= 6.52 KNOTS 
n = 14.08 REV/SEC 
135 180 225 270 315 360 
0 45 90 
POSITION ANGLE 6 (DEGREES) 
Figure 22a - F 
x 
109 
