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Dow Uap D48 Report September 1996
Page 72
72 / 181
The simulated impact percentages plotted in Figure 25 are identical with those shown
in Figure 24. The theoretical percentages in Figure 25 were obtained by trying various
combinations of B and A until the best possible fit was obtained in the sectors from +60°
to +180°. From these plots it seems apparent that a reasonable fit between malfunction-
turn and theoretical Mode-5 impact data can be found for any qa between 5,000 and
20,000 deg-Ib/ft’.
100
10
Percent in 5-deg sector (%)
0.1
0.01 i i | i i | i 1
0 20 40 60 80 100 120 140 160 180
Angle From Flight Path (deg)
Figure 25. Delta~-GEM Simulation Results with Best-Fit Shaping Constants
9/10/96 63 RTI
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