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DOW-UAP-D48, Department of the Air Force Report, 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
Delta-GEM Random-AttitudeFailuresthrough270see
Breakup.g-alpha.in.deg-lb/ft
no breakup
20,000
10,000
10
Percent in 5-deg sector (%)
5,000
A=2.60B.=10.000
A= 3.15, B-= 2,000
A=3.35, B= 2,000
A = 3.50, B = 4
0.1
0.01
0
20
40
60
80
100120
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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