Department of the Air Force Report, 1996

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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-lb/ft2.
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20
40
60
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180
Angle From Flight Path {deg)
············-················-
Figure 25. Delta-GEM Simulation Results with Best-Fit Shaping Constants
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RTI