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Fatigue analysis for CF-18 component:wing fold shear-tie lug

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Figure

Figure 1 FT312 test set-up, (a) actuator load cell installation; (b) loading lug and digital image correlation camera [1].
Figure 2 (a) Post-modification spectrum sequence plot [1]; (b) Statistical plots of spectrum load ratio
Figure 3 (a) Fracture surface and two main cracks; (b) upper crack nucleation feature: particle; c) lower crack nucleation feature: unclear
Figure 5 Shear-tie lug FE model, and the inboard beam and forward rigid link attachment points
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