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Subtitle Application of LEFM & FMDM Theory. - 2 Conventional Fatigue (High- and Low-Cycle Fatigue). - 4 Fatigue Crack Growth. - Appendix A NASA/FLAGRO 2.0 Materials Constants. Therefore, a comprehen sive structural analysis that consists of static, dynamic, fatigue, and fracture is necessary to ensure the integrity of the structure.
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