Crack Growth Simulation and Residual Strength Prediction in Airplane Fuselages PDF
189 Pages·08.66 MB·English
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presumes that any damage initiated by fatigue, accident, or corrosion will be found before catastrophic failure. [138]. The safety of the aircraft heavily depends upon finding cracks before they reach a critical length. The occurrence of WFD, however, drastically reduces the residual strength or de
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