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Fatigue Crack Growth Under Variable Amplitude Loading Through XFEM

2016; Elsevier BV; Volume: 2; Linguagem: Inglês

10.1016/j.prostr.2016.06.384

2452-3216

Haydar Dirik, Tuncay Yalçınkaya,

Non-Destructive Testing Techniques

Predicting fatigue crack growth (FCG) rate and path under variable amplitude loading (VAL) is a crucial issue in damage tolerant design commonly used in aerospace industry. The aim of the current study is to predict FCG life under VAL through Extended Finite Element Method (XFEM) and to explicitly illustrate both FCG life and crack propagation. For this purpose an algorithm is developed and integrated in ABAQUS software to analyze 3D crack propagation under VAL using Modified Generalized Willen-borg (MGW) retardation model. The results are compared with NASGRO crack propagation software and experimental FCG test data on 7075-T6 aluminum alloy under various over load (OL) and over load-under load (OL-UL) conditions which exhibit a good agreement.