Palmgren–miner’s rule and fracture mechanics based fatigue analysis of deepwater mooring lines

Xue, Xutian; Chen, Nian-Zhong

doi:10.1201/9781315157368-51

Cited by 1 publication

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“…7 Miner rule or relative Miner rule is used to calculate the fatigue damage of components under constant amplitude loading, which has certain engineering application value. 8 Critical plane method considers that fatigue failure occurs in a particular plane, and fatigue life prediction and damage analysis are studied on that particular plane. 9 Because critical plane method is based on fracture model and crack initiation mechanism, it has certain physical significance.…”

Section: Introductionmentioning

confidence: 99%

A new multiaxial fatigue life prediction model considering additional hardening effect

Liu

Wang

2014

Advances in Mechanical Engineering

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The established linear fatigue life prediction model based on the Miner rule has been widely applied to fatigue life prediction under constant amplitude uniaxial and multiaxial loading. Considering the physical significance of crack formation and propagation, a multiaxial equivalent linear fatigue life prediction model is put forward based on Miner rule and critical plane method under constant amplitude loading. The essence of this approach is that the equivalent strain, which consists of the shear strain and normal strain on the critical plane, replaces the relevant parameter of uniaxial nonlinear fatigue damage model. The principal axes of stress/strain rotate under non-proportional loading. Meanwhile, the microstructure of material and slip systems change, which lead to additional hardening effect. The ratio of cyclic yield stress to static yield stress is used to represent the cyclic hardening capacity of material, and the influence of phase difference and loading condition on the non-proportional hardening effect is considered. The multiaxial fatigue life is predicted using equivalent stain approach, maximum shear stain amplitude model, CXH model, and equivalent multiaxial liner model under proportional and/or non-proportional loading. The smooth and notched fatigue specimens of four kinds of materials (Q235B steel, titanium alloy TC4, Haynes 188, and Mod.9Cr-1Mo steel) are used in the multiaxial fatigue experiments to verify the proposed model. The predicted results of these materials are compared with the test results, and the results show that these four models can achieve good effect under proportional loading, but the proposed model performs better than the other three models under non-proportional loading. Meanwhile, it also verifies that the proposed enhancement factor can reflect the influence of phase difference and material properties on additional hardening.

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Section: Introductionmentioning

confidence: 99%