Abstract
Fatigue modeling is a fundamental step in the design against fatigue failure. The formulation of mathematical relations to correlate material deformation such as stress, strain, or energy to fatigue life requires an understanding of the cyclic behavior of material including complex phenomena such as nonproportional hardening. Multiaxial fatigue damage models are developed based on the basic principle that multiaxial deformation can be mapped onto uniaxial deformation. Depending on the assumed damage variables in a given parameter, low cycle fatigue models can be strain- or energy-based. Essentially, fatigue damage is associated with the formation of cracks that generally grow along certain orientations. Therefore, the evaluation of a fatigue damage parameter on selected planes is known as the critical plane concept. This chapter covers different aspects of strain- and energy-based fatigue damage modeling methods. Important topics such as fatigue crack behavior, cyclic nonproportional hardening, and damage accumulation are discussed. The chapter ends by explaining the link between material constitutive properties, fatigue damage model, and cyclic plasticity model to predict the fatigue failure of structures.
Original language | English |
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Title of host publication | Cyclic Plasticity of Metals |
Subtitle of host publication | Modeling Fundamentals and Applications |
Publisher | Elsevier |
Pages | 357-395 |
Number of pages | 39 |
ISBN (Electronic) | 9780128192931 |
ISBN (Print) | 9780128192948 |
DOIs | |
State | Published - 1 Jan 2021 |
Bibliographical note
Publisher Copyright:© 2022 Elsevier Inc. All rights reserved.
Keywords
- Critical plane
- Damage accumulation
- Energy-based approach
- Fatigue damage
- Fatigue life estimation
- Low cycle fatigue
- Nonproportional hardening
- Strain-based approach
- Uniaxial/multiaxial loading
ASJC Scopus subject areas
- General Engineering