2004
DOI: 10.1016/j.ijfatigue.2004.02.004
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A multi-mechanism damage coupling model

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Cited by 26 publications
(22 citation statements)
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“…The proposed CDM model relates the effects of anode microstructure defects to parametric quantities that can be observed and measured at the macroscopic scale, such as material stiffness. The CDM model accounts for material degradation in a phenomenological way through a degradation variable ( D ) that governs the reduction of the homogenized elastic modulus 12,13 : where E 0 is the initial elastic modulus and E is the elastic modulus of degraded material, as shown in Fig. 1.…”
Section: Anode Degradation Modelmentioning
confidence: 99%
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“…The proposed CDM model relates the effects of anode microstructure defects to parametric quantities that can be observed and measured at the macroscopic scale, such as material stiffness. The CDM model accounts for material degradation in a phenomenological way through a degradation variable ( D ) that governs the reduction of the homogenized elastic modulus 12,13 : where E 0 is the initial elastic modulus and E is the elastic modulus of degraded material, as shown in Fig. 1.…”
Section: Anode Degradation Modelmentioning
confidence: 99%
“…Several mechanisms are involved in the process of anode material degradation. Each mechanism requires a different degradation variable to be specified 13 . In the proposed degradation model, we have specified two degradation variables: (1) a thermomechanical degradation variable ( D m ), which is associated with stresses and the thermal aging effect and (2) a chemical degradation variable ( D c ), which is associated with the effects of coal syngas contaminants on the anode microstructure and mechanical strength.…”
Section: Anode Degradation Modelmentioning
confidence: 99%
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“…34 Thus, the model capabilities can be extended to thermomechanical fatigue and high-cycle fatigue. 35,36 Some investigations were also performed in order to understand crack initiation phenomena. Indeed, Cailletaud and Levaillant 37 have divided the fatigue damage component into two stages as a crack microinitiation and a crack micropropagation.…”
Section: Stress-formulated Approachmentioning
confidence: 99%
“…Influences of temperature evolution within cycles and material ageing on the lifetime can also be considered 34 . Thus, the model capabilities can be extended to thermomechanical fatigue and high‐cycle fatigue 35,36 . Some investigations were also performed in order to understand crack initiation phenomena.…”
Section: Introductionmentioning
confidence: 99%