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A Fatigue Crack Growth Life Prediction Model for Discontinuous Reinforced Metal-Matrix Composite: Influence of Microstructure

机译:不连续增强金属 - 基质复合材料的疲劳裂纹生长寿命预测模型:微观结构的影响

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Under the fully strain-controlled conditions, a closed-form multistage fatigue crack growth (MSFCG) life prediction model has been developed for discontinuous reinforced MMCs (DRMMCs) considering the effect of microstructural features. The model considers crack nucleation, small crack, and long crack life. The crack initiation is evaluated on the bases of slip steps deepening into a fatigue crack under the cyclic strain. Next, the small crack growth life is investigated within the microstructural threshold. Finally, for long fatigue crack propagation, previously developed model by Tevatia and Srivastava is modified and incorporated in the current model. Under the total strain-controlled conditions, reinforcement in the matrix results in an increase in both (i) the level of cyclic plastic deformation and (ii) cyclic plastic zone size near the vicinity of crack tip. The effect of initiation and small crack growth life is significant for low cycle fatigue applications.
机译:在完全应变控制的条件下,考虑到微观结构特征的效果,已经开发了闭合的多级疲劳裂纹裂纹生长(MSFCG)寿命预测模型,用于不连续增强MMCS(DRMMC)。该模型考虑了裂缝成核,小裂缝和长裂缝寿命。在循环菌株下加深疲劳裂纹的滑移步骤基础评价裂纹启动。接下来,在微观结构阈值内研究小裂纹生长寿命。最后,对于长疲劳裂纹传播,先前通过Tevatia和Srivastava进行了修改和结合在当前模型中的模型。在总应变控制条件下,基质中的增强导致(i)循环塑性变形的水平和(ii)裂缝末端附近的循环塑料区尺寸增加。对低循环疲劳应用的起始和小裂纹生长寿命的影响是显着的。

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