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Fatigue crack growth simulations of plastically graded materials using XFEM and J-integral decomposition approach

机译:使用XFEM和J-Intional分解方法疲劳裂纹裂纹增长模拟塑料分级材料

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摘要

In this work, fatigue crack growth in functionally graded materials (FGM)/plastically graded materials (PGM) is simulated using the J-integral decomposition approach and extended finite element method (XFEM). The fatigue crack growth rate is estimated by the stress intensity factor based Paris law. The stress intensity factor is computed by the J-integral decomposition approach. In this approach, state variables such as stress, strain and displacement derivatives are decomposed into their symmetric and anti-symmetric parts across the crack surface. The numerical issues faced in J-integral computation such as the evaluation of stress at spatial mirror point and strain energy density derivative are properly addressed. A novel data transfer scheme is proposed to evaluate the stresses at the spatial mirror point. In this scheme, the derivative of strain energy density is calculated by surface approximation of the strain energy density. Various fatigue crack growth problems are simulated by the proposed methodology under mode-I and mixed mode loading. A component level problem i.e. fatigue crack growth in an aero-engine turbine disc made of plastically graded material is solved to demonstrate the versatility of the presented methodology.
机译:在这项工作中,使用J-Intional分解方法和扩展有限元方法(XFEM)模拟功能渐变材料(FGM)/塑性渐变材料(PGM)的疲劳裂纹生长。由基于应力强度因子的巴黎法律估算疲劳裂纹生长速率。应力强度因子由J-Integral分解方法计算。在这种方法中,诸如应力,应变和位移衍生物的状态变量在裂缝表面上分解成其对称和抗对称部件。诸如空间镜点处应力评估和应变能量密度衍生物的j-积分计算中面临的数值问题被适当地解决。提出了一种新的数据传递方案来评估空间镜点处的应力。在该方案中,通过应变能密度的表面近似来计算应变能密度的衍生物。通过模式-I和混合模式加载,通过所提出的方法模拟各种疲劳裂纹生长问题。解决了由塑性分级材料制成的航空发动机涡轮盘中的疲劳裂纹增长,以证明所呈现的方法的多功能性。

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