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A new finite element procedure for fatigue life prediction of AL6061 plates under multiaxial loadings

机译:多轴载荷下AL6061板疲劳寿命预测的新有限元程序

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An energy-based fatigue life prediction framework was previously developed by the authors for prediction of axial, bending and shear fatigue life at various stress ratios. The framework for the prediction of fatigue life via energy analysis was based on a new constitutive law, which states the following: the amount of energy required to fracture a material is constant. In the first part of this study, energy expressions that construct the constitutive law are equated in the form of total strain energy and the distortion energy dissipated in a fatigue cycle. The resulting equation is further evaluated to acquire the equivalent stress per cycle using energy based methodologies. The equivalent stress expressions are developed both for biaxial and multiaxial fatigue loads and are used to predict the number of cycles to failure based on previously developed prediction criterion. The equivalent stress expressions developed in this study are further used in a new finite element procedure to predict the fatigue life for two and three dimensional structures. In the second part of this study, a new Quadrilateral fatigue finite element is developed through integration of constitutive law into minimum potential energy formulation. This new QUAD-4 element is capable of simulating biaxial fatigue problems. The final output of this finite element analysis both using equivalent stress approach and using the new QUAD-4 fatigue element, is in the form of number of cycles to failure for each element on a scale in ascending or descending order. Therefore, the new finite element framework can provide the number of cycles to failure at each location in gas turbine engine structural components. In order to obtain experimental data for comparison, an Al6061-T6 plate is tested using a previously developed vibration based testing framework. The finite element analysis is performed for Al6061-T6 aluminum and the results are compared with experimental results.
机译:作者先前已经开发了基于能量的疲劳寿命预测框架,用于预测各种应力比下的轴向,弯曲和剪切疲劳寿命。通过能量分析预测疲劳寿命的框架基于新的本构定律,该定律规定:破碎材料所需的能量是恒定的。在本研究的第一部分中,构成本构律的能量表达形式等同于总应变能和在疲劳循环中耗散的形变能。使用基于能量的方法,进一步评估所得方程,以获取每个循环的等效应力。针对双轴和多轴疲劳载荷开发了等效应力表达式,并根据先前制定的预测标准来预测失效循环的次数。在这项研究中开发的等效应力表达式在新的有限元程序中进一步用于预测二维和三维结构的疲劳寿命。在本研究的第二部分中,通过将本构定律整合到最小势能公式中,开发了一种新的四边形疲劳有限元。这种新的QUAD-4元件能够模拟双轴疲劳问题。使用等效应力方法和使用新的QUAD-4疲劳单元进行的有限元分析的最终输出,以升序或降序的形式按比例表示每个元素的失效循环数。因此,新的有限元框架可以在燃气涡轮发动机的结构部件中的每个位置提供故障循环的次数。为了获得用于比较的实验数据,使用先前开发的基于振动的测试框架对Al6061-T6板进行了测试。对Al6061-T6铝进行了有限元分析,并将结果与​​实验结果进行了比较。

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