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ESTIMATION OF THE TOTAL FATIGUE LIFE OF METALLIC STRUCTURES

机译:金属结构的总疲劳寿命估算

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The fatigue life of a component is defined as the total number of cycles or time to induce fatigue damage and to initiate a dominant fatigue flaw which is propagated to final failure.(Shigley & Mischke 2002) The aim of this project is to calculate the total fatigue life of metallic structures under cyclic loading by applying equations found by Basquin and Manson-Coffin. The local stresses and strains necessary for the calculation are determined by the finite element method. Former studies concerning this subject have used analytical methods to find the local conditions at the critical section. The analytical methods, based on Neuber and Molski-Glinka's approaches, permit the calculation of the local stresses and strains at the critical section of the structure's geometry as a function of the nominal stress (forces) applied. For the finite elements method, ABAQUS is used to determine the local conditions at the critical section of a T-shaped model.
机译:组件的疲劳寿命定义为引起疲劳损伤并引发主要疲劳缺陷的周期或时间总数,该缺陷会传播到最终失效。(Shigley&Mischke 2002)该项目的目的是计算总数应用Basquin和Manson-Coffin得出的方程,分析了循环荷载作用下金属结构的疲劳寿命。计算所需的局部应力和应变是通过有限元方法确定的。有关该主题的先前研究已使用分析方法来找到关键部分的当地条件。基于Neuber和Molski-Glinka方法的分析方法可以根据所施加的名义应力(力)来计算结构几何形状关键部分的局部应力和应变。对于有限元方法,ABAQUS用于确定T形模型关键部分的局部条件。

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