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Synthesis of crack initiation life in steel notched specimens under torsional fatigue based on the averaged strain energy density

机译:基于平均应变能密度的缺口疲劳试件的裂纹萌生寿命综合

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摘要

The torsional fatigue behaviour of circumferentially notched specimens made of austenitic stainless steel, SUS316L, and carbon steel, SGV410, characterized by different notch root radii has been recently investigated by Tanaka. In that contribution, it was observed that the total fatigue life of the austenitic stainless steel increases with increasing stress concentration factor for a given applied nominal shear stress amplitude. By using the electrical potential drop method, Tanaka observed that the crack nucleation life was reduced with increasing stress concentration, on the other hand the crack propagation life increased. The experimental fatigue results, originally expressed in terms of nominal shear stress amplitude, have been reanalysed by means of the local strain energy density (SED) averaged over a control volume having radius R0 surrounding the notch tip. To exclude all extrinsic effects acting during the fatigue crack propagation phase, such as sliding contact and/or friction between fracture surfaces, crack initiation life has been considered in the present work (*). In the original paper, initiation life was defined in correspondence of a 0.1÷0.4-mm-deep crack. The control radius R0 for fatigue strength assessment of notched components, thought of as a material property, has been estimated by imposing the constancy of the averaged SED for both smooth and cracked specimens at NA = 2 million loading cycles.
机译:田中最近研究了由奥氏体不锈钢SUS316L和碳钢SGV410制成的周向缺口试样的扭转疲劳行为,该试样的缺口根半径不同。在该贡献中,观察到对于给定的施加的名义剪切应力幅度,奥氏体不锈钢的总疲劳寿命随着应力集中系数的增加而增加。田中通过电位降法观察到,随着应力集中的增加,裂纹的成核寿命降低,另一方面,裂纹的扩展寿命增加。最初用名义剪切应力幅度表示的实验疲劳结果已经通过局部应变能密度(SED)进行了重新分析,该平均应变能密度是在半径为R0的槽口周围的控制体积上平均的。为了排除在疲劳裂纹扩展阶段发挥作用的所有外部影响,例如滑动接触和/或断裂表面之间的摩擦,在当前工作中已考虑了裂纹萌生寿命(*)。在原始论文中,起爆寿命定义为深0.1÷0.4-mm的裂纹。通过对NA = 2百万次加载循环施加光滑和破裂试样的平均SED常数,可以估算带缺口部件的疲劳强度评估的控制半径R0(被认为是材料特性)。

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