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Damage accumulation and ductile fracture modeling of notched specimens under biaxial loading at room temperature

机译:在室温下双轴载荷下缺口标本的损伤积累和延性裂缝模拟

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This paper presents the results of ductile fracture tests conducted on axisymmetric specimens with notch made from EN AW 2024 1351 aluminum alloy. Tests were conducted for five notch radius and seven cases of biaxial, proportional loading with tensile force and torsional moment. A model of damage accumulation and fracture based on variables of stress strain state and damage on a physical plane is proposed. The fracture criterion assumes that crack initiation will occur when a certain combination of normal and shear stress on the physical plane (elliptical criterion in the tensile stress zone and Coulomb criterion in the shear stress zone) reaches a critical value dependent on the value of the damage state variable on this plane. The damage accumulation law was formulated incrementally, and the increment of the damage state variable was made dependent on the increment of plastic deformations and stress values on the physical plane. This model was successfully verified by experimental tests and numerical simulations. which are presented in papers by Derpenski and Seweryn (2016a,b). (C) 2017 Elsevier Ltd. All rights reserved.
机译:本文介绍了在轴对称标本上进行的延伸性裂缝试验的结果,该试验与由EN 2024 1351铝合金制成的凹口。对五个凹口半径和7例双轴,比例装载进行试验,具有拉伸力和扭转力矩。提出了一种基于应力应变状态和物理平面损坏的损伤积累和裂缝模型。裂缝标准假设当物理平面上的正常和剪切应力的某种组合(剪切应力区中的椭圆标准和剪切应力区域中的库仑标准)的某种组合达到临界值时,将发生裂纹启动。依赖于损坏的值这个飞机上的状态变量。逐步配制损伤累积定律,损坏状态变量的增量取决于物理平面上的塑性变形和应力值的增量。该模型通过实验测试和数值模拟成功验证。由Derpenski和Seweryn(2016A,B)呈现论文。 (c)2017 Elsevier Ltd.保留所有权利。

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