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首页> 外文期刊>International Journal of Damage Mechanics >Damage-coupled FLD of Sheet Metals for Warm Forming and Nonproportional Loading
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Damage-coupled FLD of Sheet Metals for Warm Forming and Nonproportional Loading

机译:用于热成形和非比例载荷的薄板损伤耦合FLD

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摘要

A method of forming limit prediction for sheet metals at high temperatures and under nonproportional loading is presented. The method takes into account the strain-softening behaviors of the material at elevated temperatures. A localized necking criterion based on an isotropic damage-coupled acoustic tensor is developed and employed to determine the forming limits of strain-softening materials. The damage evolution equation is developed within the thermo-mechanical framework. A closed-form expression of the forming limit strains is derived by coupling the damage evolution equation into the localized necking criterion. A computer program, incorporating the incremental theory of plasticity, the damage evolution equation and the localized necking criterion, is developed to compute the forming limit strains under several nonproportional loading paths. A series of the uniaxial tensile tests is performed to measure the relevant mechanical properties of AA6061 at the elevated temperature of 450℃. The material damage variables are determined from the measured elastic modulii from a series of loading and unloading paths. The damage evolution equation of AA6061 at 450℃ is formulated based on the test data. The computed limit strains are compared with the test results under various loading paths and a good agreement is observed. It is found that the critical damage value is independent on the stress states and loading paths. It may be concluded that the application of the material damage as a reliable criterion of localized necking including the nonproportional loading cases.
机译:提出了一种在高温和非比例载荷下形成钣金极限预测的方法。该方法考虑了材料在高温下的应变软化行为。建立了基于各向同性损伤耦合声张量的局部颈缩准则,并将其用于确定应变软化材料的成形极限。损伤演化方程是在热机械框架内开发的。通过将损伤演化方程耦合到局部颈缩准则中,得出成形极限应变的闭合形式。开发了一种计算机程序,该程序结合了可塑性的增量理论,损伤演化方程和局部颈缩准则,以计算在几种非比例载荷路径下的成形极限应变。进行了一系列的单轴拉伸试验,以测量AA6061在450℃的高温下的相关机械性能。根据一系列加载和卸载路径的测量弹性模量确定材料损伤变量。根据试验数据建立了AA6061在450℃下的损伤演化方程。将计算出的极限应变与各种载荷路径下的测试结果进行比较,并观察到很好的一致性。发现临界损伤值与应力状态和加载路径无关。可以得出结论,将材料损坏作为局部缩颈的可靠标准,包括非比例加载情况。

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