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Experimental Characterization and Material Modelling of an AZ31 Magnesium Sheet Alloy at Elevated Temperatures under Consideration of the Tension-Compression Asymmetry

机译:考虑拉伸-压缩不对称性的高温AZ31镁合金板材的实验表征和材料建模

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摘要

Magnesium sheet alloys have a great potential as a construction material in the aerospace and automotive industry. However, the current state of research regarding temperature dependent material parameters for the description of the plastic behaviour of magnesium sheet alloys is scarce in literature and accurate statements concerning yield criteria and appropriate characterization tests to describe the plastic behaviour of a magnesium sheet alloy at elevated temperatures in deep drawing processes are to define. Hence, in this paper the plastic behaviour of the well-established magnesium sheet alloy AZ31 has been characterized by means of convenient mechanical tests (e. g. tension, compression and biaxial tests) at temperatures between 180 and 230 °C. In this manner, anisotropic and hardening behaviour as well as differences between the tension-compression asymmetry of the yield locus have been estimated. Furthermore, using the evaluated data from the above mentioned tests, two different yield criteria have been parametrized; the commonly used Hill'48 and an orthotropic yield criterion, CPB2006, which was developed especially for materials with hexagonal close packed lattice structure and is able to describe an asymmetrical yielding behaviour regarding tensile and compressive stress states. Numerical simulations have been finally carried out with both yield functions in order to assess the accuracy of the material models.
机译:镁薄板合金在航空航天和汽车工业中具有巨大的建筑材料潜力。然而,关于描述镁薄板合金塑性行为的温度相关材料参数的研究现状很少,文献中也缺乏有关屈服准则和用于描述镁薄板合金在高温下塑性行为的适当表征测试的准确陈述。在深拉伸过程中要进行定义。因此,在本文中,已经通过在180至230℃之间的温度进行方便的机械测试(例如拉伸,压缩和双轴测试)表征了完善的镁薄板合金AZ31的塑性行为。以这种方式,已经估计了屈服点的各向异性和硬化行为以及拉伸-压缩不对称之间的差异。此外,使用来自上述测试的评估数据,已经参数化了两个不同的产量标准。通常使用的Hill'48和正交各向异性屈服准则CPB2006,它是为具有六边形密堆积晶格结构的材料而专门开发的,并且能够描述关于拉伸和压缩应力状态的不对称屈服行为。最后使用两个屈服函数进行了数值模拟,以评估材料模型的准确性。

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