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Thermo-viscoplastic behaviour of 2024-T3 aluminium sheets subjected to low velocity perforation at different temperatures

机译:2024-T3铝板在不同温度下经受低速穿孔的热粘塑性行为

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摘要

This paper deals with the mechanical behaviour of the aluminium alloy 2024-T3. This alloy has particular relevance since it is widely used in the aeronautical industry for building aircraft structures. The deformation behaviour of this material has been characterised in tension under wide ranges of strain rate and temperature. Among the aluminium alloys, the AA 2024-T3 highlights due to its high flow stress and strain hardening. Moreover, the material temperature sensitivity has been found dependent on plastic strain. The Modified Rusinek-Klepaczko constitutive description [Rusinek A, Rodriguez-Martinez JA, Arias A. A thermo-viscoplastic constitutive model for FCC metals with application to OFHC copper. Int. J. Mech. Sci. 52 (2010) 120-135], which takes into account such dependence of the temperature sensitivity on plastic strain, has been applied for modelling the thermo-viscoplastic response of the material. Satisfactory agreement between experiments and analytical predictions provided by the Modified Rusinek-Klepaczko model has been found. In order to study the material behaviour under impact loading, low velocity perforation tests on AA 2024-T3 sheets have been performed at different initial temperatures using a drop weight tower. Plastic instabilities formation and progression are identified as the cause behind the target collapse for all the impact tests conducted. The results from these perforation tests are compared with those reported in [Rodriguez-Martinez JA, Pesci R, Rusinek A, Arias A, Zaera R, Pedroche DA. Thermo-mechanical behaviour of TRIP 1000 steel sheets subjected to low velocity perforation by conical projectiles at different temperatures. Int. J. Solids Struct. 47 (2010) 1268-1284.] for TRIP 1000 steel sheets. The comparison reveals that the amount of specific energy absorbed by the aluminium targets is much lower than that corresponding to the steel targets. The role played by inertia on delaying plastic instabilities formation is determined as potential responsible for such behaviour.
机译:本文研究了铝合金2024-T3的力学性能。这种合金具有特殊的意义,因为它在航空工业中广泛用于建造飞机结构。这种材料的变形行为已在很宽的应变率和温度范围内表现为张力。在铝合金中,AA 2024-T3的亮点在于其高流动应力和应变硬化。此外,已经发现材料温度敏感性取决于塑性应变。修改后的Rusinek-Klepaczko本构描述[Rusinek A,Rodriguez-Martinez JA,AriasA。FCC金属的热粘塑性本构模型,应用于OFHC铜。诠释J.机甲科学52(2010)120-135],已考虑到温度敏感性对塑性应变的这种依赖性,已被用于模拟材料的热粘塑性响应。已发现修改后的Rusinek-Klepaczko模型提供的实验与分析预测之间令人满意的一致性。为了研究冲击载荷下的材料性能,已经使用滴重塔在不同的初始温度下对AA 2024-T3板材进行了低速穿孔测试。塑性不稳定性的形成和发展被确定为所进行的所有冲击测试的目标坍塌背后的原因。将这些穿孔测试的结果与[Rodriguez-Martinez JA,Pesci R,Rusinek A,Arias A,Zaera R,Pedroche DA。 TRIP 1000钢板在不同温度下受到锥形弹丸低速穿孔的热机械性能。诠释J.固体结构。 47(2010)1268-1284。],用于TRIP 1000钢板。比较表明,铝靶材吸收的比能量远低于钢靶材所吸收的比能。惯性在延缓塑性不稳定性形成中所起的作用被确定为造成这种行为的潜在原因。

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