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Mechanical Characterisation of Aluminium Alloy 7449-T7651 at High Strain Rates and Elevated Temperatures Using Split Hopkinson Bar Testing

机译:使用分裂霍普金森棒测试在高应变速率和高温下铝合金7449-T7651的力学性能

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摘要

The mechanical behaviour of a 7 series high-strength aluminium alloy that is mainly used by the aerospace industry is under investigation. Aluminium alloy AA7449-T7651 is mechanically tested at high strain rates (SRs), from 1000 to 10,000 s~(-1) and from room temperature up to elevated temperatures (80, 140, 200, and 300?C). The mechanical characterisation is performed in compression bymeans of an experimental Split Hopkinson Pressure Bar facility. The material's flow stress (σn) and maximum stress are significantly affected by both temperature and SR Nowadays, where the numerical simulation of several mechanical applications and processes that involve high deformation rates is a requirement the mechanical behaviour of the material should be described accordingly. The experimental data are utilised to calculate the SR hardening coefficients of two commonly used material models: Cowper Symonds and Johnson-Cook.
机译:正在研究主要用于航空航天业的7系列高强度铝合金的机械性能。铝合金A7449-T7651在1000至10,000 s〜(-1)的高应变速率(SR)以及从室温到高温(80、140、200和300°C)的情况下进行了机械测试。通过实验的斯普利特霍普金森压力棒设备以压缩方式进行机械表征。如今,材料的流动应力(σn)和最大应力受温度和SR的影响很大,其中要求对涉及高变形率的几种机械应用和工艺进行数值模拟,因此应相应地描述材料的机械性能。实验数据被用来计算两种常用材料模型:考珀·西蒙兹和约翰逊·库克的SR硬化系数。

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