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Fundamental structure of steady plastic shock waves in metals

机译:金属中稳定塑性冲击波的基本结构

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摘要

The propagation of steady plane shock waves in metallic materials is considered. Following the constitutive framework adopted by R. J. Clifton [Shock Waves and the Mechanical Properties of Solids, edited by J. J. Burke and V. Weiss (Syracuse University Press, Syracuse, N.Y., 1971), p. 73] for analyzing elastic–plastic transient waves, an analytical solution of the steady state propagation of plastic shocks is proposed. The problem is formulated in a Lagrangian setting appropriate for large deformations. The material response is characterized by a quasistatic tensile (compression) test (providing the isothermal strain hardening law). In addition the elastic response is determined up to second order elastic constants by ultrasonic measurements. Based on this simple information, it is shown that the shock kinetics can be quite well described for moderate shocks in aluminum with stress amplitude up to 10 GPa. Under the later assumption, the elastic response is assumed to be isentropic, and thermomechanical coupling is neglected. The model material considered here is aluminum, but the analysis is general and can be applied to any viscoplastic material subjected to moderate amplitude shocks. Comparisons with experimental data are made for the shock velocity, the particle velocity and the shock structure. The shock structure is obtained by quadrature of a first order differential equation, which provides analytical results under certain simplifying assumptions. The effects of material parameters and loading conditions on the shock kinetics and shock structure are discussed. The shock width is characterized by assuming an overstress formulation for the viscoplastic response. The effects on the shock structure of strain rate sensitivity are analyzed and the rationale for the J. W. Swegle and D. E. Grady [J. Appl. Phys. 58, 692 (1985)] universal scaling law for homogeneous materials is explored. Finally, the ability to deduce information on the viscoplastic response of materials subjected to very high strain rates from shock wave experiments is discussed.
机译:考虑了稳态平面冲击波在金属材料中的传播。遵循R. J. Clifton所采用的本构框架[Shock Waves and Solids Mechanical Properties of Solids,由J. J. Burke和V. Weiss编辑(纽约锡拉丘兹市雪城大学出版社,1971年),第243页。 73]为分析弹塑性瞬态波,提出了塑性冲击稳态传播的解析解。该问题是在适合大变形的拉格朗日设置中提出的。材料响应的特征在于准静态拉伸(压缩)测试(提供了等温应变硬化定律)。另外,通过超声测量来确定弹性响应直至二阶弹性常数。根据这个简单的信息,可以看出,对于应力幅度高达10 GPa的铝,中等强度的冲击可以很好地描述其冲击动力学。在后面的假设下,假定弹性响应是等熵的,而忽略了热机械耦合。这里考虑的模型材料是铝,但是分析是常规的,可以应用于遭受中等振幅冲击的任何粘塑性材料。与实验数据进行了比较,包括冲击速度,质点速度和冲击结构。通过一阶微分方程的求积获得冲击结构,该方程在某些简化假设下提供了分析结果。讨论了材料参数和载荷条件对冲击动力学和冲击结构的影响。冲击宽度的特征在于,假设用于粘塑性响应的应力过大。分析了应变速率敏感性对冲击结构的影响,并提出了J. W. Swegle和D. E. Grady的基本原理[J.应用物理58,692(1985)]探索了均质材料的通用比例定律。最后,讨论了从冲击波实验中推论材料在非常高应变速率下的粘塑性响应信息的能力。

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    Molinari A.; Ravichandran G.;

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  • 年度 2004
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