聚甲基丙烯酸甲酯Hugoniot简易评价系统的开发

IF 1.7 4区 工程技术 Q3 MECHANICS
Y. Takahashi, S. Kubota, T. Saburi
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引用次数: 0

摘要

用2.5 g烈性炸药测量了聚甲基丙烯酸甲酯(PMMA)的Hugoniot冲击波速度\((U_{\textrm{S}})\) -粒子速度\((u_{\textrm{p}})\)曲线。板的厚度变化,以准确地确定\(U_{\textrm{S}}\)在PMMA的任意位置。通过图像分析得到冲击波在PMMA中沿炸药轴向传播的x-t图,并利用其导数得到任意位置上的轴向\(U_{\textrm{S}}\)。利用压力测量结果和\(U_{\textrm{S}}\)值,根据动量守恒定律计算\(u_{\textrm{p}}\),得到PMMA的Hugoniot \(U_{\textrm{S}}\) - \(u_{\textrm{p}}\)曲线。结果与用冲击枪进行的平板冲击实验的报告值吻合得很好。研究发现,采用一种不使用平面波的简单测量方法,可以对PMMA低压侧的Hugoniot \(U_{\textrm{S}}\) - \(u_{\textrm{p}}\)曲线\((u_{\textrm{p}} < 0.5\, {\textrm{km}}/{\textrm{s}})\)进行高精度的测量。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Development of simple evaluation system for Hugoniot of polymethyl methacrylate

Development of simple evaluation system for Hugoniot of polymethyl methacrylate

The Hugoniot shock wave velocity \((U_{\textrm{S}})\)–particle velocity \((u_{\textrm{p}})\) curve of polymethyl methacrylate (PMMA) was measured in an experiment using only 2.5 g of a high explosive. The thickness of the plate was varied to accurately determine \(U_{\textrm{S}}\) at an arbitrary position in the PMMA. Image analysis was conducted to obtain the xt diagram of shock wave propagating in PMMA along the axis of the explosive, and its derivative was used to obtain the on-axis \(U_{\textrm{S}}\) at an arbitrary location. Using the pressure measurement results and \(U_{\textrm{S}}\) values, the Hugoniot \(U_{\textrm{S}}\)\(u_{\textrm{p}}\) curve of PMMA was obtained by calculating \(u_{\textrm{p}}\) from the momentum conservation law. The results are in very good agreement with the reported values for flat-plate impact experiments conducted using an impact gun. It was found that the Hugoniot \(U_{\textrm{S}}\)\(u_{\textrm{p}}\) curve of PMMA on the low-pressure side \((u_{\textrm{p}} < 0.5\, {\textrm{km}}/{\textrm{s}})\) can be evaluated with high accuracy using a simple measurement method that does not use plane waves.

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来源期刊
Shock Waves
Shock Waves 物理-力学
CiteScore
4.10
自引率
9.10%
发文量
41
审稿时长
17.4 months
期刊介绍: Shock Waves provides a forum for presenting and discussing new results in all fields where shock and detonation phenomena play a role. The journal addresses physicists, engineers and applied mathematicians working on theoretical, experimental or numerical issues, including diagnostics and flow visualization. The research fields considered include, but are not limited to, aero- and gas dynamics, acoustics, physical chemistry, condensed matter and plasmas, with applications encompassing materials sciences, space sciences, geosciences, life sciences and medicine. Of particular interest are contributions which provide insights into fundamental aspects of the techniques that are relevant to more than one specific research community. The journal publishes scholarly research papers, invited review articles and short notes, as well as comments on papers already published in this journal. Occasionally concise meeting reports of interest to the Shock Waves community are published.
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