{"title":"聚甲基丙烯酸甲酯Hugoniot简易评价系统的开发","authors":"Y. Takahashi, S. Kubota, T. Saburi","doi":"10.1007/s00193-023-01121-w","DOIUrl":null,"url":null,"abstract":"<div><p>The Hugoniot shock wave velocity <span>\\((U_{\\textrm{S}})\\)</span>–particle velocity <span>\\((u_{\\textrm{p}})\\)</span> 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 <span>\\(U_{\\textrm{S}}\\)</span> at an arbitrary position in the PMMA. Image analysis was conducted to obtain the <i>x</i>–<i>t</i> diagram of shock wave propagating in PMMA along the axis of the explosive, and its derivative was used to obtain the on-axis <span>\\(U_{\\textrm{S}}\\)</span> at an arbitrary location. Using the pressure measurement results and <span>\\(U_{\\textrm{S}}\\)</span> values, the Hugoniot <span>\\(U_{\\textrm{S}}\\)</span>–<span>\\(u_{\\textrm{p}}\\)</span> curve of PMMA was obtained by calculating <span>\\(u_{\\textrm{p}}\\)</span> 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 <span>\\(U_{\\textrm{S}}\\)</span>–<span>\\(u_{\\textrm{p}}\\)</span> curve of PMMA on the low-pressure side <span>\\((u_{\\textrm{p}} < 0.5\\, {\\textrm{km}}/{\\textrm{s}})\\)</span> can be evaluated with high accuracy using a simple measurement method that does not use plane waves.\n</p></div>","PeriodicalId":775,"journal":{"name":"Shock Waves","volume":null,"pages":null},"PeriodicalIF":1.7000,"publicationDate":"2023-04-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://link.springer.com/content/pdf/10.1007/s00193-023-01121-w.pdf","citationCount":"0","resultStr":"{\"title\":\"Development of simple evaluation system for Hugoniot of polymethyl methacrylate\",\"authors\":\"Y. Takahashi, S. Kubota, T. Saburi\",\"doi\":\"10.1007/s00193-023-01121-w\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>The Hugoniot shock wave velocity <span>\\\\((U_{\\\\textrm{S}})\\\\)</span>–particle velocity <span>\\\\((u_{\\\\textrm{p}})\\\\)</span> 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 <span>\\\\(U_{\\\\textrm{S}}\\\\)</span> at an arbitrary position in the PMMA. Image analysis was conducted to obtain the <i>x</i>–<i>t</i> diagram of shock wave propagating in PMMA along the axis of the explosive, and its derivative was used to obtain the on-axis <span>\\\\(U_{\\\\textrm{S}}\\\\)</span> at an arbitrary location. Using the pressure measurement results and <span>\\\\(U_{\\\\textrm{S}}\\\\)</span> values, the Hugoniot <span>\\\\(U_{\\\\textrm{S}}\\\\)</span>–<span>\\\\(u_{\\\\textrm{p}}\\\\)</span> curve of PMMA was obtained by calculating <span>\\\\(u_{\\\\textrm{p}}\\\\)</span> 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 <span>\\\\(U_{\\\\textrm{S}}\\\\)</span>–<span>\\\\(u_{\\\\textrm{p}}\\\\)</span> curve of PMMA on the low-pressure side <span>\\\\((u_{\\\\textrm{p}} < 0.5\\\\, {\\\\textrm{km}}/{\\\\textrm{s}})\\\\)</span> can be evaluated with high accuracy using a simple measurement method that does not use plane waves.\\n</p></div>\",\"PeriodicalId\":775,\"journal\":{\"name\":\"Shock Waves\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":1.7000,\"publicationDate\":\"2023-04-12\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://link.springer.com/content/pdf/10.1007/s00193-023-01121-w.pdf\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Shock Waves\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://link.springer.com/article/10.1007/s00193-023-01121-w\",\"RegionNum\":4,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q3\",\"JCRName\":\"MECHANICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Shock Waves","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s00193-023-01121-w","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MECHANICS","Score":null,"Total":0}
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 x–t 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.
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.