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Study on correlation between geometrical correction and aerodynamic performance of microscale supersonic wind tunnel

机译：微观超声隧道几何校正与空气动力学性能的相关性研究

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Abstract >In this paper, flow visualization of the oblique shock waves of a single‐crystal silicon microscale supersonic wind tunnel is described. The microscale supersonic wind tunnel has a convergent–divergent section and a throat area of 1000?μm × 300?μm, and designed for realizing supersonic flow of Mach 2 in microscale domain. The schlieren system with integrated optical microscope was used for visualization of the oblique shock waves generated in the microscale domain. To investigate the effect of nonisentropic flow state on the inclination angle to the shock, a numerical integration of the modified Shapiro's differential equation was applied. </abstract> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> <div class="translation abstracttxt"> <span class="zhankaihshouqi fivelineshidden" id="abstract"> <span>机译：</span><Abstract XMLNS =“http://www.wiley.com/namespaces/wiley”type =“main”xml：lang =“en”> <标题类型=“main”>抽象</ title> 在本文中，描述了单晶硅微观超声隧道的倾斜冲击波的流动可视化。微观超声波风隧道具有会聚 - 发散部分和喉部面积为1000？μm×300≤μm，并设计用于在微观域中实现Mach 2的超音速流动。具有集成光学显微镜的Schlieren系统用于可视化微观域中产生的倾斜冲击波。为了研究对倾斜角对冲击的倾斜角度的影响，应用了改进的Shapiro的微分方程的数值积分。</ p> </摘要> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> </div> <div class="record"> <h2 class="all_title" id="enpatent33" >著录项</h2> <ul> <li> <span class="lefttit">来源</span> <div style="width: 86%;vertical-align: text-top;display: inline-block;"> <a href='/journal-foreign-22399/'>《Electrical engineering in Japan》</a> <b style="margin: 0 2px;">|</b><span>2018年第1期</span><b style="margin: 0 2px;">|</b><span>共9页</span> </div> </li> <li> <div class="author"> <span class="lefttit">作者</span> <p id="fAuthorthree" class="threelineshidden zhankaihshouqi"> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Murai Naoki&option=202" target="_blank" rel="nofollow">Murai Naoki;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Yamamoto Ryouto&option=202" target="_blank" rel="nofollow">Yamamoto Ryouto;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Rikuno Kouhei&option=202" target="_blank" rel="nofollow">Rikuno Kouhei;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Toriyama Toshiyuki&option=202" target="_blank" rel="nofollow">Toriyama Toshiyuki;</a> </p> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zkzz" style="display: none;">展开▼</span> </div> </li> <li> <div style="display: flex;"> <span class="lefttit">作者单位</span> <div style="position: relative;margin-left: 3px;max-width: 639px;"> <div class="threelineshidden zhankaihshouqi" id="fOrgthree"> <p>College of Science and EngineeringRitsumeikan UniversityJapan;</p> <p>College of Science and EngineeringRitsumeikan UniversityJapan;</p> <p>College of Science and EngineeringRitsumeikan UniversityJapan;</p> <p>College of Science and EngineeringRitsumeikan UniversityJapan;</p> </div> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zhdw" style="display: none;">展开▼</span> </div> </div> </li> <li > <span class="lefttit">收录信息</span> <span style="width: 86%;vertical-align: text-top;display: inline-block;"></span> </li> <li> <span class="lefttit">原文格式</span> <span>PDF</span> </li> <li> <span class="lefttit">正文语种</span> <span>eng</span> </li> <li> <span class="lefttit">中图分类</span> <span><a href="https://www.zhangqiaokeyan.com/clc/1782.html" title="输配电工程、电力网及电力系统">输配电工程、电力网及电力系统;</a></span> </li> <li class="antistop"> <span class="lefttit">关键词</span> <p style="width: 86%;vertical-align: text-top;"> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=method of characteristics&option=203" rel="nofollow">method of characteristics;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=microscale supersonic wind tunnel&option=203" rel="nofollow">microscale supersonic wind tunnel;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=oblique shock wave&option=203" rel="nofollow">oblique shock wave;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=schlieren system&option=203" rel="nofollow">schlieren system;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Shapiro's differential equation&option=203" rel="nofollow">Shapiro's differential equation;</a> </p> <div class="translation"> 机译：特性方法;微观超声波风洞;斜冲击波;Schlieren系统;Shapiro的微分方程; </div> </li> </ul> </div> </div> <div class="literature cardcommon"> <div class="similarity "> <h3 class="all_title" id="enpatent66">相似文献</h3> <div class="similaritytab clearfix"> <ul> <li class="active" >外文文献</li> <li >中文文献</li> <li >专利</li> </ul> </div> <div class="similarity_details"> <ul > <li> <div> <b>1. </b><a class="enjiyixqcontent" href="/journal-foreign-detail/0704023149879.html">Study on correlation between geometrical correction and aerodynamic performance of microscale supersonic wind tunnel</a> <b>[J]</b> . <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Murai Naoki&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Murai Naoki,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Yamamoto Ryouto&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Yamamoto Ryouto,</a> <a 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