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首页> 外文期刊>Propellants, Explosives, Pyrotechnics >Experimental Investigation of Characteristic Length Influence on a Combustion Chamber Performance with Liquid and Gelled UDMH/IRFNA Bi‐Propellants
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Experimental Investigation of Characteristic Length Influence on a Combustion Chamber Performance with Liquid and Gelled UDMH/IRFNA Bi‐Propellants

机译：用液体凝胶化UDMH / IRFNA双推进剂对特征长度影响对燃烧室性能的实验研究

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Abstract >Gel propulsion systems are of increasing interest due to their valuable energetic and safety considerations. In this paper, performance parameters of gelled UDMH/IRFNA bi‐propellant were compared with performance parameters of its liquid bi‐propellant. Fire tests were carried out with combustion chamber pressures of about 1 to 3?MPa and L* values of 89, 127 and 162?cm. The results showed that the suitable L* to obtain best performance for liquid UDMH/IRFNA combination at the mentioned conditions was 127?cm and for gelled UDMH/IRFNA bi‐propellant was 162?cm, although the increase in performance with an increase of L* from 127 to 162?cm for the gel was very low. </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 Type =“Main”XML：Lang =“en”> <标题类型=“main”>抽象</ title> >凝胶推进系统因其有价值的能量和安全考虑而越来越兴趣。 在本文中，将凝胶化UDMH / IRFNA双推进剂的性能参数与其液体双推进剂的性能参数进行了比较。 用约1至3℃的燃烧室压力进行火试验，L *值为89,127和162Ω·cm。 结果表明，在提到的条件下获得液体UDMH / IRFNA组合的最佳性能为127Ω·cm，对于凝胶化的UDMH / IRFNA双推进剂为162Ωcm，但随着L增加的性能增加 *凝胶的127到162厘米非常低。</ 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-29946/'>《Propellants, Explosives, Pyrotechnics》</a> <b style="margin: 0 2px;">|</b><span>2019年第9期</span><b style="margin: 0 2px;">|</b><span>共6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=Moghaddam Ali Saberi&option=202" target="_blank" rel="nofollow">Moghaddam Ali Saberi;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Rezaei Mohammad Reza&option=202" target="_blank" rel="nofollow">Rezaei Mohammad Reza;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Tavangar Saeed&option=202" target="_blank" rel="nofollow">Tavangar Saeed;</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>Malek Ashtar University of TechnologyTehran I. R. Iran;</p> <p>Malek Ashtar University of TechnologyTehran I. R. Iran;</p> <p>Malek Ashtar University of TechnologyTehran I. R. Iran;</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/1837.html" title="爆炸物工业、火柴工业">爆炸物工业、火柴工业;</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=Gel propellant&option=203" rel="nofollow">Gel propellant;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Combustion chamber&option=203" rel="nofollow">Combustion chamber;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Characteristic length&option=203" rel="nofollow">Characteristic length;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Performance&option=203" rel="nofollow">Performance;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Characteristic velocity&option=203" rel="nofollow">Characteristic velocity;</a> </p> <div class="translation"> 机译：凝胶推进剂;燃烧室;特征长度;性能;特征速度; </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/0704024626591.html">Experimental Investigation of Characteristic Length Influence on a Combustion Chamber Performance with Liquid and Gelled UDMH/IRFNA Bi‐Propellants</a> <b>[J]</b> . <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Moghaddam Ali Saberi&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Moghaddam Ali Saberi,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Rezaei Mohammad Reza&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Rezaei Mohammad Reza,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Tavangar Saeed&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Tavangar Saeed </a> <a href="/journal-foreign-29946/" target="_blank" rel="nofollow" class="tuijian_authcolor">Propellants, Explosives, Pyrotechnics .</a> <span>2019</span><span>,第9期</span> </span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译：用液体凝胶化UDMH / IRFNA双推进剂对特征长度影响对燃烧室性能的实验研究</span> </p> </li> <li> <div> <b>2. </b><a class="enjiyixqcontent" href="/academic-journal-foreign_international-journal-energetic-materials-chemical-propulsion_thesis/020417938326.html">IGNITION AND COMBUSTION STUDIES OF HETEROGENEOUS UDMH-RFNA GEL PROPELLANTS</a> <b>[J]</b> . <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Mohan Varma&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Mohan Varma,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=B. 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rel="nofollow" class="tuijian_auth tuijian_authcolor">,李成</a> <span> <a href="/journal-cn-9906/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 航空工程进展 </a> </span> <span> . 2012</span><span>,第003期</span> </span> </div> </li> <li> <div> <b>6. </b><a class="enjiyixqcontent" href="/academic-conference-cn_meeting-7613_thesis/020221964838.html">高温升燃烧室与双燃烧室对航空发动机总体性能影响对比</a> <b>[C]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=毛艳辉&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 毛艳辉</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=杨金虎&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,杨金虎</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=刘存喜&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,刘存喜</a> <span> <a href="/conference-cn-7613/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 2012年中国工程热物理学会燃烧学学术年会 </a> <span> <span> . 2012</span> </span> </div> </li> <li> <div> <b>7. </b><a class="enjiyixqcontent" href="/academic-degree-domestic_mphd_thesis/020313380232.html">双取代咪唑类离子液体的凝胶化及其复合膜的制备与性能表征</a> <b>[A] </b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=王婧&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 王婧</a> <span> . 2012</span> </span> </div> </li> </ul> <ul style="display: none;"> <li> <div> <b>1. </b><a class="enjiyixqcontent" href="/patent-detail/061204621054.html">双组元液体推进剂火箭发动机燃烧室及燃烧控制方法</a> <b>[P]</b> . <span> 中国专利： CN112267956B </span> <span> . 2021.08.27</span> </div> </li> <li> <div> <b>2. </b><a class="enjiyixqcontent" href="/patent-detail/06120112258322.html">双组元液体推进剂火箭发动机燃烧室及燃烧控制方法</a> <b>[P]</b> . <span> 中国专利： CN112267956A </span> <span> . 2021-01-26</span> </div> </li> <li> <div> <b>3. </b><a class="enjiyixqcontent" href="/patent-detail/06130424367801.html">METHOD OF EXPERIMENTAL CONFIRMATION OF LIQUID-PROPELLANT ROCKET ENGINE AMPLITUDE-PHASE CHARACTERISTICS AND LIQUID-PROPELLANT ROCKET ENGINE (VERSIONS)</a> <b>[P]</b> . <span> 外国专利： <!-- 俄罗斯专利： --> RU2406858C2 </span> <span> . 2010-12-20</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译：液体火箭发动机的气态相特性和液体火箭发动机（版本）的实验验证方法 </span> </p> </li> <li> <div> <b>4. </b><a class="enjiyixqcontent" href="/patent-detail/06130465718526.html">Use of additive mixtures as a means for increasing the vaporisation rate and combustion rate and also the combustion stability of liquid propellants and fuels injected into rocket combustion chambers or high-performance combustion installations</a> <b>[P]</b> . <span> 外国专利： <!-- 德国专利： --> DE3835489A1 </span> <span> . 1990-04-19</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译：使用添加剂混合物作为增加汽化率和燃烧率以及液体推进剂和喷射到火箭燃烧室或高性能燃烧装置中的燃料的燃烧稳定性的手段 </span> </p> </li> <li> <div> <b>5. </b><a class="enjiyixqcontent" href="/patent-detail/06130448207441.html">Series generator for IC engine with unit for passage of fuel through at least one magnetic field, before this propellant is supplied to combustion chamber of IC engine for improving combustion and reducing harmful influences e.g. NOx</a> <b>[P]</b> . <span> 外国专利： <!-- 德国专利： --> DE19949806A1 </span> <span> . 2001-04-26</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译：用于该内燃机的串联发电机，其具有用于使燃料通过至少一个磁场的单元，然后将该推进剂供应到该内燃机的燃烧室，以改善燃烧并减少有害影响，例如。氮氧化物 </span> </p> </li> </ul> </div> </div> </div> <div class="theme cardcommon" style="overflow: auto;display:none"> <h3 class="all_title" id="enpatent55">相关主题</h3> <ul id="subject"> </ul> </div> </div> </div> </div> <div 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