Detonation wave propagation through a single orifice plate in a circular tube

G. Ciccarelli, J.L. Boccio
{"title":"Detonation wave propagation through a single orifice plate in a circular tube","authors":"G. Ciccarelli,&nbsp;J.L. Boccio","doi":"10.1016/S0082-0784(98)80072-6","DOIUrl":null,"url":null,"abstract":"<div><p>Detonation behavior associated with the propagation of a detonation wave through an orifice plate located within a circular tube is investigated. The tube and orifice diameter used in the study are 27.3 cm and 10 cm, respectively. The test gas used is hydrogen-air at 1 atmosphere and at various initial temperatures up to 650 K. Immediately after the orifice, the detonation wave decouples and either fails or reinitiates. The reinitiation process is characterized by either spontaneous initiation, initiation due to shock reflection, or deflagration-to-detonation transition (DDT). In the case of DDT, transition is preceded by the degeneration of the decoupled detonation wave to a velocity consistent with a CJ deflagration. Delineation between these various propagation regimes could not be correlated with the detonation cell size, λ, and orifice diameter, <em>d</em>. The data, although limited, demonstrate for the first time that the <em>d<sub>c</sub>/λ</em>=13 critical tube criterion obtained at room temperature may not apply at elevated temperature conditions. The evidence for this is data obtained at 500 K that shows no detonation transmission for 30% hydrogen in air that corresponds to <em>d/λ</em>=16.7. The tests also indicate that a simple <em>d/λ</em> correlation cannot be used to determine when reinitiation due to shock reflection is possible. For example, at 650 K detonation wave failure was observed for <em>d/λ</em>&lt;7.4, and at 300 K failure was observed for <em>d/λ</em>&lt;11.</p></div>","PeriodicalId":101203,"journal":{"name":"Symposium (International) on Combustion","volume":"27 2","pages":"Pages 2233-2239"},"PeriodicalIF":0.0000,"publicationDate":"1998-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S0082-0784(98)80072-6","citationCount":"37","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Symposium (International) on Combustion","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0082078498800726","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 37

Abstract

Detonation behavior associated with the propagation of a detonation wave through an orifice plate located within a circular tube is investigated. The tube and orifice diameter used in the study are 27.3 cm and 10 cm, respectively. The test gas used is hydrogen-air at 1 atmosphere and at various initial temperatures up to 650 K. Immediately after the orifice, the detonation wave decouples and either fails or reinitiates. The reinitiation process is characterized by either spontaneous initiation, initiation due to shock reflection, or deflagration-to-detonation transition (DDT). In the case of DDT, transition is preceded by the degeneration of the decoupled detonation wave to a velocity consistent with a CJ deflagration. Delineation between these various propagation regimes could not be correlated with the detonation cell size, λ, and orifice diameter, d. The data, although limited, demonstrate for the first time that the dc=13 critical tube criterion obtained at room temperature may not apply at elevated temperature conditions. The evidence for this is data obtained at 500 K that shows no detonation transmission for 30% hydrogen in air that corresponds to d/λ=16.7. The tests also indicate that a simple d/λ correlation cannot be used to determine when reinitiation due to shock reflection is possible. For example, at 650 K detonation wave failure was observed for d/λ<7.4, and at 300 K failure was observed for d/λ<11.

爆震波在圆管内单孔板中的传播
研究了爆轰波在圆管内孔板中的传播与爆轰行为。研究中使用的管径27.3 cm,孔径10 cm。所使用的测试气体是氢-空气,在1个大气压下,在高达650 K的各种初始温度下。在孔口之后,爆震波立即解耦,要么失效,要么重新启动。再起爆过程的特点是自发起爆,由于冲击反射起爆,或爆燃到爆轰过渡(DDT)。在滴滴涕的情况下,过渡之前,解耦爆震波退化到与CJ爆燃一致的速度。这些不同传播模式之间的描述不能与爆轰池尺寸、λ和孔直径d相关联。数据虽然有限,但首次证明了在室温下获得的dc/λ=13临界管准则可能不适用于高温条件。证据是在500k下获得的数据,表明空气中30%的氢没有爆轰传输,对应于d/λ=16.7。试验还表明,不能使用简单的d/λ相关性来确定何时可能由于冲击反射而重新起爆。例如,650 K时爆震波破坏为d/λ<7.4, 300 K时爆震波破坏为d/λ<11。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信