温度干扰对末端气体自燃和爆燃发展的影响

IF 5.3 2区 工程技术 Q2 ENERGY & FUELS Proceedings of the Combustion Institute Pub Date : 2024-07-02 DOI:10.1016/j.proci.2024.105220
Linlin Yang, Yiqing Wang, Peng Dai, Zheng Chen
{"title":"温度干扰对末端气体自燃和爆燃发展的影响","authors":"Linlin Yang, Yiqing Wang, Peng Dai, Zheng Chen","doi":"10.1016/j.proci.2024.105220","DOIUrl":null,"url":null,"abstract":"Knocking is one of the main constrains in improving the thermal efficiency of spark ignition engines. It is generally accepted that normal knock and super-knock are respectively caused by autoignition and detonation development in end-gas. In this study, the effect of temperature disturbance on end-gas autoignition and detonation development in a closed circular domain is examined through 2D simulations considering detailed chemistry. In simulations we find typical end-gas combustion modes including triple-detonation, double-detonation and double-tongue structures, which were also observed in previous rapid compression machine (RCM) experiments. It is shown that the detonation development in end-gas is very sensitive to the temperature disturbance, Δ. As Δ increases, the first autoignition in end-gas induced by temperature disturbance occurs earlier while the corresponding pressure wave is weaker, which subsequently results in different combustion modes in end-gas. Specifically, for small Δ, a supersonic autoignition is initiated and then it triggers a triple-detonation structure consisting of a radial detonation induced by shock-flame coupling and two circumferential detonations that are caused by the near-wall shock compression induced detonation (NWSCD) mechanism. For moderate Δ, the radial detonation is suppressed due to the earlier first autoignition and weaker pressure waves, and thereby the double-detonation structure consisting of two circumferential detonations appears. These two detonations are formed through near wall autoignition induced detonation (NWAID) mechanism. For relatively large Δ, there is no detonation development since the end-gas is quickly consumed by autoignition, which results in a double autoignition front structure, referred to as the double-tongue structure. In this study, the formation of complicated autoignition and detonation structures is interpreted. The results provide insight in understanding the development of normal knock and super-knock in spark ignition engines.","PeriodicalId":408,"journal":{"name":"Proceedings of the Combustion Institute","volume":null,"pages":null},"PeriodicalIF":5.3000,"publicationDate":"2024-07-02","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Effect of temperature disturbance on end-gas autoignition and detonation development\",\"authors\":\"Linlin Yang, Yiqing Wang, Peng Dai, Zheng Chen\",\"doi\":\"10.1016/j.proci.2024.105220\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Knocking is one of the main constrains in improving the thermal efficiency of spark ignition engines. It is generally accepted that normal knock and super-knock are respectively caused by autoignition and detonation development in end-gas. In this study, the effect of temperature disturbance on end-gas autoignition and detonation development in a closed circular domain is examined through 2D simulations considering detailed chemistry. In simulations we find typical end-gas combustion modes including triple-detonation, double-detonation and double-tongue structures, which were also observed in previous rapid compression machine (RCM) experiments. It is shown that the detonation development in end-gas is very sensitive to the temperature disturbance, Δ. As Δ increases, the first autoignition in end-gas induced by temperature disturbance occurs earlier while the corresponding pressure wave is weaker, which subsequently results in different combustion modes in end-gas. Specifically, for small Δ, a supersonic autoignition is initiated and then it triggers a triple-detonation structure consisting of a radial detonation induced by shock-flame coupling and two circumferential detonations that are caused by the near-wall shock compression induced detonation (NWSCD) mechanism. For moderate Δ, the radial detonation is suppressed due to the earlier first autoignition and weaker pressure waves, and thereby the double-detonation structure consisting of two circumferential detonations appears. These two detonations are formed through near wall autoignition induced detonation (NWAID) mechanism. For relatively large Δ, there is no detonation development since the end-gas is quickly consumed by autoignition, which results in a double autoignition front structure, referred to as the double-tongue structure. In this study, the formation of complicated autoignition and detonation structures is interpreted. The results provide insight in understanding the development of normal knock and super-knock in spark ignition engines.\",\"PeriodicalId\":408,\"journal\":{\"name\":\"Proceedings of the Combustion Institute\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":5.3000,\"publicationDate\":\"2024-07-02\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceedings of the Combustion Institute\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.1016/j.proci.2024.105220\",\"RegionNum\":2,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENERGY & FUELS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceedings of the Combustion Institute","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.1016/j.proci.2024.105220","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0

摘要

爆震是提高火花点火发动机热效率的主要制约因素之一。一般认为,正常爆震和超级爆震分别是由尾气中的自燃和爆震发展引起的。在本研究中,我们通过二维模拟研究了温度扰动对封闭圆域中尾气自燃和爆燃发展的影响,并考虑了详细的化学成分。在模拟中,我们发现了典型的尾气燃烧模式,包括三重爆燃、双重爆燃和双舌结构,这些在之前的快速压缩机(RCM)实验中也有观察到。研究表明,尾气中的爆燃发展对温度扰动 Δ 非常敏感。随着 Δ 的增大,温度扰动引起的尾气中的第一次自燃会提前发生,而相应的压力波会减弱,从而导致尾气中出现不同的燃烧模式。具体来说,当Δ较小时,超音速自燃开始,然后引发三重爆燃结构,包括由冲击-火焰耦合诱发的径向爆燃和由近壁冲击压缩诱发爆燃(NWSCD)机制引起的两个周向爆燃。对于中等Δ,由于第一次自燃较早且压力波较弱,径向爆轰受到抑制,因此出现了由两个周向爆轰组成的双爆轰结构。这两个爆轰是通过近壁自燃诱发爆轰(NWAID)机制形成的。对于相对较大的Δ,由于末端气体很快被自燃消耗,因此没有爆轰发展,从而形成双自燃前沿结构,称为双舌结构。本研究解释了复杂自燃和起爆结构的形成。研究结果有助于理解火花点火发动机中正常爆震和超级爆震的发展。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Effect of temperature disturbance on end-gas autoignition and detonation development
Knocking is one of the main constrains in improving the thermal efficiency of spark ignition engines. It is generally accepted that normal knock and super-knock are respectively caused by autoignition and detonation development in end-gas. In this study, the effect of temperature disturbance on end-gas autoignition and detonation development in a closed circular domain is examined through 2D simulations considering detailed chemistry. In simulations we find typical end-gas combustion modes including triple-detonation, double-detonation and double-tongue structures, which were also observed in previous rapid compression machine (RCM) experiments. It is shown that the detonation development in end-gas is very sensitive to the temperature disturbance, Δ. As Δ increases, the first autoignition in end-gas induced by temperature disturbance occurs earlier while the corresponding pressure wave is weaker, which subsequently results in different combustion modes in end-gas. Specifically, for small Δ, a supersonic autoignition is initiated and then it triggers a triple-detonation structure consisting of a radial detonation induced by shock-flame coupling and two circumferential detonations that are caused by the near-wall shock compression induced detonation (NWSCD) mechanism. For moderate Δ, the radial detonation is suppressed due to the earlier first autoignition and weaker pressure waves, and thereby the double-detonation structure consisting of two circumferential detonations appears. These two detonations are formed through near wall autoignition induced detonation (NWAID) mechanism. For relatively large Δ, there is no detonation development since the end-gas is quickly consumed by autoignition, which results in a double autoignition front structure, referred to as the double-tongue structure. In this study, the formation of complicated autoignition and detonation structures is interpreted. The results provide insight in understanding the development of normal knock and super-knock in spark ignition engines.
求助全文
通过发布文献求助,成功后即可免费获取论文全文。 去求助
来源期刊
Proceedings of the Combustion Institute
Proceedings of the Combustion Institute 工程技术-工程:化工
CiteScore
7.00
自引率
0.00%
发文量
420
审稿时长
3.0 months
期刊介绍: The Proceedings of the Combustion Institute contains forefront contributions in fundamentals and applications of combustion science. For more than 50 years, the Combustion Institute has served as the peak international society for dissemination of scientific and technical research in the combustion field. In addition to author submissions, the Proceedings of the Combustion Institute includes the Institute''s prestigious invited strategic and topical reviews that represent indispensable resources for emergent research in the field. All papers are subjected to rigorous peer review. Research papers and invited topical reviews; Reaction Kinetics; Soot, PAH, and other large molecules; Diagnostics; Laminar Flames; Turbulent Flames; Heterogeneous Combustion; Spray and Droplet Combustion; Detonations, Explosions & Supersonic Combustion; Fire Research; Stationary Combustion Systems; IC Engine and Gas Turbine Combustion; New Technology Concepts The electronic version of Proceedings of the Combustion Institute contains supplemental material such as reaction mechanisms, illustrating movies, and other data.
期刊最新文献
Spray and combustion characterization under an ultra-high-density condition – Multi-fuel comparison Impact of carbon-free fuels addition on self-excited combustion oscillations in partially premixed CH4/air swirl flames Enhanced combustion performance and reduced NOx emissions during chemical looping ammonia combustion with Cu-Fe oxygen carrier Co-oxidation of pyridine and pyrrole as a dual component model compound of fuel nitrogen in coal Investigation of burning velocity of lean and rich premixed NH3/H2 turbulent flames using multi-scalar imaging
×
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
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 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 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1