{"title":"Effect of methane addition to hydrogen–air mixtures on the transition to detonation due to shock wave focusing in a \\(90^{\\circ }\\) wedge","authors":"S. Khair Allah, W. Rudy, A. Teodorczyk","doi":"10.1007/s00193-025-01217-5","DOIUrl":null,"url":null,"abstract":"<div><p>This work presents the experimental investigation of the influence of methane addition to <span>\\({\\hbox {CH}}_{{4}}\\)</span>–<span>\\(\\hbox {H}_{{2}}\\)</span>–air mixture (<span>\\(\\varphi = 0.8\\)</span>–1.6) on the critical conditions for transition to detonation in a <span>\\(90^{\\circ }\\)</span> wedge. Similar to <span>\\(\\hbox {H}_{{2}}\\)</span>–air mixtures investigated previously, for <span>\\({\\hbox {CH}}_{{4}}\\)</span>–<span>\\({\\hbox {H}}_{{2}}\\)</span>–air mixtures results showed three ignition modes: (i) flame ignition with ignition delay time longer than 1 µs, (ii) strong ignition with instantaneous transition to detonation, and (iii) weak ignition with delayed transition to detonation. In a stoichiometric mixture with 5% <span>\\({\\hbox {CH}}_{{4}}\\)</span> (i.e., 95% <span>\\({\\hbox {H}}_{{2}}\\)</span> in fuel), the transition to detonation corresponds to a shock velocity of roughly 752 m/s (an increase of 37 m/s from that obtained in <span>\\(\\hbox {H}_{{2}}\\)</span>–air) corresponding to <span>\\(M = 1.89\\)</span>. In general, 5% <span>\\(\\hbox {CH}_{{4}}\\)</span> addition caused an increase of 3.25–5.03% in the critical shock wave velocity necessary for transition to detonation for all lean and rich mixtures considered. Also, similar to that found for <span>\\({\\hbox {H}}_{{2}}\\)</span>–air mixtures, the transition-to-detonation velocity increased for a leaner and richer mixture. Moreover, it was observed that methane addition in general increased the pressure limit at the wedge tip necessary for the transition to detonation.</p></div>","PeriodicalId":775,"journal":{"name":"Shock Waves","volume":"35 3","pages":"249 - 255"},"PeriodicalIF":1.7000,"publicationDate":"2025-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Shock Waves","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s00193-025-01217-5","RegionNum":4,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q3","JCRName":"MECHANICS","Score":null,"Total":0}
引用次数: 0
Abstract
This work presents the experimental investigation of the influence of methane addition to \({\hbox {CH}}_{{4}}\)–\(\hbox {H}_{{2}}\)–air mixture (\(\varphi = 0.8\)–1.6) on the critical conditions for transition to detonation in a \(90^{\circ }\) wedge. Similar to \(\hbox {H}_{{2}}\)–air mixtures investigated previously, for \({\hbox {CH}}_{{4}}\)–\({\hbox {H}}_{{2}}\)–air mixtures results showed three ignition modes: (i) flame ignition with ignition delay time longer than 1 µs, (ii) strong ignition with instantaneous transition to detonation, and (iii) weak ignition with delayed transition to detonation. In a stoichiometric mixture with 5% \({\hbox {CH}}_{{4}}\) (i.e., 95% \({\hbox {H}}_{{2}}\) in fuel), the transition to detonation corresponds to a shock velocity of roughly 752 m/s (an increase of 37 m/s from that obtained in \(\hbox {H}_{{2}}\)–air) corresponding to \(M = 1.89\). In general, 5% \(\hbox {CH}_{{4}}\) addition caused an increase of 3.25–5.03% in the critical shock wave velocity necessary for transition to detonation for all lean and rich mixtures considered. Also, similar to that found for \({\hbox {H}}_{{2}}\)–air mixtures, the transition-to-detonation velocity increased for a leaner and richer mixture. Moreover, it was observed that methane addition in general increased the pressure limit at the wedge tip necessary for the transition to detonation.
本文介绍了在\({\hbox {CH}}_{{4}}\) - \(\hbox {H}_{{2}}\) -空气混合物(\(\varphi = 0.8\) - 1.6)中加入甲烷对\(90^{\circ }\)楔形过渡到爆轰临界条件的影响的实验研究。与之前研究的\(\hbox {H}_{{2}}\) -空气混合物类似,\({\hbox {CH}}_{{4}}\) - \({\hbox {H}}_{{2}}\) -空气混合物的结果显示出三种点火模式:(i)火焰点火,点火延迟时间大于1µs; (ii)强点火,瞬时过渡到爆轰;(iii)弱点火,延迟过渡到爆轰。在化学计量混合物中加入5% \({\hbox {CH}}_{{4}}\) (i.e., 95% \({\hbox {H}}_{{2}}\) in fuel), the transition to detonation corresponds to a shock velocity of roughly 752 m/s (an increase of 37 m/s from that obtained in \(\hbox {H}_{{2}}\)–air) corresponding to \(M = 1.89\). In general, 5% \(\hbox {CH}_{{4}}\) addition caused an increase of 3.25–5.03% in the critical shock wave velocity necessary for transition to detonation for all lean and rich mixtures considered. Also, similar to that found for \({\hbox {H}}_{{2}}\)–air mixtures, the transition-to-detonation velocity increased for a leaner and richer mixture. Moreover, it was observed that methane addition in general increased the pressure limit at the wedge tip necessary for the transition to detonation.
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.