{"title":"Fast-flame-to-detonation transition in a round tube: comparison with a square channel","authors":"M. Moran, G. Ciccarelli","doi":"10.1007/s00193-026-01279-z","DOIUrl":null,"url":null,"abstract":"<div><p>The deflagration-to-detonation transition (DDT) downstream of a 76%-blockage-ratio perforated plate was investigated in a 7.6-cm-inner-diameter polycarbonate round tube. Tests were primarily conducted in stoichiometric propane–oxygen mixtures with and without argon dilution at initial pressures of 4.2–35 kPa, and the results were compared to experiments conducted in a square channel of identical transverse dimension and with a nearly identical perforated plate. Simultaneous high-speed side- and end-view photography identified the precise location of detonation onset, and soot-coated foils provided a record of the shock dynamics preceding the onset of detonation, and the subsequent detonation cell structure. Prompt detonation initiation was independent of channel geometry, occurring at identical conditions as in the square channel. At lower initial pressures, detonation was initiated either at the channel centerline following a near-symmetric shock implosion, or subsequently following shock reflection of the near-symmetric expanding shock at the tube wall. For the “stable” argon-diluted mixtures, more reactive conditions were required for DDT in the round tube than in the square channel, demonstrating that for regular-cell structure mixtures detonation initiation is promoted by shock focusing in the channel corners. For the “unstable” <span>\\({\\textrm{C}}_{3}{\\textrm{H}}_{8}+5{\\textrm{O}}_{2}\\)</span> mixture, there was little difference in the DDT limit for the round and square channels, indicating that detonation initiation driven by hot-spot formation following transverse wave collisions is dominant, i.e., as effective as shock focusing in the corner.</p></div>","PeriodicalId":775,"journal":{"name":"Shock Waves","volume":"36 3","pages":""},"PeriodicalIF":1.8000,"publicationDate":"2026-09-06","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/s00193-026-01279-z","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
The deflagration-to-detonation transition (DDT) downstream of a 76%-blockage-ratio perforated plate was investigated in a 7.6-cm-inner-diameter polycarbonate round tube. Tests were primarily conducted in stoichiometric propane–oxygen mixtures with and without argon dilution at initial pressures of 4.2–35 kPa, and the results were compared to experiments conducted in a square channel of identical transverse dimension and with a nearly identical perforated plate. Simultaneous high-speed side- and end-view photography identified the precise location of detonation onset, and soot-coated foils provided a record of the shock dynamics preceding the onset of detonation, and the subsequent detonation cell structure. Prompt detonation initiation was independent of channel geometry, occurring at identical conditions as in the square channel. At lower initial pressures, detonation was initiated either at the channel centerline following a near-symmetric shock implosion, or subsequently following shock reflection of the near-symmetric expanding shock at the tube wall. For the “stable” argon-diluted mixtures, more reactive conditions were required for DDT in the round tube than in the square channel, demonstrating that for regular-cell structure mixtures detonation initiation is promoted by shock focusing in the channel corners. For the “unstable” \({\textrm{C}}_{3}{\textrm{H}}_{8}+5{\textrm{O}}_{2}\) mixture, there was little difference in the DDT limit for the round and square channels, indicating that detonation initiation driven by hot-spot formation following transverse wave collisions is dominant, i.e., as effective as shock focusing in the corner.
76的下游的爆燃-爆轰过渡(DDT)%-blockage-ratio perforated plate was investigated in a 7.6-cm-inner-diameter polycarbonate round tube. Tests were primarily conducted in stoichiometric propane–oxygen mixtures with and without argon dilution at initial pressures of 4.2–35 kPa, and the results were compared to experiments conducted in a square channel of identical transverse dimension and with a nearly identical perforated plate. Simultaneous high-speed side- and end-view photography identified the precise location of detonation onset, and soot-coated foils provided a record of the shock dynamics preceding the onset of detonation, and the subsequent detonation cell structure. Prompt detonation initiation was independent of channel geometry, occurring at identical conditions as in the square channel. At lower initial pressures, detonation was initiated either at the channel centerline following a near-symmetric shock implosion, or subsequently following shock reflection of the near-symmetric expanding shock at the tube wall. For the “stable” argon-diluted mixtures, more reactive conditions were required for DDT in the round tube than in the square channel, demonstrating that for regular-cell structure mixtures detonation initiation is promoted by shock focusing in the channel corners. For the “unstable” \({\textrm{C}}_{3}{\textrm{H}}_{8}+5{\textrm{O}}_{2}\) mixture, there was little difference in the DDT limit for the round and square channels, indicating that detonation initiation driven by hot-spot formation following transverse wave collisions is dominant, i.e., as effective as shock focusing in the corner.
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.