Role of the argon and helium bath gases on the structure of H2/O2 detonations

IF 6.2 2区 工程技术 Q2 ENERGY & FUELS
Farzane Zangene, Matei I. Radulescu
{"title":"Role of the argon and helium bath gases on the structure of H2/O2 detonations","authors":"Farzane Zangene,&nbsp;Matei I. Radulescu","doi":"10.1016/j.combustflame.2025.114381","DOIUrl":null,"url":null,"abstract":"<div><div>This study investigates the role of two inert mono-atomic diluents, argon and helium, on the detonation structure in order to assess the importance of vibrational non-equilibrium and wall losses. When relaxation effects and wall losses are neglected, the detonation waves in mixtures diluted with either of these gases have the same kinetics, Mach number, and specific heat ratio and hence are expected to lead to the same cellular dynamics. Differences in transport properties and species relaxation rates thus permit to establish the importance of these effects. The experiments were conducted in <span><math><mrow><mn>2</mn><msub><mrow><mtext>H</mtext></mrow><mrow><mn>2</mn></mrow></msub><mo>+</mo><msub><mrow><mtext>O</mtext></mrow><mrow><mn>2</mn></mrow></msub><mo>+</mo><mn>7</mn><mtext>Ar</mtext></mrow></math></span> and <span><math><mrow><mn>2</mn><msub><mrow><mtext>H</mtext></mrow><mrow><mn>2</mn></mrow></msub><mo>+</mo><msub><mrow><mtext>O</mtext></mrow><mrow><mn>2</mn></mrow></msub><mo>+</mo><mn>7</mn><mtext>He</mtext></mrow></math></span> mixtures in a narrow channel, where boundary layer losses can be controlled by the proximity of the detonations to their propagation limits. The initial pressure was adjusted in such a way that the induction zone length calculated from the ideal ZND model remained constant. This is expected to also constrain the cell size. The experiments revealed differences in velocity deficits and cell sizes despite maintaining a constant induction zone length across the mixtures. These differences were minimal in sensitive mixtures but became more pronounced as velocity deficits increased and cell sizes approached the channel dimensions. Near the detonation limits, the disparity in cell sizes between the two mixtures nearly doubled. We incorporated the boundary layer flow divergence in a perturbation analysis based on the square-wave detonation assumption. This permitted to establish the controlling loss parameter as the product of the induction to channel size and the inverse of the square root of the Reynolds number. The very good collapse of the experimental results with the loss parameter, and further comparison with two-dimensional numerical simulations with account for flow divergence to the third dimension, confirmed the viscous loss mechanism to be dominating. Calculations suggest that the slower relaxation of <span><math><msub><mrow><mtext>H</mtext></mrow><mrow><mn>2</mn></mrow></msub></math></span> becomes comparable with the ignition delay anticipated from the ZND model and is slower by 70% in the argon diluted system. Differences possibly highlighting the role of non-equilibrium were not observed. This suggests the vibrational non-equilibrium effect may be less apparent in cellular detonations in the system studied in this work due to the lengthening of the ignition delays owing to the non-steady detonation structure. This study establishes that the large differences between the enlarged cells observed in our experiments and numerical predictions of lossless systems can be entirely attributed to wall losses.</div><div><strong>Novelty and significance</strong></div><div>This study establishes the relative importance of vibrational non-equilibrium and boundary layer losses in controlling the detonation cellular structure in channels close to the propagation limit. The novel experimental technique consisted of changing the inert mono-atomic diluent in order to change the relaxation rates and transport coefficients, without changing the kinetics. This permitted to conclude that relaxation effects were negligible. A closed form solution for detonations with boundary layer losses was derived in the limit of high activation energy for square wave detonations. This allowed to obtain a new non-dimensional loss parameter that can scale the results obtained experimentally. An improvement over existing 2D formulation for treatment of boundary layer losses was proposed, which enabled very good agreement with experiment.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"280 ","pages":"Article 114381"},"PeriodicalIF":6.2000,"publicationDate":"2025-08-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Combustion and Flame","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010218025004183","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

Abstract

This study investigates the role of two inert mono-atomic diluents, argon and helium, on the detonation structure in order to assess the importance of vibrational non-equilibrium and wall losses. When relaxation effects and wall losses are neglected, the detonation waves in mixtures diluted with either of these gases have the same kinetics, Mach number, and specific heat ratio and hence are expected to lead to the same cellular dynamics. Differences in transport properties and species relaxation rates thus permit to establish the importance of these effects. The experiments were conducted in 2H2+O2+7Ar and 2H2+O2+7He mixtures in a narrow channel, where boundary layer losses can be controlled by the proximity of the detonations to their propagation limits. The initial pressure was adjusted in such a way that the induction zone length calculated from the ideal ZND model remained constant. This is expected to also constrain the cell size. The experiments revealed differences in velocity deficits and cell sizes despite maintaining a constant induction zone length across the mixtures. These differences were minimal in sensitive mixtures but became more pronounced as velocity deficits increased and cell sizes approached the channel dimensions. Near the detonation limits, the disparity in cell sizes between the two mixtures nearly doubled. We incorporated the boundary layer flow divergence in a perturbation analysis based on the square-wave detonation assumption. This permitted to establish the controlling loss parameter as the product of the induction to channel size and the inverse of the square root of the Reynolds number. The very good collapse of the experimental results with the loss parameter, and further comparison with two-dimensional numerical simulations with account for flow divergence to the third dimension, confirmed the viscous loss mechanism to be dominating. Calculations suggest that the slower relaxation of H2 becomes comparable with the ignition delay anticipated from the ZND model and is slower by 70% in the argon diluted system. Differences possibly highlighting the role of non-equilibrium were not observed. This suggests the vibrational non-equilibrium effect may be less apparent in cellular detonations in the system studied in this work due to the lengthening of the ignition delays owing to the non-steady detonation structure. This study establishes that the large differences between the enlarged cells observed in our experiments and numerical predictions of lossless systems can be entirely attributed to wall losses.
Novelty and significance
This study establishes the relative importance of vibrational non-equilibrium and boundary layer losses in controlling the detonation cellular structure in channels close to the propagation limit. The novel experimental technique consisted of changing the inert mono-atomic diluent in order to change the relaxation rates and transport coefficients, without changing the kinetics. This permitted to conclude that relaxation effects were negligible. A closed form solution for detonations with boundary layer losses was derived in the limit of high activation energy for square wave detonations. This allowed to obtain a new non-dimensional loss parameter that can scale the results obtained experimentally. An improvement over existing 2D formulation for treatment of boundary layer losses was proposed, which enabled very good agreement with experiment.
氩气和氦气对H2/O2爆轰结构的影响
本研究考察了两种惰性单原子稀释剂氩和氦对爆轰结构的作用,以评估振动非平衡和壁损失的重要性。当忽略松弛效应和壁面损失时,用这两种气体稀释的混合物中的爆震波具有相同的动力学、马赫数和比热比,因此预计会导致相同的细胞动力学。因此,输运性质和物种松弛率的差异可以确定这些影响的重要性。实验是在狭窄通道中的2H2+O2+7Ar和2H2+O2+7He混合物中进行的,其中边界层损失可以通过爆轰接近其传播极限来控制。调整初始压力,使从理想ZND模型计算出的感应区长度保持不变。预计这也会限制单元格的大小。实验揭示了速度缺陷和细胞大小的差异,尽管在混合物中保持恒定的诱导区长度。这些差异在敏感混合物中是最小的,但随着速度缺陷的增加和细胞尺寸接近通道尺寸而变得更加明显。在爆炸极限附近,两种混合物的电池尺寸差异几乎翻了一番。我们在方波爆轰假设的扰动分析中加入了边界层流动散度。这样就可以将控制损失参数建立为通道大小的感应与雷诺数平方根的倒数的乘积。实验结果与损失参数有很好的塌缩关系,并进一步与考虑流动散度的二维数值模拟结果进行比较,证实了粘滞损失机制占主导地位。计算表明,H2的弛豫速度与ZND模型预测的点火延迟相当,并且在氩气稀释体系中弛豫速度慢了70%。没有观察到可能突出非平衡作用的差异。这表明,在本工作所研究的系统中,振动非平衡效应可能不太明显,这是由于非稳态爆轰结构延长了点火延迟。本研究表明,在我们的实验中观察到的增大细胞与无损系统的数值预测之间的巨大差异可以完全归因于壁损失。本研究确立了振动非平衡和边界层损失在控制接近传播极限的通道内爆轰细胞结构方面的相对重要性。在不改变动力学的前提下,通过改变惰性单原子稀释剂来改变弛豫速率和输运系数。由此可以得出松弛效应可以忽略不计的结论。在方波爆轰的高活化能极限下,导出了边界层损失爆轰的封闭解。这允许获得一个新的无量纲损失参数,可以缩放实验得到的结果。对现有二维边界层损失处理公式进行了改进,与实验结果吻合较好。
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
Combustion and Flame
Combustion and Flame 工程技术-工程:化工
CiteScore
9.50
自引率
20.50%
发文量
631
审稿时长
3.8 months
期刊介绍: The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on: Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including: Conventional, alternative and surrogate fuels; Pollutants; Particulate and aerosol formation and abatement; Heterogeneous processes. Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including: Premixed and non-premixed flames; Ignition and extinction phenomena; Flame propagation; Flame structure; Instabilities and swirl; Flame spread; Multi-phase reactants. Advances in diagnostic and computational methods in combustion, including: Measurement and simulation of scalar and vector properties; Novel techniques; State-of-the art applications. Fundamental investigations of combustion technologies and systems, including: Internal combustion engines; Gas turbines; Small- and large-scale stationary combustion and power generation; Catalytic combustion; Combustion synthesis; Combustion under extreme conditions; New concepts.
×
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:604180095
Book学术官方微信