Vahid Yousefi-Asli , Shem Lau-Chapdelaine , Gaby Ciccarelli
{"title":"方形截面冲击管内正常冲击反射引发的新型弱起爆","authors":"Vahid Yousefi-Asli , Shem Lau-Chapdelaine , Gaby Ciccarelli","doi":"10.1016/j.combustflame.2024.113502","DOIUrl":null,"url":null,"abstract":"<div><p>Normal shock wave reflection driven detonation initiation was investigated in a 7.63-cm square cross-section shock tube using novel stereo visualization. High-speed schlieren video captured shock reflection and detonation onset through the sidewall of the shock tube, and simultaneously, self-luminous imaging through the end wall enabled the determination of the location of detonation onset in three-dimensional space. Tests were carried out with nitrogen- diluted stoichiometric ethylene-oxygen. Weak and strong detonation initiation modes were observed at the low and high end of the reflected shock temperature range tested, respectively. A novel reflected shock bifurcation driven weak detonation initiation mode was observed at intermediate temperatures where a flame, ignited at one, or multiple, reflecting wall corners, accelerated along the channel wall corner reaching the bifurcated reflected shock wave. The flame rapidly spread through the bifurcation stagnation bubble transitioning to detonation. The reflected shock temperature range that this new weak initiation mode was observed depends on the reflected shock pressure. For low reflected shock pressures, typical of historic detonation initiation shock reflection studies, this weak bifurcation mode was not observed. Nonreactive three-dimensional Navier-Stokes simulations showed that the reflected shock bifurcation generates flow conditions along the channel wall corners that can explain the observed flame propagation from the end wall to the stagnation bubble, and the subsequent rapid spreading in the stagnation bubble.</p></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":null,"pages":null},"PeriodicalIF":5.8000,"publicationDate":"2024-05-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Novel weak detonation initiation from normal shock reflection in square cross-section shock tubes\",\"authors\":\"Vahid Yousefi-Asli , Shem Lau-Chapdelaine , Gaby Ciccarelli\",\"doi\":\"10.1016/j.combustflame.2024.113502\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>Normal shock wave reflection driven detonation initiation was investigated in a 7.63-cm square cross-section shock tube using novel stereo visualization. High-speed schlieren video captured shock reflection and detonation onset through the sidewall of the shock tube, and simultaneously, self-luminous imaging through the end wall enabled the determination of the location of detonation onset in three-dimensional space. Tests were carried out with nitrogen- diluted stoichiometric ethylene-oxygen. Weak and strong detonation initiation modes were observed at the low and high end of the reflected shock temperature range tested, respectively. A novel reflected shock bifurcation driven weak detonation initiation mode was observed at intermediate temperatures where a flame, ignited at one, or multiple, reflecting wall corners, accelerated along the channel wall corner reaching the bifurcated reflected shock wave. The flame rapidly spread through the bifurcation stagnation bubble transitioning to detonation. The reflected shock temperature range that this new weak initiation mode was observed depends on the reflected shock pressure. For low reflected shock pressures, typical of historic detonation initiation shock reflection studies, this weak bifurcation mode was not observed. Nonreactive three-dimensional Navier-Stokes simulations showed that the reflected shock bifurcation generates flow conditions along the channel wall corners that can explain the observed flame propagation from the end wall to the stagnation bubble, and the subsequent rapid spreading in the stagnation bubble.</p></div>\",\"PeriodicalId\":280,\"journal\":{\"name\":\"Combustion and Flame\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":5.8000,\"publicationDate\":\"2024-05-31\",\"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/S0010218024002104\",\"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":"Combustion and Flame","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010218024002104","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}
Novel weak detonation initiation from normal shock reflection in square cross-section shock tubes
Normal shock wave reflection driven detonation initiation was investigated in a 7.63-cm square cross-section shock tube using novel stereo visualization. High-speed schlieren video captured shock reflection and detonation onset through the sidewall of the shock tube, and simultaneously, self-luminous imaging through the end wall enabled the determination of the location of detonation onset in three-dimensional space. Tests were carried out with nitrogen- diluted stoichiometric ethylene-oxygen. Weak and strong detonation initiation modes were observed at the low and high end of the reflected shock temperature range tested, respectively. A novel reflected shock bifurcation driven weak detonation initiation mode was observed at intermediate temperatures where a flame, ignited at one, or multiple, reflecting wall corners, accelerated along the channel wall corner reaching the bifurcated reflected shock wave. The flame rapidly spread through the bifurcation stagnation bubble transitioning to detonation. The reflected shock temperature range that this new weak initiation mode was observed depends on the reflected shock pressure. For low reflected shock pressures, typical of historic detonation initiation shock reflection studies, this weak bifurcation mode was not observed. Nonreactive three-dimensional Navier-Stokes simulations showed that the reflected shock bifurcation generates flow conditions along the channel wall corners that can explain the observed flame propagation from the end wall to the stagnation bubble, and the subsequent rapid spreading in the stagnation bubble.
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.