Marwaan Al-Khafaji , Junfeng Yang , Alison S. Tomlin , Harvey M. Thompson , Gregory de Boer , Kexin Liu
{"title":"The measurement of turbulent burning velocities of methane-hydrogen-air mixtures at elevated pressures in a spherical vessel","authors":"Marwaan Al-Khafaji , Junfeng Yang , Alison S. Tomlin , Harvey M. Thompson , Gregory de Boer , Kexin Liu","doi":"10.1016/j.combustflame.2024.113907","DOIUrl":null,"url":null,"abstract":"<div><div>Few previous experimental studies have focused on pre-mixed turbulent burning velocities (<em>u<sub>t</sub></em>) for hydrogen/air and methane/hydrogen/air mixtures, especially at the high-pressure conditions most relevant to gas turbine applications. This work employed a Schlieren technique to measure flame speeds for such mixtures in a spherical stainless steel combustion vessel, from which turbulent burning velocities were derived. The hydrogen volume fractions in methane were 30, 50, 70 and 100%. The initial pressures were 0.1, 0.5 and 1.0 MPa, and the initial temperatures were 303 and 360 K. The equivalence ratio (ϕ) was varied between 0.5 and 2 for pure hydrogen and from 0.8 to 1.2 for methane/hydrogen mixtures. The root mean square (rms) turbulent velocity (<em>u’</em>) was varied from 2.0 to 10.0 ms<sup>−1</sup>. The objectives of this study are: (a) to present an extensive experimental database of turbulent burning velocities for these mixtures over a wide range of conditions; (b) to establish a new correlation for <em>u<sub>t</sub></em> for a flame with Lewis numbers, <em>Le,</em> not equal to unity, and (c) to quantify the dependence of turbulent burning velocity on pressure, temperature, stretch rate, laminar flame instability and rms velocity. As the pressure increased, the Taylor length scales decreased, and positive stretch increased, increasing flame wrinkling and <em>u<sub>t</sub></em>. The <em>u<sub>t</sub></em> also increased as the temperature and <em>u’</em> increased. The fuel/air mixture with high laminar flame instability (<em>Le<1</em>) has higher <em>u<sub>t</sub></em> than those with higher <em>Le</em>. However, the normalised <em>u<sub>t</sub></em> peaked in the region of high laminar burning velocity. This study concluded that the increase in <em>u<sub>t</sub></em> resulting from flame reactivity (laminar burning velocity) is more important than that from positive stretch (negative <em>Ma<sub>b</sub></em>) and flame instability.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"272 ","pages":"Article 113907"},"PeriodicalIF":5.8000,"publicationDate":"2025-02-01","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/S0010218024006163","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
Few previous experimental studies have focused on pre-mixed turbulent burning velocities (ut) for hydrogen/air and methane/hydrogen/air mixtures, especially at the high-pressure conditions most relevant to gas turbine applications. This work employed a Schlieren technique to measure flame speeds for such mixtures in a spherical stainless steel combustion vessel, from which turbulent burning velocities were derived. The hydrogen volume fractions in methane were 30, 50, 70 and 100%. The initial pressures were 0.1, 0.5 and 1.0 MPa, and the initial temperatures were 303 and 360 K. The equivalence ratio (ϕ) was varied between 0.5 and 2 for pure hydrogen and from 0.8 to 1.2 for methane/hydrogen mixtures. The root mean square (rms) turbulent velocity (u’) was varied from 2.0 to 10.0 ms−1. The objectives of this study are: (a) to present an extensive experimental database of turbulent burning velocities for these mixtures over a wide range of conditions; (b) to establish a new correlation for ut for a flame with Lewis numbers, Le, not equal to unity, and (c) to quantify the dependence of turbulent burning velocity on pressure, temperature, stretch rate, laminar flame instability and rms velocity. As the pressure increased, the Taylor length scales decreased, and positive stretch increased, increasing flame wrinkling and ut. The ut also increased as the temperature and u’ increased. The fuel/air mixture with high laminar flame instability (Le<1) has higher ut than those with higher Le. However, the normalised ut peaked in the region of high laminar burning velocity. This study concluded that the increase in ut resulting from flame reactivity (laminar burning velocity) is more important than that from positive stretch (negative Mab) and flame instability.
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.