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稀释气体对甲烷层流预混火焰燃烧速度的影响 被引量:5
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作者 曹甄俊 朱彤 《同济大学学报(自然科学版)》 EI CAS CSCD 北大核心 2011年第10期1557-1562,共6页
基于GRI-Mech 3.0详细化学反应机理,利用预混燃烧模型(PREMIX Code)研究了甲烷-空气-稀释气层流预混火焰燃烧特性及火焰结构.重点探讨了不同化学当量比(0.5~1.5)、初始压力(0.05~0.40MPa)、稀释气体种类(N2,CO2及H2O)和稀释摩尔比(0~... 基于GRI-Mech 3.0详细化学反应机理,利用预混燃烧模型(PREMIX Code)研究了甲烷-空气-稀释气层流预混火焰燃烧特性及火焰结构.重点探讨了不同化学当量比(0.5~1.5)、初始压力(0.05~0.40MPa)、稀释气体种类(N2,CO2及H2O)和稀释摩尔比(0~0.35)对甲烷-空气-稀释气混合气层流预混火焰结构、层流燃烧速度、火焰厚度的影响.研究结果表明:随着稀释比的增加,层流燃烧速度逐渐变小,火焰厚度增大,火焰流动不稳定性得到抑制;CO2作为稀释气时对层流燃烧速度及火焰厚度影响最为显著.随着初始压力提高,层流燃烧速度及火焰厚度均变小;进一步提高初始压力,对火焰厚度影响并不明显. 展开更多
关键词 甲烷 层流预混火焰 层流火焰燃烧速度 稀释
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国内火焰燃烧速度测试研究现状浅析
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作者 马莉 《机械管理开发》 2009年第2期76-77,共2页
对目前国内火焰燃烧速度测量的进展情况进行了评述,以便从整体上了解这一方面的研究程度、研究热点和研究方法。
关键词 火焰燃烧速度 光电传感器 敏感元件
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管道内火焰燃烧速度测试电路设计
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作者 马莉 《机械工程与自动化》 2009年第2期147-148,共2页
气体及粉尘在管道内的燃烧爆炸特性可由火焰燃烧速度这一指标来衡量,这就要求有一套专门用于测试管道内火焰燃烧速度的装置,为此设计了火焰燃烧速度测试电路以实现火焰速度的测试。
关键词 火焰燃烧速度 燃烧速度测试电路 时基信号
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水蒸汽对焦炉气火焰燃烧速度及NO生成特性影响研究
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作者 刘自涛 《电力学报》 2013年第1期81-84,共4页
以山西华鑫肥业有限公司富氧空气转化炉为研究对象,大型化学动力学软件CHEMKIN为计算平台,采用包含53种组分、325个基元反应的甲烷燃烧详细反应机理(GRI-Mech 3.0),研究了水蒸汽对富氧空气转化炉烧嘴火焰燃烧速度及NO生成特性的影响。... 以山西华鑫肥业有限公司富氧空气转化炉为研究对象,大型化学动力学软件CHEMKIN为计算平台,采用包含53种组分、325个基元反应的甲烷燃烧详细反应机理(GRI-Mech 3.0),研究了水蒸汽对富氧空气转化炉烧嘴火焰燃烧速度及NO生成特性的影响。计算结果表明:H2O对燃烧速度的影响主要是通过解离出的H自由基参与燃烧反应引起的;H2O含量的提高可以有效抑制NO生成速率。 展开更多
关键词 燃烧反应机理 火焰燃烧速度 NO生成速率 CHEMKIN
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Jet-A表征燃料/乙醇掺混燃料层流燃烧特性研究
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作者 何旭 江正晖 +4 位作者 桑正 刘泽昌 冯光远 杨青 蒋厚实 《北京理工大学学报》 EI CAS CSCD 北大核心 2023年第7期712-718,共7页
为了研究初始温度470 K、初始压力0.1 MPa下乙醇掺混对航空煤油层流火焰燃烧特性的影响,文中利用定容燃烧弹设备结合仿真进行对比分析。结果表明,乙醇的加入显著提升了航空煤油的层流火焰燃烧速度,但仿真结果与试验数据之间存在较大的偏... 为了研究初始温度470 K、初始压力0.1 MPa下乙醇掺混对航空煤油层流火焰燃烧特性的影响,文中利用定容燃烧弹设备结合仿真进行对比分析。结果表明,乙醇的加入显著提升了航空煤油的层流火焰燃烧速度,但仿真结果与试验数据之间存在较大的偏差,在低当量比时尤为严重,需进一步优化机理。在此基础上通过敏感性分析,发现对层流火焰燃烧速度影响较大的4个基元反应,通过对4个基元反应的参数进行调整,修改得到新模型,该模型与试验值存在较好的吻合度。 展开更多
关键词 航空煤油 乙醇 层流火焰燃烧速度 敏感性分析
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Numerical Study on Laminar Burning Velocity and Flame Stability of Premixed Methane/Ethylene/Air Flames 被引量:1
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作者 陈珊珊 蒋勇 +1 位作者 邱榕 安江涛 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2012年第5期914-922,共9页
A numerical study on premixed methane/ethylene/air flames with various ethylene fractions and equivalence ratios was conducted at room temperature and atmospheric pressure. The effects of ethylene addition on laminar ... A numerical study on premixed methane/ethylene/air flames with various ethylene fractions and equivalence ratios was conducted at room temperature and atmospheric pressure. The effects of ethylene addition on laminar burning velocity, flame structure and flame stability under the condition of lean burning were investigated. The results show that the laminar burning velocity increases with ethylene fraction, especially at a large equivalence ratio. More ethylene addition gives rise to higher concentrations of H, O and OH radicals in the flame, which significantly promotes chemical reactions, and a linear correlation exists between the laminar burning velocity and the maximum H + OH concentration in the reaction zone. With the increase of ethylene fraction, the adiabatic flame temperature is raised, while the inner layer temperature becomes lower, contributing to the enhancement of combustion. Markstein length and Markstein number, representative of the flame stability, increase as more ethylene is added, indicating the tendency of flame stability to improve with ethylene addition. 展开更多
关键词 laminar burning velocity flame stability METHANE ETHYLENE
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Response of Stretched Cylindrical Diffusion Flame to Sinusoidal Oscillation of Air Flow Velocity
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作者 Yosuke Suenaga Hideki Yanaoka +1 位作者 Mamoru Kikuchi Shun Sasaki 《Journal of Mechanics Engineering and Automation》 2017年第6期321-326,共6页
An experimental study investigated the characteristics of a stretched cylindrical diffusion flame, with a convex curvature with respect to the air stream, in response to periodic air flow velocity oscillation. The fue... An experimental study investigated the characteristics of a stretched cylindrical diffusion flame, with a convex curvature with respect to the air stream, in response to periodic air flow velocity oscillation. The fuel was methane diluted with nitrogen, and the oxidizer air. The oscillation frequency was varied from 5 to 250 Hz. The results are summarized as follows. Though the fluctuation amplitude of the air stream velocity gradient was constant with respect to the frequency, the amplitude of the fuel stream increased. The fluctuation amplitude of the flame radius changed quasi-steadily from 5 to 25 Hz, and decreased with increasing frequency in the frequency range greater than 50 Hz. The flame luminosity did not respond quasi-steadily at 5 Hz, and the oscillation amplitude of flame luminosity was less than that of a steady flame, over the same velocity fluctuation range. The oscillation amplitude of luminosity peaked at 50 Hz, and was greater than that of a steady flame. It is considered that this complex change in flame luminosity with respect to frequency was closely related to the phase difference in the respective time variations in the ratio of flame thickness to radius, the velocity gradients of the air and fuel streams, and the magnitude of these values, with the ratio of flame thickness to radius related to the flame curvature effect, the velocity gradient of the air stream correlated to the flame stretch effect, and the velocity gradient of the fuel stream impacting the fuel transportation. 展开更多
关键词 COMBUSTION diffusion flame velocity oscillation flame stretch flame curvature
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Asymptotic Analysis of Transport Properties and Burning Velocities for Premixed Hydrocarbon Flames
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作者 J.Y.Law H.K.Ma 《Journal of Thermal Science》 SCIE EI CAS CSCD 2001年第2期170-175,共6页
Based on premixed flame, the theoretical model of transport properties with temperature variation was established inside a preheated zone. Lewis number of the deficient-to- stoichiometric hydrocarbon/air mixture has b... Based on premixed flame, the theoretical model of transport properties with temperature variation was established inside a preheated zone. Lewis number of the deficient-to- stoichiometric hydrocarbon/air mixture has been theoretically predicted over a wide range of preheated temperature. These predictions are compared with the experimental data on disport properties that exist in the literature. The response of the burning velocity to flame stretch can be parameterized by the laminar flame speed and Markstein length. Therefore, if the laminar flame speed and Markstein number could be accurately simulated by using an analytic expression of characterized temperature, equivalence ratio, and Lewis number, the results are applicable to the prediction of methane, acetylene, ethylene, ethane, and propane flames. Expanding previous studies on the extinction of premixed flames under the influence of stretch and incomplete reaction, the results were further classified and rescaled. Finally, it could be inferred that parameter Pq, the rescaled extinction Karlovitz number could be used to explain the degree or flame quench. 展开更多
关键词 Lewis number laminar flame speed burning velocity Markstein number Karlovitz number.
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Hysteresis and Multi-state Behavior of Counterflow Flame in a Blowing Cylindrical Burner
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作者 Hsing-Sheng Chai 《Journal of Thermal Science》 SCIE EI CAS CSCD 2009年第3期276-283,共8页
This study focuses on flame hysteresis over a porous cylindrical burner. The hysteresis results from different operation procedure of the experiment. Gradually increasing inflow velocity can transform the envelope fla... This study focuses on flame hysteresis over a porous cylindrical burner. The hysteresis results from different operation procedure of the experiment. Gradually increasing inflow velocity can transform the envelope flame into a wake flame. The blow-off curve can be plotted by determining every critical inflow velocity that makes an envelope flame become a wake flame at different fuel-ejection velocities. In contrast, decreasing the inflow veiocity can transform the wake or lift-off flame into an envelope one. The reattachment curve can be obtained by the same method to explore the blow-off curve, but the intake process is reverse. However, these two curves are not coincident, except the origin. The discrepancy between them is termed as hysteresis, and it results from the difference between the burning velocities associated with both curves. At the lowest fuel-ejection velocity, no hysteresis exists between both curves owing to nearly no burning velocity difference there. Then, raising the fuel-ejection velocity enhances hysteresis and the discrepancy between the two curves. However, as fuel-ejection velocity exceeds a critical value, the intensity of hysteresis almost keeps constant and causes the two curves to be parallel to each other. 展开更多
关键词 HYSTERESIS Blow-off curve Reattachment curve Cylindrical burner Counterflow flame
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Modeling of the turbulent burning velocity for planar and Bunsen flames over a wide range of conditions
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作者 Zhen Lu Yue Yang 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第3期10-25,I0001,共17页
We develop and assess a model of the turbulent burning velocity ST over a wide range of conditions.The aim is to obtain an explicit ST model for turbulent combustion modeling and flame analysis.The model consists of s... We develop and assess a model of the turbulent burning velocity ST over a wide range of conditions.The aim is to obtain an explicit ST model for turbulent combustion modeling and flame analysis.The model consists of sub models of the stretch factor and the turbulent flame area.The stretch factor characterizes the flame response of turbulence stretch and incorporates detailed chemistry and transport effects with a lookup table of laminar counterflow flames.The flame area model captures the area growth based on Lagrangian statistics of propagating surfaces and considers the effects of turbulence length scales and fuel characteristics.The present model predicts sT via an algebraic expression without free parameters.We assess the model using 490 cases of the direct numerical simulation or experiment reported from various research groups on planar and Bunsen flames over a wide range of conditions,covering fuels from hydrogen to n-dodecane,pressures from 1 to 30 atm,lean and rich mixtures,turbulence intensity ratios from 0.1 to 177.6,and turbulence length ratios from 0.5 to 66.7.Despite the scattering sT data in the literature,the comprehensive comparison shows that the proposed ST model has an overall good agreement over the wide range of conditions,with the averaged modeling error of 28.1%. 展开更多
关键词 Turbulent burning velocity Turbulent premixed flame Flame speed
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