Unsteady Interaction Between Laminar Propagating Flame and Array of Small Fuel Droplets
层流传播火焰与小燃料液滴阵列之间的不稳定相互作用
基本信息
- 批准号:11650233
- 负责人:
- 金额:$ 1.41万
- 依托单位:
- 依托单位国家:日本
- 项目类别:Grant-in-Aid for Scientific Research (C)
- 财政年份:1999
- 资助国家:日本
- 起止时间:1999 至 2000
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
An experimental study has been made of the ignition process of fuel droplet array or single fuel droplets subjected to a laminar flat flame propagating through a lean homogeneous propane/air mixture at constant pressure. Binary fuels consisting n-hexane and n-hexadecane or n-dodecane, and benzene and n-hexadecane were tested. Water-emulsified liquids consisting n-dodecane, and pure fuels like n-hexane, n-octane, n-dodecane and n-hexadecane were used as well. A combustion chamber made of a transparent duct was installed with spark electrodes, fine quartz fibers to suspend fuel droplets, and a shutter to allow the burned gas to escape at the top end. A high-speed video camera was provided for photographic observation of each droplet ignited by the propagating flame.Ignition delay of pure-fuel droplets increased monotonically with increase of the initial droplet diameter and decrease of fuel volatility. The influence of the initial droplet diameter on ignition delay decreased with increas … More ing fuel volatility. Ignition delay of the binary-fuel droplets decreased with increase of the volume concentration of the higher-volatility fuel. Ignition delay of the binary fuels showed a minimum and a maximum as a function of the initial droplet diameter. The diameters at the minimum and the maximum of ignition delay decreased with increasing higher-volatility fuel concentration. Ignition delay or emulsified-fuel droplets monotonically with the initial droplet diameter as expected. The increase in the volume concentration of the higher-volatility component caused an inverse result in comparison with that for the binary mixtures of fuels, since the higher-volatility component was water in this case. Part of the propagating flame behind the droplet became convex towards the unburned gas as it passed a droplet or higher-volatility fuels, while the flame remained flat for the lower-volatility fuels. The deformation length of the propagating flame behind the droplet increased with increasing higher-volatility fuel concentration. Less
对燃料液滴阵列或单个燃料液滴的点火过程进行了实验研究,该火焰在恒定压力下通过贫均质丙烷/空气混合物传播,由正己烷和正十六烷或正己烷组成。 - 测试了十二烷、苯和正十六烷,由正十二烷组成的水乳化液体,以及正己烷等纯燃料。还使用了正辛烷、正十二烷和正十六烷。由透明管道制成的燃烧室安装有火花电极、悬浮燃料液滴的细石英纤维和允许燃烧后的气体逸出的百叶窗。顶端设置有高速摄像机,用于对传播火焰点燃的每个液滴进行摄影观察。纯燃料液滴的点火延迟随着初始液滴直径的增加和直径的减小而单调增加。初始液滴直径对点火延迟的影响随着二元燃料挥发性的增加而减小。二元燃料液滴的点火延迟随着高挥发性燃料的体积浓度的增加而减小。显示了作为初始液滴直径的函数的最小值和最大值,点火延迟的最小和最大直径随着较高挥发性燃料浓度的增加而减小。正如预期的那样,与初始液滴直径单调地变化,与燃料的二元混合物相比,高挥发性组分的体积浓度的增加导致了相反的结果,因为在这种情况下,高挥发性组分是水的一部分。当液滴经过液滴或挥发性较高的燃料时,液滴后面的传播火焰会向未燃烧的气体凸出,而对于挥发性较低的燃料,火焰保持平坦。液滴后面传播的火焰随着高挥发性燃料浓度的增加而增加。
项目成果
期刊论文数量(6)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
Daisuke SEGAWA: "Ignition of Binary Mixture Droplets by a Propagating Laminar Flame"Proceedings of the Combustion Institute. Vol.28. 961-968 (2000)
Daisuke SEGAWA:“传播层流火焰点燃二元混合物液滴”燃烧研究所论文集。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
角田敏一: "層流伝ぱ火炎による二成分燃料液滴の着火"日本機械学会論文集(B編). 66・647. 1879-1884 (2000)
Toshikazu Tsunoda:“层流传播火焰点燃二元燃料滴”,日本机械工程师学会会刊(编辑 B)1879-1884(2000 年)。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Toshikazu KADOTA: "Ignition of a Binary Fuel Droplet by a Propagating Laminar Flame"Transaction of the Japan Society of Mechanical Engineers. Vol.66(B). 1879-1884 (2000)
Toshikazu KADOTA:“传播层流火焰点燃二元燃料液滴”,日本机械工程师学会汇刊。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
- 作者:
- 通讯作者:
Daisuke SEGAWA: "Ignition of Binary Mixture Droplets by a Propagating Laminar Flame"Proceedings of the Combustion Institute. 28. 961-968 (2000)
Daisuke SEGAWA:“传播层流火焰点燃二元混合物液滴”燃烧研究所论文集。
- DOI:
- 发表时间:
- 期刊:
- 影响因子:0
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- 通讯作者:
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KADOTA Toshikazu其他文献
KADOTA Toshikazu的其他文献
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{{ truncateString('KADOTA Toshikazu', 18)}}的其他基金
Comparative Research on the Quality Assurance of Engineering Education and the Degree Programs of the Graduate School of University in Japan, Europe and America
日本、欧美大学研究生院工程教育质量保障与学位课程比较研究
- 批准号:
23501049 - 财政年份:2011
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
The Dynamism of Combustion and Flame of Three-Dimensionally Dispersed Fuel System under Microgravity Conditions
微重力条件下三维分散燃料系统的燃烧与火焰动力学
- 批准号:
16360108 - 财政年份:2004
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (B)
Instrumentation Development of Compact Laser Diagnostic Systems for the Combustion Experiments under Microgravity
微重力燃烧实验紧凑型激光诊断系统的仪器开发
- 批准号:
08555241 - 财政年份:1996
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (A)
Study on the Combustion and Microexplosion of an Emulsified Fuel Droplet in High Pressure Gaseous Environments
高压气体环境中乳化燃料液滴的燃烧与微爆炸研究
- 批准号:
07650264 - 财政年份:1995
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
Combustion and Evaporation of Liquid Fuel under the Supercritical Condition at Normal Gravity and Micro Gravity
常重力和微重力超临界条件下液体燃料的燃烧与蒸发
- 批准号:
03650191 - 财政年份:1991
- 资助金额:
$ 1.41万 - 项目类别:
Grant-in-Aid for General Scientific Research (C)
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CAREER: Characterization of Propagating and Receding Flame Edges in Composition and Velocity Gradients
职业:成分和速度梯度中传播和后退火焰边缘的表征
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