Optical and Numerical Analyses of Vortex-Flame Interaction Using Simultaneous and Two-Directional High-Speed Schlieren Photography and Discrete Vortex Method
使用同步和双向高速纹影摄影和离散涡旋方法对涡旋火焰相互作用进行光学和数值分析
基本信息
- 批准号:16560182
- 负责人:
- 金额:$ 2.37万
- 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:2004
- 资助国家:日本
- 起止时间:2004 至 2005
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
The behavior of the propagating flame after the spark ignition in the plane propane-air premixed shear layer is first observed in this paper by combining the following two devised techniques; the acoustic excitation of the plane shear layer and the simultaneous and two-directional schlieren system. To obtain characteristic flame appearances due to the vortex-flame interaction in the plane premixed shear layer, another special idea of assigning two extreme points of ignition is introduced; one at the center of an organized eddy where the vortex motion plays an important role, and the other at the midpoint between two adjacent organized eddies where the rolling-up motion prevails. The two-dimensional change of flame outlines after the midpoint ignition is also simulated by superposing the flame movement with a constant burning velocity followed by thermal expansion on the two-dimensional vortex flow field described by the discrete vortex method. The results obtained are summarized as fol … More lows.(1) It is found that two types of the enhancement mechanisms of flame propagation exist among the organized eddies in the plane shear flow; one is the vortex bursting due to the vortex motion, the other is the vortex boosting due to the rolling-up motion, and exert quantitatively almost the same influences on the flame propagation enhancement process. Also found is that the vortex boosting which is one of the two configurations of vortex-flame interactions can be qualitatively captured by the proposed discrete vortex method.(2) The simulated lateral flame propagation velocities agree relatively well with the axial and lateral flame propagation velocities experimentally obtained from the simultaneous and two-directional high-speed schlieren images, although neglect of the combined effects of the baroclinic torque, the three dimensionality of vortex-flame interaction and the flame curvature leads to slight overestimation of the flame propagation velocity. This result verifies that the proposed two-dimensional discrete vortex method combined with Huygens' Principle is useful for qualitatively estimating and modeling the flame propagation velocity in the plane premixed shear layer, in spite of many assumptions introduced to simplify the numerical simulation.(3) The enhancement effects of flame propagation in the plane premixed shear layer are composed of the physical one due to the vortex-flame interactions and the chemical one through the laminar burning velocity. For both configurations of the vortex-flame interactions, the flame propagation velocity V_f with vortex interaction in the plane premixed shear layer is given by the vortex tangential velocity v_θ plus the propagation speed of the undisturbed flame (ρ_u/ρ_b)S_L, and expressed by the following simple linear equation.V_f=v_θ+(ρ_u/ρ_b)S_L Less
在本文中首先结合以下两种设计的技术,首先观察到平面丙烷 - 空气预混合剪切层的火花点火后传播火焰的行为;平面剪切层以及最简单和两方向的Schlieren系统的声学兴奋。为了获得由于平面预混合剪切层的涡旋形式相互作用而引起的特征火焰外观,引入了另一个特殊的想法,即引入了两个极端的点火点;在有组织的涡流的中心,涡流运动起着重要作用,另一个在两个相邻的有组织的涡流中的中点占据了冠军。在中点点火之后,火焰大纲的二维变化也通过超级燃料运动以恒定的燃烧速度进行模拟,然后在二维涡流流场上由离散涡流方法描述的二维涡流流场进行热膨胀。所获得的结果总结为fol…更多的低点。(1)发现在平面剪切流中有组织的涡流中存在两种类型的火焰传播的增强机制。一个是由于涡旋运动而引起的涡旋爆发,另一个是由于滚动运动引起的涡旋增强,并且对火焰传播增强过程的施加几乎相同的影响。 Also found is that the vortex boosting which is one of the two configurations of vortex-flame interactions can be Normally captured by the proposed discrete vortex method.(2) The simulated lateral flame propagation velocities agree respectively well with the axial and lateral flame propagation velocities experimentally obtained from the simple and two-directional high-speed schlieren images, although neglect of the combined effects of the斜压扭矩,涡旋 - 弗拉姆相互作用的三个维度和火焰曲率导致火焰传播速度略微高估。该结果验证了提出的二维离散涡度方法与Huygens的原理相结合,可用于在飞机上预估算和建模的定性估算和建模火焰的传播速度预处理剪切层中的火焰传播速度,尽管引入了许多假设,尽管它简化了数值模拟,但在造成了数值的效果。通过层流燃烧速度,涡旋形式相互作用和化学效果。对于Vortex-Flame交互的两种配置,在平面预混合剪切层中具有Vortex相互作用的火焰传播速度V_F由Vortex切向速度V_θ加上,加上不受干扰的火焰的传播速度(ρ_U/ρ_B)S_L,并表达等式v_f =v_θ+(ρ_U/ρ_b)s_l少
项目成果
期刊论文数量(15)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
平面せん断流中の渦と火炎の相互干渉過程の離散渦解析と光学観察
平面剪切流中涡流与火焰相互作用过程的离散涡流分析及光学观测
- DOI:
- 发表时间:2004
- 期刊:
- 影响因子:0
- 作者:大岩 紀生;石野 洋二郎
- 通讯作者:石野 洋二郎
Optical Observation and Discrete Vortex Analysis of Vortex-Flame Interaction in a Plane Premixed Shear Flow
平面预混剪切流中涡-火焰相互作用的光学观察和离散涡分析
- DOI:
- 发表时间:2005
- 期刊:
- 影响因子:0
- 作者:Norio OHIWA;Yojiro ISHINO
- 通讯作者:Yojiro ISHINO
optical Analysis and Qualitative Discrimination of Vortex-Flame Interaction in a Plane Premixed Shear Layer
平面预混剪切层中涡旋火焰相互作用的光学分析与定性判别
- DOI:
- 发表时间:2006
- 期刊:
- 影响因子:0
- 作者:Norio OHIWA;Yojiro ISHINO
- 通讯作者:Yojiro ISHINO
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OHIWA Norio其他文献
OHIWA Norio的其他文献
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{{ truncateString('OHIWA Norio', 18)}}的其他基金
Detailed Image Analysis of Vortex-Flame Interaction under Acoustic Excitation of Coherent Structure Characterized by Geometrical Configuration
几何构型相干结构声激励下涡旋-火焰相互作用的详细图像分析
- 批准号:
18560197 - 财政年份:2006
- 资助金额:
$ 2.37万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
An Experimental Approach to Vortex-Flame Interaction in Practical Turbulent Fields
实际湍流场中涡旋火焰相互作用的实验方法
- 批准号:
12650201 - 财政年份:2000
- 资助金额:
$ 2.37万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
Active Control and Noise Reduction of Turbulent Diffusion Flames with Coherent Structure by Acoustic Excitation
相干结构湍流扩散火焰的声激励主动控制与降噪
- 批准号:
08650255 - 财政年份:1996
- 资助金额:
$ 2.37万 - 项目类别:
Grant-in-Aid for Scientific Research (C)
Acoustic Excitation of Organized Eddy Structure and Dual diffusion Flames Behind a Rear-Facing Simicircular Cylinder
后向圆柱体后面有组织的涡流结构和双扩散火焰的声激发
- 批准号:
06650243 - 财政年份:1994
- 资助金额:
$ 2.37万 - 项目类别:
Grant-in-Aid for General Scientific Research (C)
Research and Development of a Turbo-Charger-Aided, Forced-Ventilated Valveless Pulse Combustor
涡轮增压辅助强制通风无阀脉冲燃烧器的研制
- 批准号:
01550173 - 财政年份:1989
- 资助金额:
$ 2.37万 - 项目类别:
Grant-in-Aid for General Scientific Research (C)