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Large eddy simulation of a planar jet flow with nanoparticle coagulation 被引量:25
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作者 Mingzhou Yu Jianzhong Lin +1 位作者 Lihua Chen Tatleung Chan 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2006年第4期293-300,共8页
Coagulation and growth of nanoparticles subject to large coherent structures in a planar jet has been explored by using large eddy simulation. The particle field is obtained by employing a moment method to approximate... Coagulation and growth of nanoparticles subject to large coherent structures in a planar jet has been explored by using large eddy simulation. The particle field is obtained by employing a moment method to approximate the nanoparticle general dynamic equa- tion. An incompressible fluid containing particles of 1 nm in diameter is projected into a particle-free ambient. The results show that the coherent structures dominate the evolution of the nanoparticle number intensity, diameter and polydispersity distributions as the jet develops. In addition, the coherent structures act to increase the diffusion of particles, and the vortex rolling-up makes the particles distributing more irregularly while the vortex pairing causes particle distributions to become uniform. As the jet travels downstream, the time-averaged particle number concentration becomes lower in the jet core and higher in the outskirts, whereas the time- averaged particle mass over the entire flow field maintains unaltered, and the time-averaged particle diameter and geometric standard deviations grow and reach their maximum on the interface of the jet region and the ambient. 展开更多
关键词 NANOPARTICLES COAGULATION planar jet Large eddy simulation Coherent structure
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Nanoparticle coagulation in a planar jet via moment method 被引量:2
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作者 于明州 林建忠 陈丽华 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2007年第11期1445-1453,共9页
Large eddy simulations of nanoparticle coagulation in an incompressible planar jet were performed. The particle is described using a moment method to approximate the particle general dynarnics equations. The time-aver... Large eddy simulations of nanoparticle coagulation in an incompressible planar jet were performed. The particle is described using a moment method to approximate the particle general dynarnics equations. The time-averaged results based on 3000 time steps for every case were obtained to explore the influence of the Schmidt number and the Damkohler number on the nanoparticle dynamics. The results show that the changes of Schmidt number have the influence on the number concentration of nanoparticles only when the particle diameter is less than 1 nm for the fixed gas parameters. The number concentration of particles for small particles decreases more rapidly along the flow direction, and the nanoparticles with larger Schmidt number have a narrower distribution along the transverse direction. The smaller nanoparticles Coagulate and disperse easily, grow rapidly hence show a stronger polydispersity. The smaller coagulation time scale can enhance the particle collision and coagulation. Frequented collision and coagulation bring a great increase in particle size. The larger the Damkohler number is, the higher the particle polydispersity is. 展开更多
关键词 NANOPARTICLES COAGULATION planar jet moment method large eddy simulation
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Large Eddy Simulation of the Particle Coagulation in High Concentration Particle-Laden Planar Jet Flow
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作者 LIN Peifeng WU Dichong +3 位作者 YU Mingzhou WANG Chao ZHANG Lite ZHU Zefei 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2011年第6期947-956,共10页
Particle coagulation by Brownian motion is an important but difficult research topic.When particle volume concentration is larger than 0.1%,the classic SMOLUCHOWSKI equation is not applicative anymore.The high concent... Particle coagulation by Brownian motion is an important but difficult research topic.When particle volume concentration is larger than 0.1%,the classic SMOLUCHOWSKI equation is not applicative anymore.The high concentration coagulation,with HEINE's correction,source terms for the Taylor-series expansion method of moments(TEMOM) are firstly driven in this paper.Ultra-fine particle(d0?100 mm) with initial volume fraction f?1% coagulation in a planar jet turbulence flow is simulated via the large eddy simulation(LES).The instantaneous and time-averaged particle distributions and the high concentration enhancement are given out.The particle number concentration distribution results show that the coagulation is more intense comparing to dilute case in previous research,especially near the nozzle exit.After jet flow is fully developed,the effect is much more obvious at the region between vortexes.The time-averaged γ(the high concentration enhance factor) distributes sharply and symmetrically about the jet centerline at the upstream,but becomes broad and flat at downstream where the cross-stream averaged γ fluctuates drastically.As a new attempt,this paper shows Brownian coagulation with high concentration also can be calculated via TEMOM appropriately,and the coagulation at the region between vortexes is about 1.38 times intensive of the dilute result calculated by the classic Smoluchowski theory. 展开更多
关键词 COAGULATION LES planar jet flow High concentration enhancement
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NUMERICAL SIMULATION OF FLOW PATTERNS IN PLANAR JETS 被引量:1
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作者 K. S. Lau 1) Yi Liu 1,2) Yin Cheng Guo 2) C. K. Chan 3) Wen Yi Lin 2) 1) Department of Applied Physics, The Polytechnic University, Hong Kong, China 2) Department of Engineering Mechanics, Tsinghua University, Be 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2001年第z1期77-81,共5页
Two dimensional spatial developing turbulent planar jets with different velocity ratios of jet fluid to co flow fluid at the inlet section are simulated with large eddy simulation give detailed information of transien... Two dimensional spatial developing turbulent planar jets with different velocity ratios of jet fluid to co flow fluid at the inlet section are simulated with large eddy simulation give detailed information of transient behaviors of coherent structures in turbulent jets and depict how the velocity ratios will affect the evolution of coherent structures. The motion of small scale structures is described by the standard Smagorinsky SGS model. Transport equation of passive scalar is also solved in order to perform numerical visualization of flow field. Transient distributions of velocity are obtained at different evolution periods of turbulent jets. Evolutions of coherent structures in flow field are also given in this paper as well as the comparison of flow patterns among three different velocity ratios. 展开更多
关键词 LARGE EDDY simulation planar jet COHERENT structure
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Nanoparticle Transportation and Brownian Diffusion in Planar Jet Flow via Large Eddy Simulation 被引量:1
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作者 Peifeng Lin Dichong Wu Zefei Zhu 《Open Journal of Fluid Dynamics》 2012年第4期354-358,共5页
The nanoparticle transportation and Brownian diffusion in planar jet flow is simulated via large eddy simulation in this work. To thorough compare the Brownian diffusion with different particle size, we computed three... The nanoparticle transportation and Brownian diffusion in planar jet flow is simulated via large eddy simulation in this work. To thorough compare the Brownian diffusion with different particle size, we computed three particle diameter dp = 1 nm, 10 nm and 50 nm in one simulation process simultaneously. The numerical results showed that at the flow de- veloping stage, the particle mass concentration pattern develops as the flow vorticity develops. The distribution is nearly uniform at the lower reaches of the nozzle exit. When the jet flow is developing on, vortexes always carry the particle from upstream to downstream, from the central axis region to the outer mixing layer of jet. At the front of the jet flow, particles distribute more homogeneous for they have more residence time to diffuse from higher concentration region to the lower concentration region. The time averaged particle concentration distribution patterns are similar to Gaussian distribution form. The maximum concentration contributed by diffusion is present at the mixing layer near the nozzle exit. The farther away from the nozzle exit in the cross-stream direction, the smaller the concentration is. The maximum concentration contributed by diffusion is several orders smaller than that contributed by flow convection. 展开更多
关键词 Large EDDY Simulation planar jet Flow NANOPARTICLE Evolution DIFFUSION
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PARTICLE SIZE DISTRIBUTION IN A PLANAR JET FLOW UNDER-GOING SHEAR-INDUCED COAGULATION AND BREAKAGE 被引量:5
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作者 GAN Fu-jun LIN Jian-zhong YU Ming-zhou 《Journal of Hydrodynamics》 SCIE EI CSCD 2010年第4期445-455,共11页
A CFD simulation is performed for a particle-laden planar jet flow.The Reynolds number is 8300,and the initial particle diameter is 1 μm.Large Eddy Simulation(LES) is employed to calculate the flow field,and the Ta... A CFD simulation is performed for a particle-laden planar jet flow.The Reynolds number is 8300,and the initial particle diameter is 1 μm.Large Eddy Simulation(LES) is employed to calculate the flow field,and the Taylor-series expansion moment method(TEMOM) is adopted to deal with the balance equation of particle coagulation and breakage.The shear-induced coagulation kernel,power-law breakage kernel and symmetric fragment distribution function are involved.The prediction of the distribution of the mean streamwise velocity of the jet is in good agreement with experimental data.The evolution of particle number concentration,volume concentration,polydispersity,particle diameter and standard geometric deviation is discussed in detail.The results show that as the jet travels downstream,the particle number concentration and volume concentration decrease,while their spans become wider.The polydispersity and particle diameter are very large in the shear layers at the upstream and in the core of vortex structures at the downstream.The particle standard geometric deviation changes within the range of 1.32 ≤σg≤ 1.96,and increases sharply in the shear layers.All variables approach the steady-state as time progresses. 展开更多
关键词 Taylor-series expansion moment method shear-induced coagulation BREAKAGE planar jet
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Dynamics and geometry of developing planar jets based on the invariants of the velocity gradient tensor
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作者 吴楠楠 SAKAI Yasuhiko +1 位作者 NAGATA Kouji ITO Yasumasa 《Journal of Hydrodynamics》 SCIE EI CSCD 2015年第6期894-906,共13页
Based on the direct numerical simulation (DNS), the developing planar jets under different initial conditions, e.g., the con- ditions of the exit Reynolds number and the exit mean velocity profile, are investigated.... Based on the direct numerical simulation (DNS), the developing planar jets under different initial conditions, e.g., the con- ditions of the exit Reynolds number and the exit mean velocity profile, are investigated. We mainly focus on the characteristics of the invariants of the velocity gradient tensor, which provides insights into the evolution of the dynamics and the geometry of the planar jets along with the flow transition. The results show that the initial flow near the jet exit is strongly predominated by the dissipation over the enstrophy, the flow transition is accompanied by a severe rotation and straining of the flow elements, where the vortex structure evolves faster than the fluid element deformation, in the fully-developed state, the irrotational dissipation is dominant and the most probable geometry of the fluid elements should remain between the biaxial stretching and the axisymmetric stretching. In addition, with a small exit Re and a parabolic profile for the exit mean streamwise velocity, the decay of the mean flow field and the magnitude of the turbulent variables will be strengthened in the process of the flow transition, however, a large exit Re will promote the flow transition to the fully-developed state. The cross-impact between the exit Re and the exit mean velocity profile is also observed in the present study. 展开更多
关键词 planar jet direct numerical simulation (DNS) velocity gradient tensor flow transition joint probability density function(joint pdf)
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Supersonic boundary layer transition induced by self-sustaining dual jets 被引量:1
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作者 刘强 罗振兵 +3 位作者 邓雄 刘志勇 王林 周岩 《Chinese Physics B》 SCIE EI CAS CSCD 2020年第1期95-98,共4页
To promote high-speed boundary layer transition,this paper proposes an active self-sustaining dual jets(SDJ)actuator utilizing the energy of supersonic mainflow.Employing the nanoparticle-based planar laser scattering... To promote high-speed boundary layer transition,this paper proposes an active self-sustaining dual jets(SDJ)actuator utilizing the energy of supersonic mainflow.Employing the nanoparticle-based planar laser scattering(NPLS),supersonic flat-plate boundary layer transition induced by SDJ is experimentally investigated in an Ma-2.95 low-turbulence wind tunnel.Streamwise and spanwise NPLS images are obtained to analyze fine flow structures of the whole transition process.The results reveal the transition control mechanisms that on the one hand,the jet-induced shear layer produces unstable Kelvin–Helmholtz instabilities in the wake flow,on the other hand,the jets also generates an adverse pressure gradient in the boundary layer and induce unstable streak structures,which gradually break down into turbulence downstream.The paper provides a new method for transition control of high-speed boundary layer,and have prospect both in theory and engineering application. 展开更多
关键词 supersonic boundary layer transition self-sustaining dual jets nanoparticle-based planar laser scattering(NPLS) vortex structures
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甲烷平面射流扩散火焰的大涡模拟 被引量:9
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作者 刘奕 郭印诚 +2 位作者 张会强 王希麟 林文漪 《工程热物理学报》 EI CAS CSCD 北大核心 2003年第2期343-346,共4页
本文对甲烷-空气平面自由射流扩散火焰进行了大涡模拟,采用分步投影法求解动量方程,湍流亚格子项采用动态模式模拟,化学反应速率亚格子项采用动态相似模式模拟,压力泊松方程采用修正的循环消去法快速求解,空间方向采用二阶精度的差分格... 本文对甲烷-空气平面自由射流扩散火焰进行了大涡模拟,采用分步投影法求解动量方程,湍流亚格子项采用动态模式模拟,化学反应速率亚格子项采用动态相似模式模拟,压力泊松方程采用修正的循环消去法快速求解,空间方向采用二阶精度的差分格式,在时间方向上采用二阶精度的显式差分格式。模拟结果给出了湍流扩散火焰的瞬态发展变化过程,表明射流扩散火焰的发展过程存在着“湍流控制”和“化学反应控制”两个不同阶段。 “湍流控制”阶段仅存在于火焰发展初期的极短时间内。 展开更多
关键词 大涡模拟 平面射流 扩散火焰 拟序结构 湍流燃烧
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平面射流中纳米粒子积聚的矩方法 被引量:12
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作者 于明州 林建忠 陈丽华 《应用数学和力学》 CSCD 北大核心 2007年第11期1287-1295,共9页
应用大涡模拟方法求解平面湍射流场,矩方法求解纳米粒子的一般动力学方程.通过对每种情况3000个时间步的平均,得到了Schmidt数和Damkohler数对纳米粒子动力学特性的影响.结果发现,当气体参数不变时,Schmidt数的变化只对直径小于1 nm的... 应用大涡模拟方法求解平面湍射流场,矩方法求解纳米粒子的一般动力学方程.通过对每种情况3000个时间步的平均,得到了Schmidt数和Damkohler数对纳米粒子动力学特性的影响.结果发现,当气体参数不变时,Schmidt数的变化只对直径小于1 nm的颗粒数密度的分布产生影响.直径小的颗粒其颗粒数密度沿流动方向下降迅速,而具有大Schmidt数的颗粒,沿横向的分布较窄.较小的颗粒容易发生积聚和扩散,并且体积增长较快,因而颗粒多分散性较为明显.小的颗粒积聚时间尺度能增强颗粒的碰撞和积聚频率,导致颗粒尺寸迅速增大.Damkohler数越大,颗粒的多分散也越明显. 展开更多
关键词 纳米粒子 积聚 平面射流 矩方法 大涡模拟
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入流滑移条件对两相射流特性影响的大涡模拟研究 被引量:2
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作者 范全林 张会强 +2 位作者 郭印诚 王希麟 林文漪 《燃烧科学与技术》 EI CAS CSCD 2001年第1期99-103,共5页
研究了入流滑移条件对空间发展的气粒两相平面湍射流的非定常流动特性的影响。以 Re数 130 0 0的平面不可压缩湍射流流动为例 ,气相场用 Euler方法求解 ,通过大涡模拟 ( large- eddy simulation,L ES) ,直接求解大尺度涡运动的 Navier- ... 研究了入流滑移条件对空间发展的气粒两相平面湍射流的非定常流动特性的影响。以 Re数 130 0 0的平面不可压缩湍射流流动为例 ,气相场用 Euler方法求解 ,通过大涡模拟 ( large- eddy simulation,L ES) ,直接求解大尺度涡运动的 Navier- Stokes方程 ,小尺度涡用标准 Smagorinsky亚格子模式模拟。颗粒相的运动用 L agrangian方法直接求解。在不同入流滑移条件下 ( Up0 / U0 =α) :α=1,两相无滑移 ;α=0 .5 ,中等滑移情况 ;α=0 ,颗粒相以静止状态进入射流 ,分别求解了 5种尺度 ,共 2 5× 10 4个颗粒的运动方程。结果表明 :对于 Stokes数远小于 1或量级在 O( 1)附近的颗粒 ,颗粒与气相拟序结构的相互作用行为对入流滑移条件的变化不敏感。但是 Stokes数显著大于 1的颗粒 。 展开更多
关键词 滑移条件 大涡模拟 平面射流 拟序结构 数值模拟 两相射流 燃烧
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燃料型NO生成的实验研究 被引量:2
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作者 郭治民 张会强 +2 位作者 王希麟 郭印诚 林文漪 《工程热物理学报》 EI CAS CSCD 北大核心 2003年第5期881-884,共4页
在二维平面射流中进行了燃料型NO的实验研究,采用在甲烷中加入NH_3的方法来模拟燃料氮。实验结果表明:实验过程中生成的NO主要是燃料型NO,热力型NO和快速型NO占排放的总NO的比例很小,同时随着NH_3的增加,NO迅速增加,并且NO浓度沿轴向呈... 在二维平面射流中进行了燃料型NO的实验研究,采用在甲烷中加入NH_3的方法来模拟燃料氮。实验结果表明:实验过程中生成的NO主要是燃料型NO,热力型NO和快速型NO占排放的总NO的比例很小,同时随着NH_3的增加,NO迅速增加,并且NO浓度沿轴向呈双峰分布。 展开更多
关键词 燃料型NO 平面射流 双峰分布
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自由表面二维平面射流冲击传热的理论分析 被引量:5
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作者 马重芳 陈永昌 《北京工业大学学报》 CAS CSCD 2000年第3期59-62,共4页
对二维平面射流冲击平板时的层流流动(和传热)给出了速度和温度边界层的综合解析,用积分方法得到了平面射流冲击传热的驻点区和部分壁面射流区的换热关系式,并将等热流壁面的分析结果与实验数据进行比较,结果基本吻合,
关键词 射流冲击传热 边界层 自由表面 二维平面射流
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颗粒加入方式对平面射流中颗粒弥散影响的离散涡模拟 被引量:1
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作者 李伟锋 代正华 +4 位作者 刘海峰 龚欣 于广锁 王辅臣 于遵宏 《燃烧科学与技术》 EI CAS CSCD 北大核心 2005年第4期355-360,共6页
用离散涡方法对平面射流进行数值模拟,得到了与实验定量符合的速度场,采用单向耦合的Lagrangian方法模拟了流场中颗粒的弥散.颗粒进入流场的初始径向位置由满足不同概率分布的随机数决定.结果表明:对St 1的颗粒,初始径向位置的概率分布... 用离散涡方法对平面射流进行数值模拟,得到了与实验定量符合的速度场,采用单向耦合的Lagrangian方法模拟了流场中颗粒的弥散.颗粒进入流场的初始径向位置由满足不同概率分布的随机数决定.结果表明:对St 1的颗粒,初始径向位置的概率分布对其弥散的影响不显著;对St^o(1)和St 1的颗粒,弥散显著受到初始径向位置概率分布的影响,其弥散函数在上抛物线形概率分布时最大,均匀分布时次之,截尾高斯分布时最小. 展开更多
关键词 气-固两相平面射流 拟序结构 离散涡方法 概率分布 弥散函数
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有限空间内平面相交射流的数值模拟 被引量:3
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作者 章旋 徐通模 +1 位作者 郭宏生 惠世恩 《热能动力工程》 CAS CSCD 北大核心 1994年第6期313-316,379,共5页
本文利用SIMPLE算法对有限空间内平面相交射流的等温流场进行了数值模拟。差分格式为乘方格式,文中计算和分析了相交射流的夹角、间距和截面突扩比对流场和射流汇合的影响。计算结果在定性上是合理的。
关键词 平面相交射流 等温流 流场模拟 数学模型
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气固两相自由射流颗粒弥散实验研究综述 被引量:1
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作者 邢春礼 费颖 +2 位作者 韩俊 吴少华 秦裕琨 《节能技术》 CAS 2009年第5期437-440,共4页
本文为水平浓淡煤粉燃烧技术研发基础工作之一。以双矩形气固两相平行射流为研究背景,作者考察了气固两相平面和圆自由射流的实验研究。综述表明,大涡拟序结构的存在和初始条件对自由射流颗粒弥散的影响是关键的,利用St数可定性估计这... 本文为水平浓淡煤粉燃烧技术研发基础工作之一。以双矩形气固两相平行射流为研究背景,作者考察了气固两相平面和圆自由射流的实验研究。综述表明,大涡拟序结构的存在和初始条件对自由射流颗粒弥散的影响是关键的,利用St数可定性估计这种影响,颗粒尺寸和负荷对气固两相流场的湍流结构具有显著影响,大颗粒尾涡脱落显著地影响湍流结构的事实使数值模拟气固两相流动的努力面临着模拟方法选择与指导工程设计的矛盾要求。因此,数值模拟技术需要评估,这是继续的工作。 展开更多
关键词 平面射流 颗粒弥散 湍流结构 拟序结构 数值模拟
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超声速气流中液体横向射流的破碎特性 被引量:8
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作者 李锋 吕付国 +3 位作者 罗卫东 赵凯 王昌胜 熊溢威 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2015年第12期2356-2362,共7页
为了研究超燃冲压发动机燃烧室内液体燃料雾化掺混特性,确定影响雾化的关键因素以实现高效燃烧,在超燃冷态雾化实验平台,以纹影法为主,同时辅助以平面激光诱导荧光(PLIF)技术和基于向前散射原理的颗粒直径测量技术,分别对横向射流航... 为了研究超燃冲压发动机燃烧室内液体燃料雾化掺混特性,确定影响雾化的关键因素以实现高效燃烧,在超燃冷态雾化实验平台,以纹影法为主,同时辅助以平面激光诱导荧光(PLIF)技术和基于向前散射原理的颗粒直径测量技术,分别对横向射流航空煤油RP-3和水在超声速气流中的流场波系结构、射流穿透深度和诱导弓形激波强度等进行了实验研究,并对射流雾化掺混特性进行了数理分析.结果表明:定义的无量纲参数能够定性分析两种液体横向射流在超音速流场中的变化规律,并得到与实验结果一致的结论;在动压比1.0-3.3范围内,射流穿透深度和诱导弓形激波强度随着动压比和射流速度的增加而增加;表面张力和黏度对超声速射流掺混有重要影响. 展开更多
关键词 超燃冲压发动机 横向射流 纹影法 平面激光诱导荧光(PLIF) 雾化
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平面撞击流振荡特性 被引量:14
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作者 孙志刚 李伟锋 +1 位作者 刘海峰 于遵宏 《化工学报》 EI CAS CSCD 北大核心 2009年第2期338-344,共7页
The oscillation characteristics of two planar opposed jets were studied by using high-speed camera,smoke wire visualization and hot-wire anemometry(HWA).The oscillation periods of two planar opposed jets at different ... The oscillation characteristics of two planar opposed jets were studied by using high-speed camera,smoke wire visualization and hot-wire anemometry(HWA).The oscillation periods of two planar opposed jets at different nozzle separations and exit nozzle velocities were studied.The results showed two models of instabilities:streamwise quasi-periodic oscillation model and deflection oscillation model.The oscillation model was mainly streamwise quasi-periodic oscillation model at L<5H(where L was the nozzle separation and H was the nozzle slot height),and it was mainly deflection oscillation model at L>5H.The deflection oscillation model had a stable period which decreased with increasing normalized nozzle separation. 展开更多
关键词 平面喷嘴 振荡特性 撞击流 烟线法 流场显示
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双平行平面射流输运特性研究 被引量:1
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作者 陈力哲 宋稚娟 邢春礼 《节能技术》 CAS 2009年第5期421-422,478,共3页
平行射流输运特性研究具有较重要的理论意义和工程价值,对水平浓淡煤粉燃烧也有较重要的意义。本文实验研究了双平行平面射流动量、能量和质量输运,结果表明:速度分布表现为双射流相互吸引并最终汇合成单一射流;温度分布反映了冷射流为... 平行射流输运特性研究具有较重要的理论意义和工程价值,对水平浓淡煤粉燃烧也有较重要的意义。本文实验研究了双平行平面射流动量、能量和质量输运,结果表明:速度分布表现为双射流相互吸引并最终汇合成单一射流;温度分布反映了冷射流为加热射流所卷吸;浓度分布反映了惯性力的占优作用。三种变量分布反映了动量、能量和质量输运性质的根本性区别。 展开更多
关键词 平面射流 输运特性 平行射流
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流动环境中热水负浮力射流的近区特性分析 被引量:3
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作者 杨中华 槐文信 《华中科技大学学报(自然科学版)》 EI CAS CSCD 北大核心 2006年第2期58-60,共3页
在对流动环境中平面热水负浮力射流进行数值模拟的基础上就近区特性进行分析,得到了不同排放角度和射流比下涡心和分离点位置等特征量的值.分析了水面上流速、温度、湍动能及其耗散率变化规律,对涡心断面上的动量方程和湍动能平衡进行... 在对流动环境中平面热水负浮力射流进行数值模拟的基础上就近区特性进行分析,得到了不同排放角度和射流比下涡心和分离点位置等特征量的值.分析了水面上流速、温度、湍动能及其耗散率变化规律,对涡心断面上的动量方程和湍动能平衡进行了研究.计算结果分析发现回流区内湍动能最大值存在滞后的现象,浮力作用对时均量的影响较大,而对紊动量的影响则比较小. 展开更多
关键词 平面负浮力射流 热水排放 数值模拟 动量平衡 湍动能平衡
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