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正交射流燃烧器气固两相流动的数值计算 被引量:1
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作者 徐明厚 韩才元 《华中理工大学学报》 CSCD 北大核心 1994年第3期69-73,共5页
运用气相k-ε模型和颗粒相代数方程模型对正交射流煤粉燃烧器气固两相流场进行了数值模拟,获得了该燃烧器内的气、固两相速度分布,颗粒质量流分布,并与实验值进行了对比,两者定性符合,同时,探讨了颗粒直径对颗粒混合的影响,得... 运用气相k-ε模型和颗粒相代数方程模型对正交射流煤粉燃烧器气固两相流场进行了数值模拟,获得了该燃烧器内的气、固两相速度分布,颗粒质量流分布,并与实验值进行了对比,两者定性符合,同时,探讨了颗粒直径对颗粒混合的影响,得到了一些很有价值的结论。 展开更多
关键词 正交射流 煤粉燃烧器 气固两相流动
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The Structure of A Turbulent Jet in A Crossflow-Effect of Jet-Crossflow Velocity 被引量:6
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作者 李行伟 匡翠萍 陈国谦 《China Ocean Engineering》 SCIE EI 2002年第1期1-20,共20页
A comprehensive numerical study on the three-dimensional structure of a turbulent jet in crossflow is performed. The jet-to-crossflow velocity ratio (R) varies in the range of 2 - 16; both vertical jets and inclined j... A comprehensive numerical study on the three-dimensional structure of a turbulent jet in crossflow is performed. The jet-to-crossflow velocity ratio (R) varies in the range of 2 - 16; both vertical jets and inclined jets without excess streamwise momentum are considered. The numerical results of the Standard two-equation k-ε model show that the turbulent structure can be broadly categorised according to the jet-to-crossflow velocity ratio. For strong to moderate jet discharges, i.e. R> 4, the jet is characterized by a longitudinal transition through a bent-over phase during which the jet becomes almost parallel with the main freestream, to a sectional vortex-pair flow with double concentration maxima; the computed flow details and scalar mixing characteristics can be described by self-similar relations beyond a dimensionless distance of around 20-60. The similarity coefficients are only weakly dependent on R. The cross-section scalar field is kidney-shaped and bifurcated, vvith distinct double concentration maxima; the aspect ratio is found to be around 1.2. A loss in vertical momentum is ob-served and the added mass coefficient of the jet motion is found to be approximately 1. On the other hand, for weak jets in strong crossflow, i. e. R ≥ 2, the lee of the jet is characterized by a negative pressure region. Although the double vortex flow can stili be noted, the scalar field becomes more symmetrical and no longer bifurcated. The similarity coeffcients are al-so noticeably different. The predicted jet flovv characteristics and mixing rates are well supported by experimental and field dala 展开更多
关键词 turbulent jet crossflow advected line puff mixing concentration dilution double-vortex momentim added mass SELF-SIMILARITY turbulence modeling bifurcation environmental fluid mechanics
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AN INVESTIGATION OF TURBULENT RECTANGULAR JET DISCHARGED INTO A NARROW CHANNEL WEAK CROSSFLOW 被引量:5
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作者 PATHAK Manabendra DASS Anoop K. DEWAN Anupam 《Journal of Hydrodynamics》 SCIE EI CSCD 2008年第2期154-163,共10页
A computational investigation of the mean flow field of turbulent rectangular jets issuing into a narrow channel crossflow is presented. The length of the jet slot spans more than 55% of the crossflow channel bed, lea... A computational investigation of the mean flow field of turbulent rectangular jets issuing into a narrow channel crossflow is presented. The length of the jet slot spans more than 55% of the crossflow channel bed, leaving a small clearance between the jet edge and sidewalls. A finite volume code employing the standard k-εmodel is used to predict the mean, three-dimensional flow field. The mean flow field is investigated for two velocity ratios (6 and 9). Important flow features, such as the formation of different vortical structures and their characteristics owing to different values of the velocity ratio, are discussed. Some predicted results are compared with the experimental data reported in the literature. The predicted mean and turbulent flow properties are shown to be in good agreement with the experimental data. 展开更多
关键词 turbulent jet crossflow narrow charmel velocity ratio VORTICES
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Large-eddy simulations and vortex structures of turbulent jets in crossflow 被引量:5
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作者 GUAN Hui1,2 & WU ChuiJie2 1 School of Mechanical and Power Engineering,East China University of Science and Technology,Shanghai 200237,China 2 Research Center for Fluid Dynamics,PLA University of Science and Technology,Nanjing 211101,China 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2007年第1期118-132,共15页
Using the method of large-eddy simulation, the 3-dimensional turbulent jets in crossflow with stream-wise and transverse arrangements of nozzle are simulated, emphasizing on the dynamical process of generation and evo... Using the method of large-eddy simulation, the 3-dimensional turbulent jets in crossflow with stream-wise and transverse arrangements of nozzle are simulated, emphasizing on the dynamical process of generation and evolution of vortex structures in these flows. The results show that the basic vortex structures in literatures, such as the counter-rotating vortex pair, leading-edge vortices, lee-side vortices, hanging vortices, kidney vortices and anti-kidney vortices, are not independent physical substances, but local structures of the basic vortex structure of turbulent jets in crossflow-the 3-D stretching vortex rings originating from the orifice of the nozzle, which is discovered in this study. Therefore, the most important large-scale structures of turbulent jets in crossflow are unified to the 3-D vortex rings which stretch and twist in stream-wise and swing in transverse directions. We also found that the shedding frequencies of vortex rings are much lower than the one corresponding to the appearance of leading-edge and lee-side vortices in the turbulent jets. 展开更多
关键词 turbulent jet in crossflow COHERENT structure large-eddy simulation
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Effects of the jet-to-crossflow momentum ratio on a sonic jet into a supersonic crossflow 被引量:2
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作者 Guo-Lei Wang~(a)) and Xi-Yun Lu~(b)) Department of Modern Mechanics,University of Science and Technology of China,Hefei,Anhui 230026,China 《Theoretical & Applied Mechanics Letters》 CAS 2011年第1期53-57,共5页
Numerical investigation of a transverse sonic jet injected into a supersonic crossflow was carried out using large-eddy simulation for a free-stream Mach number M = 1.6 and a Reynolds number Re = 1.38×10~5 based ... Numerical investigation of a transverse sonic jet injected into a supersonic crossflow was carried out using large-eddy simulation for a free-stream Mach number M = 1.6 and a Reynolds number Re = 1.38×10~5 based on the jet diameter.Effects of the jet-to-crossflow momentum ratio on various fundamental mechanisms dictating the intricate flow phenomena,including flow structures, turbulent characters and frequency behaviors,have been studied.The complex flow structures and the relevant flow features are discussed to exhibit the evolution of shock structures,vortical structures and jet shear layers.The strength of the bow shock increases and the sizes of the barrel shock and Mach disk also increase with increasing momentum ratio.Turbulent characters are clarified to be closely related to the flow structures.The jet penetration increases with the increase of the momentum ratio.Moreover,the dominant frequencies of the flow structures are obtained using spectral analysis.The results obtained in this letter provide physical insight in understanding the mechanisms relevant to this complex flow 展开更多
关键词 large-eddy simulation compressible turbulent flow jet into supersonic crossflow
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FLOW CHARACTERISTICS OF TURBULENT JETS INJECTED OBLIQUELY IN CROSSFLOW 被引量:1
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作者 GUOTing-ting LIShao-hua XUZhong 《Journal of Hydrodynamics》 SCIE EI CSCD 2004年第3期312-315,共4页
Numerical simulation has been performed to investigate the characteristics ofthe turbulent jet issuing obliquely into a crossflow, at the injection angles of 90° and 60°. TheSIMPLEC algorithm in the body-fit... Numerical simulation has been performed to investigate the characteristics ofthe turbulent jet issuing obliquely into a crossflow, at the injection angles of 90° and 60°. TheSIMPLEC algorithm in the body-fitted coordinates and the wall-function method using the RNG k-εturbulence model have been adopted to simulate this flow at two jet-to-crossflow velocity ratios, 2and 4. The numerical results are good agreement with the experimental measurements, the jettrajectories have been given, the separation events in the lee of the jet exit have been found, andthe forming mechanism has been analyzed. 展开更多
关键词 crossflow turbulent jet turbulence model numerical simulation WAKE
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Fractal characteristics of round jets in steady crossflow 被引量:1
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作者 Yuliang Li Chaoquan Chen Chunbo Jiang 《Chinese Science Bulletin》 SCIE EI CAS 1999年第15期1366-1369,共4页
The fractal dimensions of turbulent round jets in steady crossflow has been analyzed by using planar laser-induced fluorescence (PLIF) method. The relation between the fractal dimension and the momentum ratio, the var... The fractal dimensions of turbulent round jets in steady crossflow has been analyzed by using planar laser-induced fluorescence (PLIF) method. The relation between the fractal dimension and the momentum ratio, the variation of the fractal dimension with the elevation of jet and the dilution have been investigated. The comparison of the fractal characteristics between the multiple jets and the signal jet has been carried out. 展开更多
关键词 STEADY crossflow turbulent jet measurement of FRACTAL dimension.
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急冷器内液滴运动蒸发的数值模拟 被引量:3
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作者 王健 仇性启 申玉辉 《石油化工》 CAS CSCD 北大核心 2011年第10期1073-1077,共5页
建立了错流射流单液滴蒸发运动过程的数学模型,对急冷器内急冷油液滴运动蒸发过程进行了数值模拟,探讨了液滴运动轨迹和蒸发特性。模拟结果表明,液滴初始直径越小,裂解气流温度越高,液滴蒸发越快,液滴生存时间越短;初始射流速度对急冷... 建立了错流射流单液滴蒸发运动过程的数学模型,对急冷器内急冷油液滴运动蒸发过程进行了数值模拟,探讨了液滴运动轨迹和蒸发特性。模拟结果表明,液滴初始直径越小,裂解气流温度越高,液滴蒸发越快,液滴生存时间越短;初始射流速度对急冷油液滴在裂解气流内的贯穿距离和生存时间影响较小,提高初始射流速度,并不能明显加速液滴蒸发;液滴初始直径、射流角度对液滴运动轨迹有较大影响;在液滴初始直径为1.0 mm、裂解气速度10.0 m/s、急冷油初始射流速度24.0 m/s的条件下,临界射流角度约为137°。 展开更多
关键词 急冷器 错流射流 液滴蒸发 液滴运动 裂解气
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展向喷嘴湍流横向射流大涡模拟及其统计分析 被引量:1
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作者 关晖 吴锤结 《力学季刊》 CSCD 北大核心 2013年第3期353-360,共8页
采用大涡模拟方法数值模拟了展向椭圆喷嘴的湍流横向射流,对其大尺度结构的时空演化和湍流脉动速度场的时间序列分析、频谱分析、PDF分析以及时、空截面上的统计平均特性进行分析。结果表明,在射流出口附近的下游核心区中速度脉动剧烈,... 采用大涡模拟方法数值模拟了展向椭圆喷嘴的湍流横向射流,对其大尺度结构的时空演化和湍流脉动速度场的时间序列分析、频谱分析、PDF分析以及时、空截面上的统计平均特性进行分析。结果表明,在射流出口附近的下游核心区中速度脉动剧烈,显现出明显的湍流特征.除了三维涡环脱落、扭曲、变形、摆动所对应频率之外,还存在很宽的湍流基频,它与在喷嘴出口附近产生的三维涡环的时空演化过程密切相关.由于展向椭圆喷嘴的湍流横向射流中的三维涡环快速脱落和强相互作用导致射流尾迹中的强湍流脉动,展向椭圆喷嘴湍流横向射流的PDF空间演化特征结构复杂。在射流核心区的湍流偏应力变化平缓,其统计平均值分布接近左右对称。展向椭圆喷嘴的湍流横向射流脉动速度场具有极为复杂的统计行为,与流向椭圆喷嘴相比具有更好的掺混能力。 展开更多
关键词 湍流横向射流 展向椭圆喷嘴 大涡模拟 湍流统计分析
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湍流横向射流大涡模拟及大尺度结构的涡环模型
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作者 关晖 吴锤结 《河海大学学报(自然科学版)》 CAS CSCD 北大核心 2005年第2期165-169,共5页
采用大涡模拟方法数值模拟了流向椭圆喷嘴的湍流横向射流,重点研究其旋涡结构的产生、发展等动力学演化过程.结果表明:文献中所报道的横向射流基本涡结构,如反向旋转涡对、前缘涡、后缘涡、悬涡、肾涡、反肾涡等并非独立的物理实体,而... 采用大涡模拟方法数值模拟了流向椭圆喷嘴的湍流横向射流,重点研究其旋涡结构的产生、发展等动力学演化过程.结果表明:文献中所报道的横向射流基本涡结构,如反向旋转涡对、前缘涡、后缘涡、悬涡、肾涡、反肾涡等并非独立的物理实体,而是分别对应于新发现的横向射流基本涡结构———起始于喷嘴的三维拉伸涡环的局部结构. 展开更多
关键词 湍流横向射流 拟序结构 大涡模拟 并行计算
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