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特大井喷H_2S扩散的数值模拟分析 被引量:11
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作者 练章华 周兆明 +2 位作者 王辉 李孝军 林铁军 《天然气工业》 EI CAS CSCD 北大核心 2009年第11期112-115,共4页
含H2S气体的高压井喷是一个非常复杂的扩散问题,涉及多组分气体的混合、运移、扩散、气象条件以及复杂的地形空间影响。为此,采用可行的计算流体动力学(CFD)对这一复杂的大空间流场问题进行了数值模拟研究,根据重庆开县特大井喷事故现... 含H2S气体的高压井喷是一个非常复杂的扩散问题,涉及多组分气体的混合、运移、扩散、气象条件以及复杂的地形空间影响。为此,采用可行的计算流体动力学(CFD)对这一复杂的大空间流场问题进行了数值模拟研究,根据重庆开县特大井喷事故现场三维地貌等高线数据建立了井喷H2S扩散的CFD流场计算的有限元模型,结合当时气象条件,用Fluent软件的UDF功能编写了边界间歇风速的函数,数学模型中采用了适合于预测大气流动的大涡模拟运动方程,将CFD有限元模型和建立的数学模型用Fluent软件的解算器,对H2S气体的扩散和运移规律进行了详细的数值模拟研究,获得了H2S气体在该井场周围山谷地形的积聚、运移规律以及风向对气云扩散的影响,获得了H2S和CH4两种气体扩散的时空分布云图。模拟结果和事故现场调查结果一致。 展开更多
关键词 井喷H2S CH4 cfd扩散 数值模拟 开县
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CFD study of flow-diffusion process in Y-shape micromixer
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作者 陈卓 张睿琦 王晓娜 《Journal of Central South University》 SCIE EI CAS CSCD 2016年第4期969-974,共6页
A CFD simulation was carried out to investigate the mixing process in a Y-shape micromixer with the software Fluent 6.3. The definition of the "diffusion angle" is proposed to describe the molecular diffusio... A CFD simulation was carried out to investigate the mixing process in a Y-shape micromixer with the software Fluent 6.3. The definition of the "diffusion angle" is proposed to describe the molecular diffusion process associated with the flow at low Reynolds number. The linear relationship between the diffusion angle and the Peclet number(Pe) is determined by both theoretical analysis and numerical simulation. Moreover, the simulation results reveal that the diffusion angle is only related to the Peclet number whilst it is irrelevant to the changes of Re(Reynolds number) and Sc(Schmidt number). The range of Peclet number and Reynolds number for experimental measurement are also suggested as Pe≤10000 and Re≤10. 展开更多
关键词 SIMULATION flow-diffusion process molecular diffusion Y-shape micromixer
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Influence of impeller diameter on overall gas dispersion properties in a sparged multi-impeller stirred tank 被引量:4
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作者 包雨云 王冰洁 +2 位作者 林明丽 高正明 杨杰 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2015年第6期890-896,共7页
The impeller configuration with a six parabolic blade disk turbine below two down-pumping hydrofoil propellers, identified as PDT + 2CBY, was used in this study. The effect of the impeller diameter D, ranging from0.30... The impeller configuration with a six parabolic blade disk turbine below two down-pumping hydrofoil propellers, identified as PDT + 2CBY, was used in this study. The effect of the impeller diameter D, ranging from0.30 T to 0.40T(T as the tank diameter), on gas dispersion in a stirred tank of 0.48 m diameter was investigated by experimental and CFD simulation methods. Power consumption and total gas holdup were measured for the same impeller configuration PDT + 2CBY with four different D/T. Results show that with D/T increases from 0.30 to 0.40, the relative power demand(RPD) in a gas–liquid system decreases slightly. At low superficial gas velocity VSof 0.0078 m·s-1, the gas holdup increases evidently with the increase of D/T. However, at high superficial gas velocity, the system with D/T = 0.33 gets a good balance between the gas recirculation and liquid shearing rate, which resulted in the highest gas holdup among four different D/T. CFD simulation based on the two-fluid model along with the Population Balance Model(PBM) was used to investigate the effect of impeller diameter on the gas dispersion. The power consumption and total gas holdup predicted by CFD simulation were in reasonable agreement with the experimental data. 展开更多
关键词 Gas holdup MIXING Multiphase reactors Relative power demand cfd Multi-impeller stirred tank
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CFD investigation and PIV validation of flow field in a compact return diffuser under strong part-load conditions 被引量:9
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作者 ZHOU Ling SHI WeiDong +1 位作者 CAO WeiDong YANG HongBin 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2015年第3期405-414,共10页
The internal flow fields in a compact return diffuser under strong part-load conditions are investigated both numerically and experimentally.For numerical simulation,three-dimensional unsteady Reynolds-Averaged Navier... The internal flow fields in a compact return diffuser under strong part-load conditions are investigated both numerically and experimentally.For numerical simulation,three-dimensional unsteady Reynolds-Averaged Navier–Stokes equations are solved on high-quality structured grids in conjunction with the shear stress transport k–turbulence model by employing the computational fluid dynamics(CFD)software ANSYS-Fluent 14.5.For flow field measurements,a special test rig is designed and the two-dimensional particle image velocimetry(PIV)measurements are conducted in the diffuser midplane to capture the complex flow field and for validation of the CFD results.The analysis of the results has been focused on the flow structure in the diffuser,especially under part-load conditions.The detailed comparison between CFD and PIV results is performed.Vortical flow and recirculation flow patterns in the diffuser are captured and analyzed.Large flow separation and backflow appear under the part-load flow conditions.This paper provides a good data set for developing as well as evaluating the accuracy of various CFD models for capturing the complex flow field in a compact return diffuser used with multistage pumps. 展开更多
关键词 return diffuser numerical simulations part-load conditions particle image velocimetry
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Noise Reduction and Surge Margin Improvement Using Tapered Diffuser Vane in a Centrifugal Compressor 被引量:3
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作者 Takashi Goto Eri Ohmoto +1 位作者 Yutaka Ohta Eisuke Outa 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第1期21-25,共5页
Improvement of surge margin and reduction of interaction tone noise radiated from a centrifugal compressor with a vaned diffuser is discussed from experiments and CFD analyses.Two types of one-side tapered diffuser va... Improvement of surge margin and reduction of interaction tone noise radiated from a centrifugal compressor with a vaned diffuser is discussed from experiments and CFD analyses.Two types of one-side tapered diffuser vanes,which are shroud-and hub-side tapered vanes,were used in the experiments.The height of the leading edge of the tapered vanes varied from 100% to 10%.Both types of tapered vanes are effective for the reduction of the interaction tone noise radiated from the compressor,because of the smaller interaction area between impeller-discharge flow and diffuser vane surface.Especially,the hub-side tapered diffuser vane suppresses the evolution of the leading-edge vortex,which causes reverse-flow in the diffuser passage.Furthermore,the hub-side tapered diffuser vane,which has an optimized diffuser leading edge shape,can improve the compressor pressure-rise characteristics at low-flow operation and can enlarge the surge margin. 展开更多
关键词 Centrifugal compressor tapered diffuser vane interaction tone noise cfd
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