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脉动气流喷雾干燥的数值模拟 被引量:7
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作者 吴中华 刘相东 《农业工程学报》 EI CAS CSCD 北大核心 2002年第4期18-21,共4页
利用 CFD模型对脉动气流喷雾干燥过程进行了数值模拟 ,得到了干燥过程中干燥室气体流场和颗粒运动轨迹、气体局部湿度和温度变化及不同初始直径颗粒在干燥室内干燥情况的详细信息 ,解决了由于难以动态测量上述参数而不能清楚了解该干燥... 利用 CFD模型对脉动气流喷雾干燥过程进行了数值模拟 ,得到了干燥过程中干燥室气体流场和颗粒运动轨迹、气体局部湿度和温度变化及不同初始直径颗粒在干燥室内干燥情况的详细信息 ,解决了由于难以动态测量上述参数而不能清楚了解该干燥过程的难题。模拟结果表明脉动气流喷雾干燥具有干燥时间短 ,蒸发速度大等特点。 展开更多
关键词 脉动气 流喷雾干燥 数值模拟 物料干燥 气体动力学分析
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Numerical simulation study of gob air leakage field and gas migration regularity in downlink ventilation 被引量:4
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作者 ZHANG Jian-rang WANG Chun-qiao DONG Ding-wen 《Journal of Coal Science & Engineering(China)》 2011年第3期316-320,共5页
Aiming at the issue that mass of gas emission from mining gob and the gas exceeded in working face, gob air leakage field and gas migration regularity in downlink ventilation was studied. In consideration of the influ... Aiming at the issue that mass of gas emission from mining gob and the gas exceeded in working face, gob air leakage field and gas migration regularity in downlink ventilation was studied. In consideration of the influence of natural wind pressure to analyze the stope face differential pressure, gob air leakage field distribution and gas migration regularity theoretically. Established a two-dimensional physical model with one source and one doab, and applied computational fluid dynamics analysis software Fluent to do numerical simulation, analyzed and contrasted to the areas of gob air leakage on size and gas emission from gob to working face on strength when using the downlink ventilation and uplink ventilation. When applied downward ventilation in stope face, the air leakage field of gob nearly working face, and the air leakage intensity were smaller than uplink, this can effectively reduce the gas emission from gob to working face; when used downlink ventilation, the air leakage airflow carry the lower amount of gas to doab than uplink ventilation, and more easily to mix the gas, reduced the possibility of gas accumulation in upper comer and the stratified flows, it can provide protection to mine with safe and effective production. 展开更多
关键词 downlink ventilation natural wind pressure air leakage field gas migration numerical simulation
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Unsteady simulation for a high-speed train entering a tunnel 被引量:10
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作者 Xin-hua LI Jian DENG +2 位作者 Da-wei CHEN Fang-fang XIE Yao ZHENG 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2011年第12期957-963,共7页
In order to study the unsteady aerodynamics effects in railway tunnels,the 3D Reynolds average Navier-Stokes equations of a viscous compressible fluid are solved,and the two-equation k-ε model is used in the simulati... In order to study the unsteady aerodynamics effects in railway tunnels,the 3D Reynolds average Navier-Stokes equations of a viscous compressible fluid are solved,and the two-equation k-ε model is used in the simulation of turbulence,while the dynamic grid technique is employed for moving bodies.We focus on obtaining the changing tendencies of the aerodynamic force of the train and the aerodynamic pressures on the tunnel wall and train surface,and discovering the relationship between the velocity of the train and the intensity of the micro pressure wave at the tunnel exit.It is shown that the amplitudes of the pressure changes in the tunnel and on the train surface are both approximately proportional to the square of the train speed,so are the microwave and the drag of the train. 展开更多
关键词 High-speed train AERODYNAMICS Railway tunnel Numerical analysis
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Compressor and Turbine Multidisciplinary Design for Highly Efficient Micro-gas Turbine 被引量:2
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作者 BARSI Dario PERRONE ANDrea +4 位作者 QU Yonglei RATTO Luca RICCI Gianluca SERGEEV Vitaliy ZUNINO Pietro 《Journal of Thermal Science》 SCIE EI CAS CSCD 2018年第3期259-269,共11页
Multidisciplinary design optimization (MDO) is widely employed to enhance turbomachinery compo- nents efficiency. The aim of this work is to describe a complete tool for the aero-mechanical design of a radial in- fl... Multidisciplinary design optimization (MDO) is widely employed to enhance turbomachinery compo- nents efficiency. The aim of this work is to describe a complete tool for the aero-mechanical design of a radial in- flow turbine and a centrifugal compressor. The high rotational speed of such machines and the high exhaust gas temperature (only for the turbine) expose blades to really high stresses and therefore the aerodynamics design has to be coupled with the mechanical one through an integrated procedure. The described approach employs a fuUy 3D Reynolds Averaged Navier-Stokes (RANS) solver for the aerodynamics and an open source Finite Element Analysis (FEA) solver for the mechanical integrity assessment. Due to the high computational cost of both these two solvers, a meta model, such as an artificial neural network (ANN), is used to speed up the optimization design process. The interaction between two codes, the mesh genera- tion and the post processing of the results are achieved via in-house developed scripting modules. The obtained results are widely presented and discussed. 展开更多
关键词 Micro-gas turbine Multidisciplinary Optimization Centrifugal Compressor Centripetal Turbine
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