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搅拌釜内气液动态相对稳定状态及雷诺数计算 被引量:2
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作者 赵英 张珍禛 +2 位作者 刘一哲 文家武 郭锴 《化学工程》 CAS CSCD 北大核心 2015年第5期49-52,67,共5页
设计了一种全新的测量搅拌釜内动态体系温度、压力的设备及方案,以CO2-H2O体系为特征体系,对搅拌状态下气液二相动态相对稳定状态进行了研究。搅拌釜内流体发生湍动,达到相平衡的气液二相的传质极限发生偏移。在不同温度(288.15—307.15... 设计了一种全新的测量搅拌釜内动态体系温度、压力的设备及方案,以CO2-H2O体系为特征体系,对搅拌状态下气液二相动态相对稳定状态进行了研究。搅拌釜内流体发生湍动,达到相平衡的气液二相的传质极限发生偏移。在不同温度(288.15—307.15 K)和转速(190—520 r/min)下进行实验,温度一定时,动态平衡偏移率随湍动程度的增大而增大。温度为307.15 K、转速为520 r/min时,动态平衡偏移率高达27%。利用动态平衡偏移率反算搅拌釜内的雷诺数ReD,将其与传统计算得出的雷诺数ReT进行比较拟合得到关联式。 展开更多
关键词 气液传质 搅拌 流体湍动 态传质平衡 雷诺数
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Turbulent boundary layers and hydrodynamic flow analysis of nanofluids over a plate 被引量:4
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作者 AOUINET Hana DHAHRI Maher +2 位作者 SAFAEI Mohammad Reza SAMMOUDA Habib ANQI Ali E. 《Journal of Central South University》 SCIE EI CAS CSCD 2021年第11期3340-3353,共14页
A numerical analysis of the log-law behavior for the turbulent boundary layer of a wall-bounded flow is performed over a flat plate immersed in three nanofluids(Zn O-water,SiO_(2)-water,TiO_(2)-water).Numerical simula... A numerical analysis of the log-law behavior for the turbulent boundary layer of a wall-bounded flow is performed over a flat plate immersed in three nanofluids(Zn O-water,SiO_(2)-water,TiO_(2)-water).Numerical simulations using CFD code are employed to investigate the boundary layer and the hydrodynamic flow.To validate the current numerical model,measurement points from published works were used,and the compared results were in good compliance.Simulations were carried out for the velocity series of 0.04,0.4 and 4 m/s and nanoparticle concentrations0.1% and 5%.The influence of nanoparticles’ concentration on velocity,temperature profiles,wall shear stress,and turbulent intensity was investigated.The obtained results showed that the viscous sub-layer,the buffer layer,and the loglaw layer along the potential-flow layer could be analyzed based on their curving quality in the regions which have just a single wall distance.It was seen that the viscous sub-layer is the biggest area in comparison with other areas.Alternatively,the section where the temperature changes considerably correspond to the thermal boundary layer’s thickness goes a downward trend when the velocity decreases.The thermal boundary layer gets deep away from the leading edge.However,a rise in the volume fraction of nanoparticles indicated a minor impact on the shear stress developed in the wall.In all cases,the thickness of the boundary layer undergoes a downward trend as the velocity increases,whereas increasing the nanoparticle concentrations would enhance the thickness.More precisely,the log layer is closed with log law,and it is minimal between Y^(+)=50 and Y^(+)=95.The temperature for nanoparticle concentration φ=5%is higher than that for φ=0.1%,in boundary layers,for all studied nanofluids.However,it is established that the behavior is inverted from the value of Y^(+)=1 and the temperature for φ =0.1% is more important than the case of φ =5%.For turbulence intensity peak,this peak exists at Y^(+)=100 for v=4 m/s,Y^(+)=10 for v=0.4 m/s and Y^(+)=8 for v=0.04 m/s. 展开更多
关键词 turbulent boundary layers nanofluids hydrodynamic flow wall shear stress turbulent intensity
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Computational fluid dynamics simulation of gas-liquid two phases flow in 320 m^3 air-blowing mechanical flotation cell using different turbulence models 被引量:4
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作者 沈政昌 陈建华 +2 位作者 张谌虎 廖幸锦 李玉琼 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第6期2385-2392,共8页
According to the recently developed single-trough floating machine with the world's largest volume(inflatable mechanical agitation flotation machine with volume of 320 m3) in China, the gas-fluid two-phase flow in... According to the recently developed single-trough floating machine with the world's largest volume(inflatable mechanical agitation flotation machine with volume of 320 m3) in China, the gas-fluid two-phase flow in flotation cell was simulated using computational fluid dynamics method. It is shown that hexahedral mesh scheme is more suitable for the complex structure of the flotation cell than tetrahedral mesh scheme, and a mesh quality ranging from 0.7 to 1.0 is obtained. Comparative studies of the standard k-ε, k-ω and realizable k-ε turbulence models were carried out. It is indicated that the standard k-ε turbulence model could give a result relatively close to the practice and the liquid phase flow field is well characterized. In addition, two obvious recirculation zones are formed in the mixing zones, and the pressure on the rotor and stator is well characterized. Furthermore, the simulation results using improved standard k-ε turbulence model show that surface tension coefficient of 0.072, drag model of Grace and coefficient of 4, and lift coefficient of 0.001 can be achieved. The research results suggest that gas-fluid two-phase flow in large flotation cell can be well simulated using computational fluid dynamics method. 展开更多
关键词 computational fluid dynamics (CFD) simulation flotation cell gas-liquid two-phases flow
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