首页> 外文会议>ASME turbo expo: turbomachinery technical conference and exposition >THREE-DIMENSIONAL VISUALIZATION OF FLOW CHARACTERISTICS USING A MAGNETIC RESONANCE IMAGING (MRI) IN A LATTICE COOLING CHANNEL
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THREE-DIMENSIONAL VISUALIZATION OF FLOW CHARACTERISTICS USING A MAGNETIC RESONANCE IMAGING (MRI) IN A LATTICE COOLING CHANNEL

机译:晶格冷却通道中使用磁共振成像(MRI)的流动特性的三维可视化

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Flow structures in lattice cooling channels are investigated experimentally by measuring three-dimensional velocity components over entire duct. The lattice cooling structure is formed by crossing two sets of parallel inclined ribs. Heat transfer is enhanced when coolant flows through the narrow sub-channels between the ribs. According to the past literature, longitudinal vortex structures are formed inside the subchannels due to interactions between crossing flows. In this study, three-dimensional velocity field measurement is performed using MRI scanner to clarify the flow mechanism. The rib inclination angle is varied from 30 to 60 degrees. Reynolds number is set at approximately 8,000 based on the whole duct inlet hydraulic diameter and bulk velocity. Working fluid is 0.015mol/L copper sulfate aqueous solution. Measured results show that coolants in the upper and lower sub-channels interact not only at the both ends of the duct, but also at diamond-shaped openings formed by opposite sub-channels. The exchange of momentum between the upper and lower sub-channels occurs at the openings, leading to sustained longitudinal vortex in each sub-channel as mentioned in the literature. When the ribs are arranged with obtuse angle, a large vortex spreads across the contact surface, while the vortex structure independently stays in each sub-channel for acute rib angle. The measured velocity fields are compared with numerically-simulated ones using a RANS solver. Overall flow pattern is captured, but flow interaction between the upper and lower sub-channels is underestimated.
机译:通过测量整个管道上的三维速度分量,对格子冷却通道中的流动结构进行了实验研究。格子冷却结构是通过使两组平行的倾斜肋交叉而形成的。当冷却剂流过肋之间的狭窄子通道时,传热会增强。根据过去的文献,由于交叉流之间的相互作用,在子通道内部形成了纵向涡旋结构。在这项研究中,使用MRI扫描仪进行三维速度场测量,以阐明流动机理。肋骨倾斜角度从30度到60度不等。根据整个管道入口的液压直径和整体速度,雷诺数设置为大约8,000。工作液为0.015mol / L的硫酸铜水溶液。测量结果表明,上下子通道中的冷却剂不仅在管道的两端相互作用,而且在相对的子通道形成的菱形开口处也相互作用。上部子通道和下部子通道之间的动量交换发生在开口处,从而导致每个子通道中持续的纵向涡流,如文献所述。当肋以钝角布置时,大的涡流在接触表面上扩散,而涡结构独立地停留在每个子通道中,以形成锐角。使用RANS求解器将测得的速度场与数值模拟的速度场进行比较。捕获了总体流动模式,但是上,下子通道之间的流动相互作用被低估了。

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