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首页> 外文期刊>International Journal of Naval Architecture and Ocean Engineering >Effects of boundary layer and liquid viscosity and compressible air on sloshing characteristics
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Effects of boundary layer and liquid viscosity and compressible air on sloshing characteristics

机译:边界层,液体粘度和可压缩空气对晃荡特性的影响

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In this paper, numerical investigations for tank sloshing, based on commercial CFD package FLUENT, are performed to study effects of boundary layer grid, liquid viscosity and compressible air on sloshing pressure, wave height and rising time of impact pressure. Also, sloshing experiments for liquids of different viscosity are carried out to validate the numerical results. Through comparison of numerical and experimental results, a computational model including boundary layer grid can predict the sloshing pressure more accurately. Energy dissipation due to viscous friction leads to reduction of sloshing pressure and wave elevation. Sloshing pressure is also reduced because of cushion effect of compressible air. Due to high viscosity damping effect and compressible air effect, the rising time of impact pressure becomes longer. It is also found that liquid viscosity and compressible air influence distribution of dynamic pressure along the vertical tank wall.
机译:本文基于商业CFD组件FLUENT,对油箱晃荡进行了数值研究,以研究边界层网格,液体粘度和可压缩空气对晃荡压力,波高和冲击压力上升时间的影响。另外,针对不同粘度的液体进行了晃荡实验,以验证数值结果。通过数值和实验结果的比较,包括边界层网格的计算模型可以更准确地预测晃荡压力。粘性摩擦导致的能量耗散会导致晃动压力和波高降低。由于可压缩空气的缓冲作用,晃动压力也降低了。由于高粘度阻尼效应和可压缩空气效应,冲击压力的上升时间变得更长。还发现,液体粘度和可压缩空气影响沿垂直罐壁的动压分布。

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