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Flow of a nanofluid in the microspacing within co-rotating discs of a Tesla turbine

机译:特斯拉涡轮机同向旋转盘内微间距中纳米流体的流动

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This article presents, for the first time, the fluid dynamics of the rotating flow of a nanofluid through the narrow spacings within co-rotating discs of a Tesla turbine. The inter-disc-spacing of multiple concentric discs of a Tesla disc turbine is usually of the order of 100 μm. The study is conducted with the help of both mathematical analysis and computational fluid dynamic simulations. Numerical values are reported for a specific nanofluid which is a dilute solution of ferro-particles in water (maximum volume fraction considered is 0.05). The velocity field, pressure field and fluid pathlines are calculated in the three-dimensional, axi-symmetric flow domain for prescribed boundary values for the velocity components at inlet. Detailed comparisons between the analytical and computational solutions are provided. It is explained how the fluid dynamics of rotating flow within a Tesla disc turbine is influenced by the change in volume fraction of nanoparticles. The present study reveals that, with an increase in the volume fraction of nanoparticles, the pressure-drop in the radial direction increases; the tangential velocity at any point inside the computational domain tends to increase (even though its boundary value at inlet is kept fixed for each set of computation); however, the radial velocity field remains almost invariant. The present analysis shows that, with a suitable selection of the combination of geometric and flow parameters, the use of nanofluid leads to a significant improvement in the power output (the magnitude of increase would depend on the choice of nanofluid; the sample calculations show more than 30% increase in power output when the volume fraction of nanoparticles increases from 0 to 0.05). Moreover, the gain in power output is achieved without appreciably affecting the efficiency of the turbine. Indeed the present study shows that it is possible to achieve a high efficiency (a figure of 56% is included in the paper as a sample case), revealing the potential of the Tesla disc turbine to emerge as an attractive engineering product in the field of micro-turbines.
机译:本文首次展示了纳米流体通过特斯拉涡轮机同向旋转盘内狭窄空间的旋转流的流体动力学。 Tesla盘式涡轮机的多个同心盘的盘间间距通常为100μm量级。该研究是在数学分析和计算流体动力学模拟的帮助下进行的。报道了特定纳米流体的数值,该纳米流体是铁颗粒在水中的稀溶液(认为最大体积分数为0.05)。速度场,压力场和流体路径线是在三维轴对称流域中针对入口处速度分量的指定边界值进行计算的。提供了分析和计算解决方案之间的详细比较。解释了特斯拉盘式涡轮机内旋转流的流体动力学如何受到纳米颗粒体积分数变化的影响。本研究表明,随着纳米颗粒体积分数的增加,径向压降增加。计算域内任意点处的切线速度趋于增加(即使对于每组计算,入口处的边界值保持固定);但是,径向速度场几乎保持不变。本分析表明,通过适当选择几何参数和流量参数的组合,使用纳米流体可显着提高功率输出(增加的幅度取决于纳米流体的选择;样本计算显示出更多)当纳米粒子的体积分数从0增加到0.05时,功率输出将增加30%以上)。而且,在不明显影响涡轮效率的情况下实现了功率输出的增益。的确,本研究表明,有可能实现高效率(作为示例,论文中包含56%的数字),这揭示了Tesla盘式涡轮机有潜力在以下领域成为有吸引力的工程产品:微型涡轮机。

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