Numerical Prediction of Cavitation for a Horizontal Axis Tidal Turbine

IF 2 3区 工程技术 Q3 MECHANICS
Adriano Evangelisti, Giuliano Agati, Domenico Borello, Luca Mazzotta, Paolo Capobianchi, Paolo Venturini
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引用次数: 0

Abstract

This paper aims at assessing cavitation in a scaled tidal turbine geometry through numerical simulations. Cavitation occurrence is predicted by using the Singhal cavitation model, based on the Rayleigh-Plesset equation, for treating bubble dynamics. Turbulence is modelled adopting a Reynolds Averaged Navier Stokes (RANS) approach, specifically employing the Shear Stress Transport (SST) k-ω model to simulate the fluid flow. The Reboud density function is applied to adjust the eddy viscosity computation in the cavitation region. Initially, cavitation and turbulence models are validated using a NACA 66 (mod) hydrofoil profile as a test case. Numerical and experimental pressure coefficients are compared on the hydrofoil suction side for a selected cavitation condition. A Mesh Sensitivity Analysis (MSA) is performed to ensure simulation accuracy, comparing numerical results with experimental data on the Horizontal Axis Tidal Turbine (HATT) scaled domain. Based on this analysis, the optimal computational grid is selected. Experimental and numerical power and thrust coefficients are then compared across different tip speed ratios. Finally, cavitation occurrence is evaluated for four different regimes, namely the cut-in, the peak-power, the curve highest velocity and the off-set tip speed ratios. Computational Fluid Dynamics (CFD) solutions reveal vapor formation around turbine components, highlighting regions most exposed to cavitation onset.

水平轴潮汐水轮机空化的数值预测
本文旨在通过数值模拟来评估潮汐涡轮机几何形状中的空化现象。采用基于Rayleigh-Plesset方程的Singhal空化模型对气泡动力学进行了预测。湍流模型采用Reynolds average Navier Stokes (RANS)方法,特别是采用剪切应力输运(SST) k-ω模型来模拟流体流动。利用反弹密度函数对空化区的涡动粘度计算进行了调整。首先,使用NACA 66 (mod)水翼剖面作为测试用例验证了空化和湍流模型。在选定的空化条件下,比较了水翼吸力侧的数值压力系数和实验压力系数。为了保证仿真精度,在水平轴潮汐水轮机(HATT)标度域进行了网格敏感性分析(MSA),并将数值结果与实验数据进行了比较。在此基础上,选择了最优计算网格。然后比较了不同叶尖速比下的实验和数值功率和推力系数。最后,评估了四种不同情况下的空化发生情况,即切入、峰值功率、曲线最高速度和偏移尖端速度比。计算流体动力学(CFD)解决方案揭示了涡轮部件周围的蒸汽形成,突出了最容易出现空化的区域。
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来源期刊
Flow, Turbulence and Combustion
Flow, Turbulence and Combustion 工程技术-力学
CiteScore
5.70
自引率
8.30%
发文量
72
审稿时长
2 months
期刊介绍: Flow, Turbulence and Combustion provides a global forum for the publication of original and innovative research results that contribute to the solution of fundamental and applied problems encountered in single-phase, multi-phase and reacting flows, in both idealized and real systems. The scope of coverage encompasses topics in fluid dynamics, scalar transport, multi-physics interactions and flow control. From time to time the journal publishes Special or Theme Issues featuring invited articles. Contributions may report research that falls within the broad spectrum of analytical, computational and experimental methods. This includes research conducted in academia, industry and a variety of environmental and geophysical sectors. Turbulence, transition and associated phenomena are expected to play a significant role in the majority of studies reported, although non-turbulent flows, typical of those in micro-devices, would be regarded as falling within the scope covered. The emphasis is on originality, timeliness, quality and thematic fit, as exemplified by the title of the journal and the qualifications described above. Relevance to real-world problems and industrial applications are regarded as strengths.
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