Computational Fluid Dynamic Analysis of a Marine Hydrokinetic Crossflow Turbine in Low Reynolds Number Flow

Minh N. Doan, Ivan H. Alayeto, Kana Kumazawa, S. Obi
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引用次数: 4

Abstract

This study focuses on surveying different turbulence models and dynamic mesh techniques to simulate a marine hydrokinetic (MHK) crossflow turbine at Rec ≈ 7,000. While several research projects have shown that studies of MHK devices in low Re flow could still yield interesting and significant results, existing computational fluid dynamic (CFD) simulations were conducted at the chord based Re of 105 ∼ 106. The wake and power production of a laboratory-scaled MHK crossflow turbine were numerically simulated and compared with relevant experimental data. The vertical axis turbine operated in a small flume with 20% blockage ratio and was fabricated by mounting three NACA0012 (2.54 cm chord length) straight blades at a radius of 3.41 cm and 15° pitch angle. Within OpenFOAM environment, blade-resolved models were built with Spalart-Allmaras, k-omega shear stress transport (SST), and k-kl-omega unsteady Reynolds-averaged Navier-Stokes simulation (URANS) in both two and three dimensions. Results from each model were compared with the experimental power measurement and flow field obtained by monoscopic particle image velocimetry (2D PIV). Additionally, four different techniques for moving the solid boundaries (turbine blades) in the unsteady simulation were presented and compared in terms of solution consistency and required computational power. Overset mesh, time-deforming mesh, and moving immersed boundary are all available in this open source environment, beside the common rotating mesh technique, and possess the potential to be applied to a more complicated configuration of turbines.
船用低雷诺数水动力横流涡轮计算流体动力学分析
本文主要研究了不同的湍流模型和动态网格技术,以模拟Rec≈7,000的海洋水动力(MHK)横流涡轮机。虽然一些研究项目已经表明,在低回流条件下对MHK装置的研究仍然可以产生有趣和重要的结果,但现有的计算流体动力学(CFD)模拟是在105 ~ 106的弦流条件下进行的。对实验室规模的MHK横流涡轮的尾迹和功率产生进行了数值模拟,并与相关实验数据进行了比较。垂直轴涡轮在堵塞比为20%的小水槽中运行,由3个NACA0012(弦长2.54 cm)直叶片以3.41 cm半径和15°俯角安装而成。在OpenFOAM环境下,采用Spalart-Allmaras、k-omega剪切应力输运(SST)和k-kl-omega非定常reynolds -average Navier-Stokes模拟(URANS)在二维和三维上建立叶片解析模型。将各模型的计算结果与实验功率测量结果和单镜粒子图像测速(2D PIV)得到的流场结果进行了比较。此外,在非定常模拟中,提出了四种不同的移动固体边界(涡轮叶片)的技术,并在解的一致性和所需的计算能力方面进行了比较。在这个开源环境中,除了常见的旋转网格技术之外,覆盖网格,时间变形网格和移动浸入边界都是可用的,并且具有应用于更复杂的涡轮机配置的潜力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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