THE PERFORMANCE OF A NEW IMMERSED BOUNDARY METHOD ON SIMULATING UNDERWATER LOCOMOTION AND SWIMMING

A. Hemmati, Utku Senturk, T. Buren, A. Smits
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The differences in thrust generation and propulsion efficiency of square and convex thin panels are examined to identify the effect of trailing edge shape using proper orthogonal decomposition. The effect of Reynolds number is also evaluated by comparing the wake at Reynolds numbers of 2,000 and 10,000. INTRODUCTION Many biological species have evolved to develop efficient propulsive systems for swimming that also exhibit high speed and maneuverability (Sambiley, 1990; Sumich & Morrissey, 2004). Understanding the mechanics of aquatic propulsion has attracted the attention of many researchers over the years. Such explorations can yield valuable information on designing energy efficient and fast systems with high maneuverability and stealth that match and possibly surpass the performance of biological species. In this regard, it is often useful to focus on simple systems that can be used to study fundamental aspects of swimming performance. For instance, the implications of the trailing-edge shape of a tail fin as well as its orientation and movement (that is, harmonic fin motion) on the formation of vortex structures, wake dynamics and thrust generation plays a dominant role in understanding physics of fish-like swimming (Van Buren et al., 2016). The oscillating motion of a NACA 0012 airfoil was studied by Triantafyllou et al. (1991) as a representative of swimming motion by fish, which demonstrated a maximum propulsive efficiency of 25% for the Strouhal number St = 0.25− 0.35, where St = fpc/U , fp is the frequency of oscillation, c is the fin characteristic length, and U is the swimming speed. The extensive study by Buchholz & Smits (2006) on the wake of a pitching rigid rectangular panel at moderate Reynolds numbers (Re =Uc/ν) revealed that the flow is dominated by horseshoe-like structures. The aspect ratio of the panel was identified to impact the wake, and thus, the propulsive performance efficiency, which ranged from 9%− 21%. Green & Smits (2008) investigated the distribution of pressure on the pitching panel, which revealed that the favorable streamwise pressure gradient that is present over most of the panel reversed near the trailing edge. There are many experimental challenges, however, in determining detailed surface pressure distributions in unsteady wakes, and it is even more difficult to determine the instantaneous shear stress distributions. In contrast, computational fluid dynamics (CFD) can be used to give insight into the stress distributions, and characterize the wake and identify implications of the wake dynamics on thrust generation. CFD simulations can also be helpful in providing insight into wake structures, their formation and interactions, and the effects of Reynolds number. Numerical simulations of Blondeaux et al. 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引用次数: 3

Abstract

We report the benchmark results of a new Immersed Boundary Method (IBM) incorporated into Direct Numerical Simulation (DNS) of a pitching panel, representing fishlike swimming, using foam-extend-3.2. The panel is flat and thin, and it has a triangular (convex) trailing edge, similar to that seen in the caudal fin of some fish. The accuracy of the solver is verified by comparing four cases of bluff body wake simulations with reported experimental and numerical studies. For example, the structure of the mean wake compared well with that obtained using PIV in a companion experiment. The differences in thrust generation and propulsion efficiency of square and convex thin panels are examined to identify the effect of trailing edge shape using proper orthogonal decomposition. The effect of Reynolds number is also evaluated by comparing the wake at Reynolds numbers of 2,000 and 10,000. INTRODUCTION Many biological species have evolved to develop efficient propulsive systems for swimming that also exhibit high speed and maneuverability (Sambiley, 1990; Sumich & Morrissey, 2004). Understanding the mechanics of aquatic propulsion has attracted the attention of many researchers over the years. Such explorations can yield valuable information on designing energy efficient and fast systems with high maneuverability and stealth that match and possibly surpass the performance of biological species. In this regard, it is often useful to focus on simple systems that can be used to study fundamental aspects of swimming performance. For instance, the implications of the trailing-edge shape of a tail fin as well as its orientation and movement (that is, harmonic fin motion) on the formation of vortex structures, wake dynamics and thrust generation plays a dominant role in understanding physics of fish-like swimming (Van Buren et al., 2016). The oscillating motion of a NACA 0012 airfoil was studied by Triantafyllou et al. (1991) as a representative of swimming motion by fish, which demonstrated a maximum propulsive efficiency of 25% for the Strouhal number St = 0.25− 0.35, where St = fpc/U , fp is the frequency of oscillation, c is the fin characteristic length, and U is the swimming speed. The extensive study by Buchholz & Smits (2006) on the wake of a pitching rigid rectangular panel at moderate Reynolds numbers (Re =Uc/ν) revealed that the flow is dominated by horseshoe-like structures. The aspect ratio of the panel was identified to impact the wake, and thus, the propulsive performance efficiency, which ranged from 9%− 21%. Green & Smits (2008) investigated the distribution of pressure on the pitching panel, which revealed that the favorable streamwise pressure gradient that is present over most of the panel reversed near the trailing edge. There are many experimental challenges, however, in determining detailed surface pressure distributions in unsteady wakes, and it is even more difficult to determine the instantaneous shear stress distributions. In contrast, computational fluid dynamics (CFD) can be used to give insight into the stress distributions, and characterize the wake and identify implications of the wake dynamics on thrust generation. CFD simulations can also be helpful in providing insight into wake structures, their formation and interactions, and the effects of Reynolds number. Numerical simulations of Blondeaux et al. (2005) on a pitching foil showed vortex-loop (chain-like) structures dominate the wake at Re = 1000, as found experimentally by Green et al. (2011). Blondeaux et al. (2005) used a distinctly developed CFD solver based on the Immersed Boundary Method (IBM). Jantzen et al. (2014) also used an IBM-based CFD solver to evaluate the wake of pitching rigid rectangular panels at Re = 300. This study provided details on the vortex formation process in the wake of rectangular panels of aspect ratios 2 and 4, revealing that the Reynolds number influences the formation frequency and length of leading edge vortices, and that higher aspect ratios result in early detachment of leading edge vortices. The IBM is routinely used in fluid flow simulations as an alternative to the boundary-fitted method due to its lower computational cost. The IBM formulation in foam-extend3.2 uses a discrete forcing approach based on a weighted least square approximation to impose boundary conditions independent of the actual boundaries. This approach can capture the boundary as a sharp interface, which eliminates the issue of smearing. It also mitigates the distortion of cells around the moving boundaries, while alleviating errors that arise from transformation of curvilinear grids (Lundquist et al., 2009). See also Iaccarino & Verzicco (2003) and Mittal & Iaccarino (2005). Jasak et al. (2014) incorporated the IBM forcing approach into OpenFOAM as part of foam-extend-3.2. Case studies included flows over fixed bodies. In particular, a high Re flow case using the k− ε model showed a lack of stability for extreme mesh refinements. Şentürk et al. (2016) extended this work to consider the (a) 2D flow over a stationary circular cylinder, (b) 2D wake of a transversely
一种新的浸入边界法在模拟水下运动和游泳中的性能
我们报告了一种新的浸入边界方法(IBM)与直接数值模拟(DNS)相结合的基准结果,使用泡沫扩展-3.2表示鱼状游泳的俯俯板。面板又平又薄,它有一个三角形(凸)的后缘,类似于在一些鱼的尾鳍上看到的。通过将四例钝体尾流模拟与已报道的实验和数值研究进行比较,验证了求解器的准确性。例如,平均尾流的结构与用PIV在一个伴随实验中得到的结果比较好。采用适当的正交分解方法,分析了方形薄板和凸薄板在推力产生和推进效率方面的差异,确定了尾缘形状对推力产生和推进效率的影响。通过比较雷诺数为2000和10000时的尾迹,对雷诺数的影响进行了评价。许多生物物种已经进化出高效的游泳推进系统,也表现出高速度和机动性(Sambiley, 1990;Sumich & Morrissey, 2004)。多年来,对水生生物推进机制的理解引起了许多研究人员的关注。这种探索可以为设计具有高机动性和隐蔽性的节能和快速系统提供有价值的信息,这些系统可以匹配甚至可能超过生物物种的性能。在这方面,关注简单的系统通常是有用的,这些系统可以用来研究游泳表现的基本方面。例如,尾鳍的尾缘形状及其方向和运动(即谐波鳍运动)对涡结构的形成、尾流动力学和推力产生的影响在理解鱼状游泳的物理过程中起着主导作用(Van Buren et al., 2016)。Triantafyllou等人(1991)研究了NACA 0012翼型的振荡运动作为鱼游动运动的代表,结果表明,当斯特劳哈尔数St = 0.25 ~ 0.35时,最大推进效率为25%,其中St = fpc/U, fp为振荡频率,c为鳍特征长度,U为游动速度。Buchholz & Smits(2006)对中等雷诺数(Re =Uc/ν)的俯仰刚性矩形板尾迹进行了广泛的研究,结果表明,这种流动主要由马蹄形结构主导。面板的展弦比被确定为影响尾流,从而影响推进性能效率,范围从9%到21%。Green & Smits(2008)研究了俯仰板上的压力分布,结果表明,在俯仰板的大部分上存在的有利的流向压力梯度在后缘附近发生逆转。然而,在确定非定常尾迹中详细的表面压力分布方面存在许多实验挑战,而确定瞬时剪应力分布则更加困难。相比之下,计算流体动力学(CFD)可以用来深入了解应力分布,描述尾流特征,并确定尾流动力学对推力产生的影响。CFD模拟也有助于深入了解尾流结构、它们的形成和相互作用,以及雷诺数的影响。Blondeaux et al.(2005)对俯伏桨叶的数值模拟表明,在Re = 1000时,涡环(链状)结构主导了尾流,这与Green et al.(2011)的实验结果一致。Blondeaux等人(2005)使用了一种基于浸入边界法(IBM)的独特开发的CFD求解器。Jantzen等人(2014)也使用基于ibm的CFD求解器来评估Re = 300时俯仰刚性矩形板的尾迹。本文详细研究了长弦比为2和4的矩形板尾迹中涡的形成过程,发现雷诺数影响前缘涡的形成频率和长度,且长弦比越高,前缘涡越早脱离。由于计算成本较低,IBM通常用于流体流动模拟,作为边界拟合方法的替代方法。foam-extend3.2中的IBM公式使用基于加权最小二乘近似的离散强制方法来施加独立于实际边界的边界条件。这种方法可以捕获边界作为一个尖锐的界面,这消除了涂抹的问题。它还减轻了移动边界周围细胞的畸变,同时减轻了曲线网格转换产生的误差(Lundquist et al., 2009)。参见Iaccarino & Verzicco(2003)和Mittal & Iaccarino(2005)。Jasak等人(2014)将IBM强制方法纳入OpenFOAM,作为foam- extended -3.2的一部分。案例研究包括在固定物体上的流动。特别是,使用k−ε模型的高回流情况表明,极端网格细化缺乏稳定性。
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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