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Air bubble breakup in shear water flows generated by a plug conduit: An experimental investigation 塞式导管产生的剪切水流中的气泡破裂:实验研究
IF 2.5 3区 工程技术 Pub Date : 2024-01-11 DOI: 10.1007/s42241-024-0079-6
Han Wu, Mao-lin Zhou, Wei-lin Xu, Wang-ru Wei, Jian-bo Li

In the context of a sudden contraction plug conduit, the near-wall area experiences a significant shearing effect of water flow, however, the extent to which this shearing effect occurs in bubble-water flow and the related variation mechanisms of air bubble size and number remain unclear. This study employs a model test method to investigate the diffusion process of bubble-water flow in a sudden contraction plug conduit. The size and number of bubbles, as well as their distribution along the shearing section under varying initial air volume conditions, are studied in detail using a high-speed image acquisition system. The experimental findings reveal a self-similar relationship between the number and size of bubbles and their cross-sectional distribution over time. The bubble number and size vary in three stages, i.e., quasi-suspension, shearing, and shearing completion stages. The direction perpendicular to the conduit exhibits peak values in bubble number distribution over the three stages, with peak value location varying with the near-wall area. As time progresses, the peak value increases, and a larger initial air volume corresponds to a smaller distance of the peak value location from the wall. The size of air bubbles near the wall is consistent with the minimum diameter of air bubbles in shear flow and is hardly affected by the initial air volume. These results aid in comprehending the change law of two-phase water and air flow under a strong shearing effect in the plug conduit, and provide useful insights for hydraulic design in fluid engineering.

在突发性收缩塞导管中,近壁区域会受到水流的明显剪切作用,但这种剪切作用在气泡-水流中的发生程度以及气泡大小和数量的相关变化机制仍不清楚。本研究采用模型试验方法来研究骤缩塞导管中气泡-水流的扩散过程。利用高速图像采集系统详细研究了不同初始空气量条件下气泡的大小、数量及其沿剪切段的分布情况。实验结果表明,气泡的数量和大小与其横截面分布之间随着时间的推移存在自相似关系。气泡的数量和大小在三个阶段发生变化,即准悬浮阶段、剪切阶段和剪切完成阶段。在这三个阶段中,垂直于导管方向的气泡数量分布呈现峰值,峰值位置随近壁面积的变化而变化。随着时间的推移,峰值逐渐增大,初始空气量越大,峰值位置与管壁的距离就越小。靠近壁面的气泡大小与剪切流中气泡的最小直径一致,几乎不受初始空气量的影响。这些结果有助于理解塞子导管中强剪切效应下水气两相流的变化规律,并为流体工程中的水力设计提供了有益的启示。
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引用次数: 0
An experimental study on the impact behavior of cavitation inside tip clearance of a hydrofoil 水翼顶端间隙内气蚀冲击行为的实验研究
IF 2.5 3区 工程技术 Pub Date : 2024-01-11 DOI: 10.1007/s42241-024-0078-7
Yan-tao Cao, Liang-hao Xu, Xiao-xing Peng

Tip clearance cavitation is one of the most common cavitation phenomena exist on duct propellers, pumps and some hydraulic turbines, which may lead to erosion of the components. Due to the influence of the nearby wall, cavitation inside the tip clearance is more complicated than other cases without interaction. So far, the understanding about the impact mechanism of tip clearance cavitation is still limited. In this paper, to obtain the impact behavior of tip clearance cavitation, a high-speed camera was used to capture the cavitation behavior inside the tip clearance of a hydrofoil, and surface paint coating peeling method was applied to show the impact region. Results indicated that cavitation around the tip of the hydrofoil was composed of a tip separation cavity and a tip leakage vortex cavity, and the one with contribution to impact was the tip separation cavity. Through the comprehensive analysis of the paint peeling region and dynamic behavior of tip separation cavity, the impact was found to be related to the local collapse and rebound of the cloud cavitation shed from the attached part. In addition, the influence of tip clearance size on the behavior of tip clearance cavitation was also investigated. As the tip clearance size increased, the tip separation cavity tended to transfer from sheet cavitation to vortex cavitation. These findings can provide a sound basis for evaluating the erosion risk arising from the tip clearance cavitation.

摘要 尖端间隙气蚀是管道推进器、泵和某些水轮机上最常见的气蚀现象之一,可能导致部件的侵蚀。由于受到附近壁面的影响,叶尖间隙内的空化比其他无相互作用的情况更为复杂。到目前为止,人们对叶尖间隙空化的影响机理的了解还很有限。本文利用高速摄像机捕捉水翼顶端间隙内的空化行为,并采用表面油漆涂层剥离法显示冲击区域,以获得顶端间隙空化的冲击行为。结果表明,水翼顶端周围的空化由顶端分离腔和顶端泄漏涡流腔组成,其中对冲击有贡献的是顶端分离腔。通过对油漆剥落区域和顶端分离腔的动态行为进行综合分析,发现冲击与附着部分脱落的云气蚀的局部塌陷和反弹有关。此外,还研究了尖端间隙大小对尖端间隙空化行为的影响。随着针尖间隙尺寸的增大,针尖分离空化趋向于从片状空化转移到涡状空化。这些发现为评估尖端间隙空化所产生的侵蚀风险提供了可靠的依据。
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引用次数: 0
Numerical analysis of turbulent fluctuations around an axisymmetric body of revolution based on wall-modeled large eddy simulations 基于壁模型大涡流模拟的轴对称旋转体周围湍流波动数值分析
IF 2.5 3区 工程技术 Pub Date : 2024-01-11 DOI: 10.1007/s42241-024-0077-8
Kang-jian He, Fu-chang Zhou, Wei-wen Zhao, Jian-hua Wang, De-cheng Wan

Wall-modeled large eddy simulation (WMLES) is used to investigate turbulent fluctuations around an axisymmetric body of revolution. This study focuses on evaluating the ability of WMLES to predict the fluctuating flow over the axisymmetric hull and analyzing the evolution of turbulent fluctuations around the body. The geometry is the DARPA SUBOFF bare model and the Reynolds number is 1.2×107, based on the free-stream velocity and the length of the body. Near-wall flow structures and complex turbulent fluctuation fields are successfully captured. Time-averaged flow quantities, such as time-averaged pressure and skin-friction coefficients, and time-averaged velocity profiles on the stern, achieved great agreements between WMLES results and experimental data. Self-similarity of time-averaged velocity defects within a self-similar coordinate up to twelve diameters from the tail. A comprehensive analysis of second-order statistics in the mid-body, stern, and wake regions is condutced. Numerical results agree well with experimental data and previous wall-resolved large eddy simulation (WRLES) results about root mean square (rms) of radial and axial fluctuating velocities at the stern. Turbulent fluctuations including turbulent kinetic energy (TKE) and second-order velocity statistics are identified as dual peak behavior and non-self-similar over the wake length, consistent with previous findings in the literature. This assessment enhances the understanding of WMLES capabilities in capturing complex fluctuating flow around axisymmetric geometries.

壁模型大涡模拟(WMLES)用于研究轴对称旋转体周围的湍流波动。本研究的重点是评估 WMLES 预测轴对称船体上波动流的能力,并分析船体周围湍流波动的演变。几何模型为 DARPA SUBOFF 裸模型,雷诺数为 1.2×107,基于自由流速度和体长度。成功捕获了近壁流动结构和复杂的湍流波动场。时间平均流动量,如时间平均压力和表皮摩擦系数,以及船尾的时间平均速度剖面,在 WMLES 结果和实验数据之间取得了很好的一致性。在距离尾部 12 个直径的自相似坐标内,时间平均速度缺陷具有自相似性。对船体中部、船尾和尾流区域的二阶统计进行了全面分析。数值结果与实验数据和之前的壁面分辨大涡流模拟(WRLES)结果非常吻合,即船尾径向和轴向波动速度的均方根(rms)。包括湍流动能(TKE)和二阶速度统计在内的湍流波动被确定为双峰行为,并且在整个尾流长度上是非自相似的,这与之前文献中的发现是一致的。这项评估加深了人们对 WMLES 捕捉轴对称几何结构周围复杂波动流的能力的理解。
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引用次数: 0
Investigations of the dynamical behaviors of a millimeter-scale cavitation bubble near the rigid wall 对刚性壁附近毫米级空化气泡动力学行为的研究
IF 2.5 3区 工程技术 Pub Date : 2023-12-28 DOI: 10.1007/s42241-023-0075-2
Dan Zi, Dong-qiao He, Zhi-feng Yao, Fu-jun Wang, Qiang Zhong, Pin Lyu

The collapse of the cavitation bubble near the rigid wall emits shock waves and creates micro-jet, causing cavitation damage and operation instability of the hydraulic machinery. In this paper, the millimeter-scale bubble near the rigid wall was investigated experimentally and numerically with the help of a laser photogrammetry system with nanosecond-micron space-time resolution and the open source package OpenFOAM-2212. The morphological characteristics of the bubble during its growth phase, collapse phase and rebound phase were observed by experiment and numerical simulation, and characteristics of the accompanying phenomena including the shock wave propagation and micro-jet evolution were well elucidated. The numerical results agree well with the experimental data. The bubble starts from a tiny small size with high internal pressure and expands into a sphere with a radius of 1.07 mm for γ = d / Rmax = 1.78. The bubble collapses into a heart shape and moves towards to the rigid wall during its collapse phase, resulting in a higher pressure load for the rigid wall in the second collapse. The maximum pressure of the shock wave of the first bubble collapse phase reaches 5.4 MPa, and the velocity of the micro-jet reaches approximately 100 m/s. This study enriches the existing experimental and numerical results of the dynamics of the near-wall cavitation bubble.

刚性壁附近空化气泡的坍塌会产生冲击波并形成微射流,造成空化破坏和液压机械的运行不稳定。本文利用纳秒微米级时空分辨率的激光照排系统和开源软件包 OpenFOAM-2212 对刚性壁附近的毫米级气泡进行了实验和数值研究。通过实验和数值模拟观察了气泡在生长阶段、塌陷阶段和反弹阶段的形态特征,并很好地阐明了伴随现象的特征,包括冲击波传播和微射流演化。数值结果与实验数据非常吻合。当 γ = d/Rmax = 1.78 时,气泡从很小的尺寸开始膨胀,内部压力很高,膨胀成半径为 1.07 毫米的球体。气泡坍缩成心形,并在坍缩阶段向刚性壁移动,导致刚性壁在第二次坍缩时承受更大的压力负荷。第一个气泡坍塌阶段冲击波的最大压力达到 5.4 兆帕,微射流的速度约为 100 米/秒。这项研究丰富了现有的近壁空化气泡动力学实验和数值结果。
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引用次数: 0
Laser-induced cavitation bubble near boundaries 激光诱导的边界附近空化气泡
IF 2.5 3区 工程技术 Pub Date : 2023-12-12 DOI: 10.1007/s42241-023-0074-3
Jia-xin Yu, Xiao-yu Wang, Jin-sen Hu, Jun-wei Shen, Xiang-qing Zhang, Xiao-xiao Zheng, Yu-ning Zhang, Zhi-feng Yao

Laser-induced cavitation bubble has been widely used to investigate the mechanisms of hydraulic machinery cavitation erosion and to explore applications in atomization, alloy strengthening, ultrasonic chemistry, biomedicine, surface cleaning and materials processing. This paper consolidates existing research findings on the cavitation bubble dynamics near different boundaries and provides insights for future research work. Firstly, the dynamics of a single cavitation bubble in an infinite field is presented. Subsequently, the focus shifts to the dynamics of cavitation bubble near a rigid wall, angular walls, particles and hydrofoil. Lastly, the paper delves into the dynamics of cavitation bubble within a droplet, revealing the microscopic mechanism of droplet breakup induced by cavitation bubble.

摘要 激光诱导空化泡已被广泛用于研究液压机械空化侵蚀的机理,并探索其在雾化、合金强化、超声化学、生物医学、表面清洁和材料加工等方面的应用。本文综合了现有关于不同边界附近空化泡动力学的研究成果,为今后的研究工作提供了启示。首先,介绍了无限场中单个空化泡的动力学。随后,重点转向刚性壁、角壁、颗粒和水翼附近的空化泡动力学。最后,论文深入研究了液滴内空化泡的动力学,揭示了空化泡诱发液滴破裂的微观机制。
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引用次数: 0
Recent progress on the jetting of single deformed cavitation bubbles near boundaries 边界附近单个变形空化气泡喷射的最新进展
IF 2.5 3区 工程技术 Pub Date : 2023-12-12 DOI: 10.1007/s42241-023-0071-6
Jing-zhu Wang, Guang-hang Wang, Qing-yun Zeng, Yi-wei Wang

Cavitation occurs widely in nature and engineering and is a complex problem with multiscale features in both time and space due to its associating violent oscillations. To understand the important but complicated phenomena and fluid mechanics behind cavitation, a great deal of effort has been invested in investigating the collapse of a single bubble near different boundaries. This review aims to cover recent developments in the collapse of single bubbles in the vicinity of complex boundaries, including single boundaries and two parallel boundaries, and open questions for future research are discussed. Microjets are the most prominent features of the non-spherical collapse of cavitation bubbles near boundaries and are directed toward rigid walls and away from free surfaces. Such a bubble generally splits, resulting in the formation of two axial jets directed opposite to each other under the constraints of an elastic boundary or two parallel boundaries. The liquid jet penetrates the bubble, impacts the boundary, and exerts a great deal of stress on any nearby boundary. This phenomenon can cause damage, such as the erosion of blades in hydraulic machinery, the rupture of human blood vessels, and underwater explosions, but can also be exploited for applications, such as needle-free injection, drug and gene delivery, surface cleaning, and printing. Many fascinating developments related to these topics are presented and summarized in this review. Finally, three directions are proposed that seem particularly fruitful for future research on the interaction of cavitation bubbles and boundaries.

空化现象广泛存在于自然界和工程领域,由于其伴随的剧烈振荡,它是一个在时间和空间上都具有多尺度特征的复杂问题。为了理解空化背后重要而复杂的现象和流体力学,人们投入了大量精力研究不同边界附近单个气泡的坍塌。本综述旨在介绍复杂边界(包括单一边界和两个平行边界)附近单个气泡坍缩的最新研究进展,并讨论未来研究的开放性问题。微射流是空化气泡在边界附近非球形塌陷的最显著特征,它朝向刚性壁,远离自由表面。这种气泡一般会分裂,在弹性边界或两个平行边界的限制下形成两个方向相反的轴向射流。液体射流穿透气泡,冲击边界,并对附近的任何边界施加很大的应力。这种现象会造成损害,如液压机械叶片的侵蚀、人体血管的破裂和水下爆炸,但也可用于各种应用,如无针注射、药物和基因输送、表面清洁和打印。本综述介绍并总结了与这些主题相关的许多引人入胜的发展。最后,本文提出了三个方向,这三个方向似乎是空化气泡与边界相互作用未来研究的主要方向。
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引用次数: 0
A numerical study of hydrodynamic characteristics and hydrological processes in the coastal wetlands during extreme events 极端事件期间沿海湿地水动力特征和水文过程的数值研究
IF 2.5 3区 工程技术 Pub Date : 2023-12-12 DOI: 10.1007/s42241-023-0072-5
Ming-liang Zhang, Xiao-sen Zhu, Yu-jia Wang, Heng-zhi Jiang, Lei Cui

Providing accurate predictions of extreme water levels through numerical simulation has become essential for disaster prevention and damage mitigation in coastal wetland areas. This study applies the FVCOM model to simulate storm surges caused by several typhoons in the Bohai Sea and the North Huanghai Sea. The vegetation drag force caused by salt marsh plants is inserted into the FVCOM model for model improvement with vegetation effect by integrating RS and GIS technologies. A parametric typhoon model is coupled with background wind fields derived to acquire the spatio-temporal variations of wind and pressure fields in the computational domain. The simulation results reproduce the extreme storm surges induced by typhoon events very well. The modeling results are compared by validating with literature results to examine the effect of vegetation on tidal waves in tidal mud flats. Moreover, the coupled model is also applied to explore storm surge attenuation and land intrusion during Typhoon Winnie in the wetlands of the Liao River Estuary. The simulation results indicate that salt marsh plants can reduce the flow current with little impact on tide flooding/ebbing in vegetated regions. Furthermore, the results show that typhoon presence increases the inundation depth and extendes the flood time in the tidal wetlands of the study region. The FVCOM model incorporating the method with vegetation drag force can provide new insights to understand the comprehensive impact of tidal wetland plants on hydrodynamic characteristics in the Bohai Sea and other waters, hence presents a more accurate quantification of the hydrological process of storm surge in the tidal wetlands.

通过数值模拟对极端水位进行准确预测对于沿海湿地地区的防灾减灾工作至关重要。本研究应用 FVCOM 模型模拟了渤海和黄海北部多个台风引起的风暴潮。在 FVCOM 模型中加入了盐沼植物引起的植被阻力,通过集成 RS 和 GIS 技术,利用植被效应对模型进行改进。台风参数模型与背景风场耦合,获取计算域内风场和气压场的时空变化。模拟结果很好地再现了台风事件引发的极端风暴潮。模拟结果与文献结果进行了对比验证,以研究植被对滩涂潮汐波的影响。此外,该耦合模型还被用于探讨台风 "温妮 "期间辽河口湿地的风暴潮衰减和陆地入侵问题。模拟结果表明,在植被覆盖的区域,盐沼植物可以减弱水流,而对潮水淹没/侵蚀的影响很小。此外,模拟结果表明,台风的存在增加了研究区域潮汐湿地的淹没深度,延长了淹没时间。结合植被阻力法的 FVCOM 模型可为了解渤海及其他水域潮汐湿地植物对水动力特性的综合影响提供新的见解,从而更准确地量化潮汐湿地风暴潮的水文过程。
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引用次数: 0
Entropy production by dissipation effects and characteristic vortex evolution in a rocket turbopump 火箭涡轮泵中耗散效应产生的熵和特征涡流演变
IF 2.5 3区 工程技术 Pub Date : 2023-12-12 DOI: 10.1007/s42241-023-0073-4
De-you Li, Jia-qi Zhu, Rui-yi Zhang, Yi Zhang, Zhi-peng Li, Hong-jie Wang, Zhi-peng Ren

The relationship between entropy production and vortex evolution affects the efficiency and stability of rotating machinery. This study investigated the energy characteristics of a rocket turbopump and revealed the correlated mechanisms of the entropy production rate using the dissipation effects and characteristic vortex evolution. For the first time, direct and turbulent dissipation and rigid and shear vorticity decomposition methods were utilized to analyze the correlation between flow loss and characteristic vorticities in rotating machinery. With an increase in the flow rate, the hydraulic losses of the dissipation effects and wall decreased by 60% and 38.3%, respectively, and the proportions of the input energy decreased (from 13% to 8%) and remained stable (8%), respectively. The local direct dissipative entropy production (DDEP) in the inducer-impeller is strongly related to shear entropy, and the correlated effect of total enstrophy on DDEP is weaker than that of shear vorticity, indicating that rigid enstrophy suppresses direct dissipation. The correlation between turbulent dissipation and rigid enstrophy was significantly weaker in the static flow passage of the turbopump owing to the weak rigid rotational effect. The correlation between the rigid entropy and local turbulent dissipative entropy production (TDEP) gradually increased with increasing flow rate, reaching a medium correlation (the maximal correlated degree in the turbopump) and exhibiting rigid rotation effects on the hydraulic loss. Moreover, the flow rate significantly affected the correlation (except for the diffuser), and the two characteristic vorticities reached a maximum at the designed flow rate owing to optimal efficiency and minimum hydraulic loss.

熵产生和涡流演变之间的关系影响着旋转机械的效率和稳定性。本研究对火箭涡轮泵的能量特性进行了研究,并利用耗散效应和特征涡旋演化揭示了熵产生率的相关机制。研究首次利用直接耗散和湍流耗散以及刚性和剪切涡度分解方法分析了旋转机械中流动损失与特征涡度之间的相关性。随着流速的增加,耗散效应和壁面的水力损失分别降低了 60% 和 38.3%,输入能量的比例分别降低(从 13% 降至 8% )和保持稳定(8%)。诱导器-叶轮中的局部直接耗散熵产生(DDEP)与剪切熵密切相关,总熵对 DDEP 的相关影响弱于剪切涡度,表明刚性熵抑制了直接耗散。在涡轮泵的静态流道中,由于刚性旋转效应较弱,湍流耗散与刚性熵之间的相关性明显减弱。刚性熵与局部湍流耗散熵(TDEP)之间的相关性随着流速的增加而逐渐增大,达到中等相关性(涡轮泵中的最大相关性),并表现出刚性旋转对水力损失的影响。此外,流量对相关性有明显影响(扩散器除外),并且由于效率最优和水力损失最小,两个特征涡度在设计流量下达到最大。
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引用次数: 0
Experimental study of the dynamics of a single cavitation bubble excited by a focused laser near the boundary of a rigid wall 刚性壁面边界附近聚焦激光激发单个空化气泡动力学的实验研究
IF 2.5 3区 工程技术 Pub Date : 2023-11-30 DOI: 10.1007/s42241-023-0069-0
Xiang-qing Zhang, Xiao-fei Zhang, Xu Qiu, Dan Gao, Yu-ning Zhang

Based on high-speed photographic experiments, this study presents a detailed qualitative and quantitative analysis of the dynamics of a single cavitation bubble near the boundary of a rigid wall in asymmetric settings. The main findings are reported as follows: (1) The non-sphericity of the bubble interface decreases with increasing spacing between the bubble and the boundary, and the asymmetry of the bubble becomes more significant with increasing asymmetry angle. (2) The motion mode of the bubble cluster in the second oscillation cycle can be divided into two typical modes depending on the direction of movement. (3) The angle between the oblique jet pointing towards the upper wall surface and the horizontal direction in the second oscillation cycle decreases as the dimensionless spacing decreases.

基于高速摄影实验,本文对非对称条件下刚性壁面边界附近单个空化气泡的动力学进行了详细的定性和定量分析。主要研究结果如下:(1)气泡界面的非球性随气泡与边界间距的增大而减小,而气泡的不对称性随不对称角的增大而增强。(2)气泡团在第二个振荡周期的运动模式根据运动方向可分为两种典型模式。(3)在第二振荡周期中,指向上壁面的斜射流与水平方向的夹角随着无量纲间距的减小而减小。
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引用次数: 0
Numerical study on the aerodynamic and hydrodynamic performances of an ultra-high-speed AAMV 超高速AAMV气动与水动力性能数值研究
IF 2.5 3区 工程技术 Pub Date : 2023-11-30 DOI: 10.1007/s42241-023-0070-7
Qi-jun Ni, Shi-jun Ji, Yi Jiang, Sheng-zhong Li, Yang Liu, Wei-tong Xu

In order to investigate the resistance performance of an ultra-high-speed aerodynamically alleviated marine vehicle (AAMV), finite volume method (FVM)-based computational fluid dynamics (CFD) software STAR CCM+ is used to simulate the forward motion of this vehicle. The calculated results are validated as they reach good agreement with experimental data. Comparing the motions of models with and without aero-wings, the hybrid aerodynamic and hydrodynamic mechanism of this novel hull is discussed. Study is subsequently performed that how step configuration, spray rail and deadrise angle act on hull behavior and resistance. The results show that models with double steps and spray rail possess better resistance characteristics at high speeds, and planing surface with variable deadrise angle could further improve the overall navigation performance.

为了研究超高速空气动力学缓和船舶(AAMV)的阻力性能,采用基于有限体积法(FVM)的计算流体动力学(CFD)软件STAR CCM+对该船舶的正向运动进行了模拟。计算结果与实验数据吻合较好,得到了验证。比较了带翼和不带翼模型的运动,讨论了这种新型船体的气动和水动力混合机理。随后,研究了阶梯结构、喷淋导轨和死升角对船体性能和阻力的影响。结果表明,采用双台阶和喷雾导轨的模型在高速下具有更好的阻力特性,采用可变死升角的平面可以进一步提高整体导航性能。
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引用次数: 0
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Journal of Hydrodynamics
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