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Vortex visualization of tropical cyclones by Liutex 热带气旋的涡旋可视化
IF 3.5 3区 工程技术 Pub Date : 2025-06-04 DOI: 10.1007/s42241-025-0018-1
Oscar Alvarez, Chenxi Ma, Sim Aberson, Chaoqun Liu

Analysis of the flow field of tropical cyclones in the mature stage by the Liutex methods, such as the Omega Liutex and the Liutex core line, is reported. This is the first known study analyzing tropical cyclones with the Liutex method. Liutex has the potential to enable greater understanding of tropical cyclone dynamics and to improve forecasts of their track, intensity, and structure.

本文报道了利用Omega柳特克斯和柳特克斯核心线等柳特克斯方法对热带气旋成熟期的流场进行分析。这是已知的第一个用柳特克斯方法分析热带气旋的研究。柳特克斯有可能使人们更好地了解热带气旋的动力学,并改进其轨迹、强度和结构的预报。
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引用次数: 0
Vortex dynamics mechanism of the staggered impeller suppressing pressure fluctuations in a double-suction centrifugal pump 双吸离心泵交错叶轮抑制压力波动的涡动力学机理
IF 3.5 3区 工程技术 Pub Date : 2025-06-04 DOI: 10.1007/s42241-025-0017-2
Jin-hao Liu, Dong-sen An, Jian-zhong Zhu, Yi Zhang, Qing-long Zhu, Fu-jun Wang, Chao-yue Wang

The fact that the staggered impeller of a double-suction centrifugal pump can effectively suppress pressure fluctuations has been proved by engineering practice, but the flow mechanism behind it is still not fully understood. In this study, numerical simulations with a proof experiment were conducted, and the vortex dynamics analyses were performed using the newly developed rigid vorticity (Liutex) theory. The following valuable results are obtained: (1) In terms of the intuitive vortex structure, each blade of the impeller induces a trailing vortex rope with a strong rigid vorticity, which gradually evolves inside the volute casing with the rotation of the impeller. The trailing vortex ropes of the symmetric impeller are symmetrically distributed, while those of the staggered impeller present a staggered distribution, and the latter corresponds to a relatively lower rigid vorticity. (2) In terms of the correlation between the vortex and the pressure, the high rigid vorticity zone corresponds to the low-pressure zone. For a fixed point in the volute casing, there is a major “falling-rising” fluctuation in pressure as the symmetric vortex ropes transit it simultaneously, and a minor “falling-rising” fluctuation in pressure as the staggered vortex ropes transit it successively, corresponding to a lower peak-to-peak value of the pressure fluctuations. (3) In terms of the relation between the vortex and the velocity, the vortex ropes induced by the left and right impellers are counter-rotating and develop along the radial direction. This pattern results in high-speed zones at the middle part of the cross-section of the volute casing, both in the streamwise and radial directions, and contributes to velocity fluctuations due to the evolving vortex rope. However, the staggered distribution of vortex ropes can weaken the coupling of vortex pairs, thereby causing lower velocity and pressure pulsations, but can make the main frequency twice that of the symmetric impeller. This study enriches our physical knowledge by revealing the vortex dynamics mechanism of the staggered impeller of a double-suction centrifugal pump to suppress pressure fluctuations.

双吸离心泵交错叶轮能有效抑制压力波动的事实已被工程实践证明,但其背后的流动机理仍未完全了解。本文进行了数值模拟和验证实验,并利用刚建立的刚性涡量理论进行了涡动力学分析。得到了以下有价值的结果:(1)从直观的涡结构上看,叶轮的每个叶片都诱导出一个具有强刚性涡量的尾涡绳,随着叶轮的转动,尾涡绳在蜗壳内逐渐演化。对称叶轮尾涡绳呈对称分布,交错叶轮尾涡绳呈交错分布,后者对应的刚性涡量相对较低。(2)从涡与压力的相关性来看,高刚性涡量区对应于低压区。对于蜗壳内某定点,对称涡绳同时通过时,压力出现较大的“下降-上升”波动,交错涡绳先后通过时,压力出现较小的“下降-上升”波动,对应的压力波动峰间值较小。(3)从涡与速度的关系来看,左右叶轮诱导的涡绳是反向旋转的,沿径向发展。这种模式导致蜗壳横截面的中部出现高速区,无论在流向还是径向上都是如此,并且由于涡绳的演变导致了速度波动。然而,涡旋绳的交错分布会削弱涡旋对的耦合,从而导致较低的速度和压力脉动,但会使主频率是对称叶轮的两倍。本研究通过揭示双吸离心泵交错叶轮抑制压力波动的涡动力学机理,丰富了我们的物理知识。
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引用次数: 0
An insight into the competition in the coupling response of an S-shaped flexible riser subjected to both internal and external flows s型柔性立管在内外流作用下的耦合响应竞争研究
IF 2.5 3区 工程技术 Pub Date : 2025-04-29 DOI: 10.1007/s42241-025-0013-6
Hong-jun Zhu, Kai-rui Deng, Wen-li Liu, Yue Gao

This study experimentally examines the coupling response of an S-shaped flexible riser exposed to internal gas-liquid two-phase flow and external shear current using the optical non-intrusive measurement. The vibration tests were conducted with the internal fluid transported at a constant velocity of vi = 0.9 m/s with three representative gas-liquid ratios (Qg/Ql) and the depth-averaged reduced velocity of external current (Urm) ranging from 9.32 to 23.19. The riser top was hanged underneath an oscillating cylindrical platform. The out-of-plane response is enhanced in the presence of external current, while the in-plane response is suppressed due to the more even distribution of liquid slugs. The response competition among the riser, buoyancy module and platform is quantified in terms of dominant frequencies and interaction lengths, which are sensitive to Qg/Ql, Urm. The shift of zero value among the coupling length, affecting length and affected length indicates the switching of dominant role. In general, the response competition in the in-plane direction is more intense than that in the out-of-plane direction.

采用光学非侵入式测量方法,实验研究了s型柔性隔水管在内部气液两相流和外部剪切流作用下的耦合响应。振动试验条件为:内流体以恒定流速vi = 0.9 m/s, 3种代表性气液比(Qg/Ql),外电流深度平均减速速度(Urm)范围为9.32 ~ 23.19。立管顶部悬挂在一个摆动的圆柱形平台下面。在外部电流的存在下,面外响应增强,而由于液塞分布更均匀,面内响应被抑制。立管、浮力模块和平台之间的响应竞争被量化为主导频率和相互作用长度,它们对Qg/Ql、Urm敏感。零值在耦合长度、影响长度和受影响长度之间的移位表明主导作用的转换。一般情况下,面内方向的响应竞争比面外方向的响应竞争更激烈。
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引用次数: 0
Influence of hydrofoil characteristic thickness on the cavitation erosion risk distribution of clearance vortex cavitation and its mechanisms 水翼特征厚度对间隙涡空化蚀蚀风险分布的影响及其机理
IF 2.5 3区 工程技术 Pub Date : 2025-04-29 DOI: 10.1007/s42241-025-0014-5
Jia-le Huang, Huai-yu Cheng, Yan-tao Cao, Bin Ji

To clarify the influence of the hydrofoil characteristic thickness on the distribution characteristics and mechanisms of clearance cavitation erosion risk, a large eddy simulation (LES) is conducted to study the clearance cavitating flow around NACA0012 and NACA0024 hydrofoils under identical conditions. The study predicts cavitation erosion risk using three methods: The erosive power method (EPM), the improved gray level method (IGLM) and the energy conservation method (ECM). The numerical results are in good agreement with the experiment data and the ECM is applied due to its simplicity in parameter adjustment and low sensitivity. The results indicate that the characteristic thickness significantly influences the flow field, leading to variations in the position and intensity of cavitation collapse, ultimately resulting in notable differences in cavitation erosion risk distribution. The high cavitation erosion risk region on the clearance surface of NACA0012 is concentrated around the midsection, while it is concentrated in the upstream region for the NACA0024, with a lower frequency of extreme events. Tip separation vortex (TSV) cavitation is the main cause of the differences in cavitation erosion risk distribution. On the clearance surface of the NACA0012, TSV cavitation primarily collapses in the central region, whereas for the NACA0024 hydrofoil, TSV cavitation occurs only in the upstream region of the clearance surface and exhibits more stability. The differences in vorticity distribution near the clearance surface partially influence the distribution of TSV cavitation, thereby affecting the characteristics of cavitation erosion risk distribution. The larger characteristic thickness of the NACA0024 reduces the effects of the stretching term and the baroclinic torque term, weakening the effect of vorticity on TSV cavitation, resulting in more stable patterns of the TSV cavitation.

为明确水翼特征厚度对间隙空化侵蚀风险分布特征及机理的影响,采用大涡模拟(LES)研究了相同条件下NACA0012和NACA0024水翼周围的间隙空化流动。研究采用侵蚀功率法(EPM)、改进灰度法(IGLM)和能量守恒法(ECM)三种方法预测空化侵蚀风险。数值计算结果与实验数据吻合较好,该方法具有参数调整简单、灵敏度低的优点。结果表明,特征厚度对流场影响显著,导致空化塌陷的位置和强度发生变化,最终导致空化侵蚀风险分布存在显著差异。NACA0012的空化侵蚀高风险区集中在中段附近,而NACA0024的空化侵蚀高风险区集中在上游区域,极端事件发生频率较低。叶尖分离涡(TSV)空化是造成空化侵蚀风险分布差异的主要原因。在NACA0012的间隙面,TSV空化主要发生在间隙面中部区域,而在NACA0024的水翼中,TSV空化只发生在间隙面上游区域,且表现出更强的稳定性。间隙面附近涡度分布的差异会部分影响TSV空化的分布,从而影响空化侵蚀风险分布的特征。NACA0024较大的特征厚度减小了拉伸项和斜压转矩项的影响,减弱了涡量对TSV空化的影响,使TSV空化模式更加稳定。
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引用次数: 0
A review on the research progress of turbulent drag reduction and gas layer stability on superhydrophobic surfaces 超疏水表面湍流减阻和气层稳定性研究进展综述
IF 2.5 3区 工程技术 Pub Date : 2025-04-29 DOI: 10.1007/s42241-025-0010-9
Jin-hui Yue, Hao-yun Zheng, Xiao-qi Cheng, Hai-ping Tian, Jian-xia Bai, Nan Jiang

Superhydrophobic drag reduction technique has garnered significant attention in recent years due to its outstanding performance in reducing frictional drag, presenting promising application potential in areas such as marine vessels and pipeline transportation. This paper provides a comprehensive review of the wetting theory and slip theory associated with superhydrophobic surfaces, and systematically summarizes the mechanisms of turbulence drag reduction from the perspective of coherent turbulent structures. The research on the combination of superhydrophobic and other drag reduction techniques to improve the drag reduction effect is summarized, focusing on the combined drag reduction of superhydrophobic-riblet. The stability and recoverability of the gas layers on superhydrophobic surfaces are critical for advancing this technology toward practical engineering applications. Consequently, this review places particular emphasis on recent research progress concerning the enhancement and restoration of the underwater gas-liquid interface stability on superhydrophobic surfaces.

近年来,超疏水减阻技术因其在减少摩擦阻力方面的优异性能而备受关注,在船舶、管道运输等领域具有广阔的应用前景。本文全面综述了与超疏水表面相关的润湿理论和滑移理论,并从相干湍流结构的角度系统地总结了湍流减阻机理。综述了超疏水与其他减阻技术相结合以提高减阻效果的研究进展,重点介绍了超疏水-细纹复合减阻技术。超疏水表面气体层的稳定性和可恢复性是将该技术推向实际工程应用的关键。因此,本文重点介绍了近年来关于增强和恢复超疏水表面上水下气液界面稳定性的研究进展。
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引用次数: 0
Numerical simulation of three-dimensional focused waves by new deep water HLGN model 新型深水HLGN模型三维聚焦波的数值模拟
IF 2.5 3区 工程技术 Pub Date : 2025-04-29 DOI: 10.1007/s42241-025-0015-4
Shi-liang Duan, Bin-bin Zhao, Masoud Hayatdavoodi, Kun Zheng

Rogue waves pose a significant threat to the safety of ships and offshore structures, making it crucial to understand their physical mechanisms, such as spatial-temporal focusing, which can lead to their formation. This study investigates three-dimensional focused waves using the newly developed deep-water high-level Green-Naghdi (HLGN) model. Through numerical simulations, we evaluate the selection of the involved wave numbers within the HLGN model and present the algorithm for the three-dimensional implementation. Validation of the model is conducted through numerical reproduction of the three-dimensional focused waves considered in other’s laboratory measurements. The simulated wave profiles and velocity fields are compared with experimental data, demonstrating strong agreement. Discussion is provided about the robustness and accuracy of the HLGN model in simulating three-dimensional focused waves under deep-water conditions.

流氓浪对船舶和海上结构的安全构成重大威胁,因此了解其物理机制至关重要,例如时空聚焦,这可能导致它们的形成。本文利用新开发的深水高水平Green-Naghdi (HLGN)模型研究了三维聚焦波。通过数值模拟,我们评估了HLGN模型中涉及波数的选择,并提出了三维实现的算法。通过对其他实验室测量中考虑的三维聚焦波的数值再现,对模型进行了验证。将模拟的波廓线和速度场与实验数据进行了比较,结果表明两者吻合较好。讨论了HLGN模型在模拟深水条件下三维聚焦波时的鲁棒性和准确性。
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引用次数: 0
Study on the combined vortex characteristics of cavity vortex in the sediment transport pipe of the desilting channel with a swirling flow generator 旋流发生器泥沙通道输沙管道腔涡组合涡特性研究
IF 2.5 3区 工程技术 Pub Date : 2025-04-29 DOI: 10.1007/s42241-025-0011-8
Jun-hu Nan, Hong-ling Hu, Wei Li, Chao Xu, Shang-wu Du

To clarify the internal flow field characteristics of cavity vortex in the sediment transport pipe (STP) of the desilting channel with a swirling flow generator (DCSFG), this study adopted a method combining model test, numerical simulation, and theoretical analysis to investigate flow field characteristics such as water flow regime, cavity morphology, pressure, flow velocity and vorticity, analyze the distribution of combined vortex indexes and radial pressure difference of cavity vortex, and discuss the motion feature differences between the combined vortex in the cavity vortex and the ideal combined vortex. The results show that large eddy simulation (LES) exhibits higher accuracy than the Realizable k -ε model, the distribution of combined vortex n values along typical cross-sections inside the STP ranges from −0.901 to 0.913 radially, indicating quasi-forced vortex motion on the inner side of the vortex area and quasi-free vortex motion on the outer side, the theoretical values of radial pressure difference align well with the simulation results, with a maximum relative error of 15%, confirming that the flow characteristics of the vortex are in accordance with the motion features of combined vortex, the distribution of radial pressure, tangential velocity, and vorticity in the cavity vortex conform to the distribution pattern of ideal combined vortex, whereas significant differences exist in terms of fluid force conditions, structural composition, and generation mechanism. The research findings may provide reference for further analyzing the sediment transport mechanism in the cavity vortex and for the practical engineering design and application of the DCSFG.

为明确带旋流发生器(DCSFG)的排沙通道输沙管道(STP)内腔涡内部流场特征,本研究采用模型试验、数值模拟和理论分析相结合的方法,研究了水流型、腔形态、压力、流速和涡量等流场特征,分析了组合涡指数的分布和腔涡径向压差。并讨论了空腔涡中组合涡与理想组合涡的运动特征差异。结果表明:大涡模拟(LES)比Realizable k -ε模型具有更高的精度,STP内典型截面上的组合涡n值沿径向分布范围为- 0.901 ~ 0.913,表明涡区内侧为准强迫涡运动,外侧为准自由涡运动,径向压差理论值与模拟结果吻合较好,最大相对误差为15%;空腔涡的径向压力、切向速度和涡量分布符合理想组合涡的分布规律,证实了涡流的流动特性与组合涡的运动特性一致,但在流体受力条件、结构组成、产生机理等方面存在显著差异。研究结果可为进一步分析空腔涡输沙机理以及DCSFG的实际工程设计和应用提供参考。
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引用次数: 0
Effect of impeller front shroud perforation on gas-liquid two phase flow performance of the multistage side channel pump 叶轮前叶冠穿孔对多级侧流道泵气液两相流动性能的影响
IF 2.5 3区 工程技术 Pub Date : 2025-04-29 DOI: 10.1007/s42241-025-0012-7
Fan Wu, Fan Zhang, Shou-qi Yuan, Ke Chen, Qiu-hong Hong

To enhance the gas-liquid mixed transport performance of the first-stage centrifugal impeller of the multistage side-channel pump, a diagonal perforation oriented towards the exit is fabricated in the front shroud of the impeller. Based on the Euler-Euler non-homogeneous model and the SST k -ω turbulence model, the gas-liquid two-phase unsteady numerical simulation of the internal flow under various inlet gas volume fraction (IGVF) is conducted, the reliability of the simulation is verified through comparison with experiments. The results indicate that under the circumstances of high flowrate and high IGVF, the perforation design of the front shroud can increase the head of the centrifugal impeller by 4%–7% while the efficiency is slightly decreased under gas-liquid two phase flow. According to the internal flow analysis and Liutex vortex identification, the high-pressure and high-speed fluid in the front pump chamber is introduced into the impeller through the front shroud perforation, smashing and dispersing the originally aggregated bubble groups in the flow channel, causing the average pressure in the impeller to rise after the perforation, increasing the number and intensity of vortexes, significantly reducing the number and the accumulation area of bubbles, greatly reducing the air volume fraction of the impeller. The bubble blockage phenomenon in the flow channel is observably improved, and the gas-liquid mixed transport capacity of the centrifugal impeller is significantly enhanced, providing a theoretical basis for the optimization design of the gas-liquid two-phase flow of vane pumps.

为了提高多级侧流道泵第一级离心叶轮的气液混合输送性能,在叶轮前叶冠处制造了一个面向出口的斜孔。基于Euler-Euler非均匀模型和SST k -ω湍流模型,对不同进口气体体积分数(IGVF)下的气液两相非定常内部流动进行了数值模拟,通过与实验对比验证了模拟的可靠性。结果表明:在大流量、高IGVF条件下,前叶冠的穿孔设计可使离心叶轮扬程提高4% ~ 7%,而在气液两相流条件下,效率略有下降。根据内部流动分析和Liutex涡识别,前泵腔内的高压高速流体通过前叶冠穿孔引入叶轮,将流道内原本聚集的泡群粉碎分散,使穿孔后叶轮内的平均压力升高,旋涡数量和强度增加,气泡数量和积聚面积显著减少;大大降低了叶轮的风量分数。流道内气泡堵塞现象明显改善,离心叶轮气液混合输送能力显著增强,为叶片泵气液两相流的优化设计提供了理论依据。
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引用次数: 0
A novel hull form optimization framework based on multi-fidelity deep neural network 一种基于多保真度深度神经网络的船体形状优化框架
IF 2.5 3区 工程技术 Pub Date : 2025-04-17 DOI: 10.1007/s42241-025-0007-4
Ya-bo Wei, Guo-hua Pan, Passakorn Paladaechanan, De-cheng Wan

With the advancements in computer technology, the simulation-based design (SBD) technology has emerged as a highly effective method for hull form optimization. The SBD approach often employs various methods to evaluate the hydrodynamic performance of the sample ships. Although the surrogate model is applied to SBD method to replace time-consuming evaluation, many high-fidelity data are typically required to guarantee the accuracy of the surrogate model, resulting in significant computational costs. To improve the optimization efficiency and reduce computational burdens, we propose a novel hull form optimization framework utilizing the multi-fidelity deep neural network (MFDNN), leveraging multi-source data fusion and transfer learning. This framework constructs an accurate multi-fidelity surrogate model which correlates design parameters with hydrodynamic performance of the hull by blending data with different fidelity. Besides, computational fluid dynamics (CFD) evaluations based on viscous flow are served as the high-fidelity model, while potential-theory evaluations represent the low-fidelity model. Then, this framework is validated using mathematical functions to prove its practicability in optimization. Finally, the optimization design of the resistance of the DTMB-5415 ship is carried out. Our findings demonstrate that this framework can take into account both efficiency and accuracy, which is preferable in optimization tasks. The optimized hull form obtained by the framework has better resistance performance.

随着计算机技术的进步,基于仿真的船体设计(SBD)技术已成为一种高效的船体形状优化方法。SBD方法通常采用各种方法来评估样品船的水动力性能。虽然将代理模型应用于SBD方法来代替耗时的评估,但通常需要大量高保真度的数据来保证代理模型的准确性,导致计算成本很高。为了提高优化效率和减少计算量,我们提出了一种利用多保真度深度神经网络(MFDNN),利用多源数据融合和迁移学习的新型船体形状优化框架。该框架通过混合不同保真度的数据,构建了精确的多保真度替代模型,将设计参数与船体水动力性能联系起来。其中,基于粘性流动的计算流体力学(CFD)评价为高保真模型,而势理论评价为低保真模型。然后,利用数学函数对该框架进行了验证,证明了其在优化中的实用性。最后,对DTMB-5415型舰船进行了阻力优化设计。我们的研究结果表明,该框架可以兼顾效率和准确性,这是优选的优化任务。经框架优化后的船体外形具有较好的抗阻性能。
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引用次数: 0
Research on the tongue-induced vortex in the semi-spiral suction chamber and its influence on cavitation 半螺旋吸力室内舌形涡及其对空化的影响研究
IF 2.5 3区 工程技术 Pub Date : 2025-04-17 DOI: 10.1007/s42241-025-0008-3
Yu-xin Du, Jia-mei Ma, Shi-jie Zhang, Hong-zhong Lu, Chao-yue Wang, Zhi-feng Yao

This paper aims to elucidate the vortex evolution characteristics generated by the tongue of the semi-spiral suction chamber and its influence on the cavitation of the pump. Based on the turbulent viscosity correction model, the internal flow of a centrifugal pump with a specific speed of 160 was simulated, and experimental data verified the simulation. This study focuses on analyzing the conditions of large flow rate, high-efficiency, and partial flow rate. The results show that the tongue will induce a tongue-induced vortex. The tongue-induced vortex extends from the tongue region to the impeller region, and its shape is curved and slender. The shape and volume of the tongue-induced vortex are related to the flow rate. The vortex’s shape is blurred and small in the partial flow rate. There is a complete and obvious curved slender vortex in the high-efficiency zone. In large flow conditions, the vortex’s shape is consistent with the high-efficiency zone and the volume is larger. The vortex’s strength is positively correlated with the circulation of the inlet, which is in the suction chamber. The tongue-induced vortex affects the distribution position of the low-pressure zone on the blade, thereby promoting the leading edge cavitation.

本文旨在阐明半螺旋吸入腔舌部产生的涡演化特征及其对泵空化的影响。基于紊流粘度校正模型,对比转速为160的离心泵内部流动进行了仿真,实验数据验证了仿真结果。本研究重点分析了大流量、高效率和部分流量的条件。结果表明,舌面会产生舌形涡。舌形涡由舌形区向叶轮区延伸,形状呈弯曲细长型。舌形涡的形状和体积与流量有关。在偏流量下,涡的形状模糊且较小。高效区内有一个完整而明显的弯曲细长涡。在大流量条件下,涡的形状与高效区一致,体积较大。涡的强度与入口的循环正相关,入口在吸力室中。舌形涡影响叶片低压区的分布位置,从而促进前缘空化。
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引用次数: 0
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Journal of Hydrodynamics
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