Pub Date : 2026-01-15DOI: 10.1016/j.jfluidstructs.2026.104514
Shuai Huang , Qingshan Yang , Zhanfang Liu , Haohong Li , Wenshan Shan , Chen Li
Tall slender structures are prone to aeroelastic instability, such as vortex resonance and galloping, in which the along-wind response is often neglected in conventional analyses. Recent experimental studies, however, have shown that near the wind speed corresponding to across-wind resonance, the along-wind vibration becomes coupled with the across-wind vibration, resulting in a significant amplification of the along-wind response and a reduction of the across-wind response. The underlying nonlinear self-excited forces driving this coupled behavior remain insufficiently understood. This study proposes a method for identifying the self-excited forces of tall slender structures accounting for along- and across-wind coupling. Displacement responses in both directions were measured through wind tunnel tests using a pivot model, followed by complex modal parameter identification. It was found that the mode with a frequency close to the across-wind natural frequency predominantly governs the structural response. A mathematical model was then established to predict coupled vibrations and to identify nonlinear self-excited forces. A generalized Van der Pol-type damping model was employed to capture the amplitude dependence of the first-mode damping ratio. Finally, the prediction model and the self-excited force identification method were validated against experimental results. The proposed approach provides a theoretical framework for analyzing aeroelastic instability of tall slender structures with along- and across-wind coupling effects.
细长高架结构容易发生涡共振和驰动等气动弹性失稳,而在这些失稳中,沿风响应在传统分析中往往被忽略。然而,最近的实验研究表明,在横风共振对应的风速附近,顺风振动与横风振动耦合,导致顺风响应明显放大,横风响应减弱。驱动这种耦合行为的潜在非线性自激力仍然没有得到充分的了解。本文提出了一种考虑顺风和横风耦合的高细长结构自激力识别方法。采用主轴模型进行风洞试验,测量了两个方向的位移响应,然后进行了复杂模态参数辨识。研究发现,接近横风固有频率的模态主导结构响应。然后建立数学模型来预测耦合振动和识别非线性自激力。采用广义Van der pol型阻尼模型来捕捉第一模态阻尼比的幅值依赖性。最后,根据实验结果对预测模型和自激力识别方法进行了验证。该方法为分析具有顺风和横风耦合效应的高细长结构的气动弹性失稳提供了理论框架。
{"title":"Mathematical modeling of nonlinear coupled along- and across-wind aeroelastic responses in tall slender structures with square section","authors":"Shuai Huang , Qingshan Yang , Zhanfang Liu , Haohong Li , Wenshan Shan , Chen Li","doi":"10.1016/j.jfluidstructs.2026.104514","DOIUrl":"10.1016/j.jfluidstructs.2026.104514","url":null,"abstract":"<div><div>Tall slender structures are prone to aeroelastic instability, such as vortex resonance and galloping, in which the along-wind response is often neglected in conventional analyses. Recent experimental studies, however, have shown that near the wind speed corresponding to across-wind resonance, the along-wind vibration becomes coupled with the across-wind vibration, resulting in a significant amplification of the along-wind response and a reduction of the across-wind response. The underlying nonlinear self-excited forces driving this coupled behavior remain insufficiently understood. This study proposes a method for identifying the self-excited forces of tall slender structures accounting for along- and across-wind coupling. Displacement responses in both directions were measured through wind tunnel tests using a pivot model, followed by complex modal parameter identification. It was found that the mode with a frequency close to the across-wind natural frequency predominantly governs the structural response. A mathematical model was then established to predict coupled vibrations and to identify nonlinear self-excited forces. A generalized Van der Pol-type damping model was employed to capture the amplitude dependence of the first-mode damping ratio. Finally, the prediction model and the self-excited force identification method were validated against experimental results. The proposed approach provides a theoretical framework for analyzing aeroelastic instability of tall slender structures with along- and across-wind coupling effects.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104514"},"PeriodicalIF":3.5,"publicationDate":"2026-01-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145980246","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-13DOI: 10.1016/j.jfluidstructs.2025.104497
James L. Fields , Anshul Suri , Caleb J. Barnes , Jack J. McNamara , Datta V. Gaitonde
This paper investigates the interplay between the Kelvin-Helmholtz (K-H) instability, aeroelastic flutter, and laminar shock-boundary layer interactions. The coupled system is studied by performing modal-based analyses over distinct phases of the aeroelastic response. The initial response is comparable to classical panel flutter and is dominated by first- and second-mode panel deflections. Over time, a frequency lock-in occurs between K-H waves in the flow and high-order modes in the panel, resulting in mutual growth. The growth of the K-H instability leads to a period of cascading frequency and modal content in which energy is channeled into several discrete oscillating panel modes. It is shown through a bispectral mode decomposition that the frequency cascade is driven by nonlinear interactions between panel modes. The asymptotic state of the aeroelastic system is classified as a multi-mode limit cycle oscillation and exhibits a traveling wave flutter. The time-mean flow field exhibits reductions in both the separation bubble volume and downstream boundary layer thickness in the presence of the fluttering panel, supporting the notion of fluid-structure interaction as a means for passive flow control of SBLIs.
{"title":"Interplay between shock-induced panel flutter and the Kelvin-Helmholtz instability in laminar flow","authors":"James L. Fields , Anshul Suri , Caleb J. Barnes , Jack J. McNamara , Datta V. Gaitonde","doi":"10.1016/j.jfluidstructs.2025.104497","DOIUrl":"10.1016/j.jfluidstructs.2025.104497","url":null,"abstract":"<div><div>This paper investigates the interplay between the Kelvin-Helmholtz (K-H) instability, aeroelastic flutter, and laminar shock-boundary layer interactions. The coupled system is studied by performing modal-based analyses over distinct phases of the aeroelastic response. The initial response is comparable to classical panel flutter and is dominated by first- and second-mode panel deflections. Over time, a frequency lock-in occurs between K-H waves in the flow and high-order modes in the panel, resulting in mutual growth. The growth of the K-H instability leads to a period of cascading frequency and modal content in which energy is channeled into several discrete oscillating panel modes. It is shown through a bispectral mode decomposition that the frequency cascade is driven by nonlinear interactions between panel modes. The asymptotic state of the aeroelastic system is classified as a multi-mode limit cycle oscillation and exhibits a traveling wave flutter. The time-mean flow field exhibits reductions in both the separation bubble volume and downstream boundary layer thickness in the presence of the fluttering panel, supporting the notion of fluid-structure interaction as a means for passive flow control of SBLIs.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104497"},"PeriodicalIF":3.5,"publicationDate":"2026-01-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145980249","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-12DOI: 10.1016/j.jfluidstructs.2026.104512
Ming Lei , Qingyuan Gai , Tongfu Zou , Dan Xia
To enhance the surface operation capabilities of traditional bionic underwater vehicles (BUVs) in, this study explored the feasibility of dolphins performing cross-medium standing-and-turning (SAT) behavior on the water surface from a hydrodynamics perspective. A physical model and computational model of the robotic dolphin’s surface SAT behavior were established. After numerous attempts, the surface SAT behavior of the robotic dolphin was successfully replicated through coordinated movements of the body, caudal fin, and pectoral fins, and the quantitative relationship between controllable parameters and hydrodynamic performance was investigated. By combining data analysis and flow field distribution patterns, the underlying physical mechanisms of the robotic dolphin’s surface SAT behavior were revealed. The results indicate that the turning trajectory of SAT behavior exhibits a circular characteristic, and the turning radius can be adjusted by modifying the kinematic parameters. Additionally, when the movement parameters of the body and caudal fin are fixed, and the phase difference between the two pectoral fins is T/2, the robotic dolphin achieves optimal turning maneuverability, with a maximum turning speed of 1.69 rad/s and a turning efficiency of up to 45.5%. Notably, by optimizing kinematic parameters, the robotic dolphin achieves cross-medium in-situ turning with exceptionally high maneuverability, which is indeed a very valuable discovery. The findings provide a cross-medium fluid dynamics explanation for the development of BUVs with dual underwater/surface operating capabilities.
{"title":"Hydrodynamic study of a novel surface standing-and-turning behavior of robotic dolphins","authors":"Ming Lei , Qingyuan Gai , Tongfu Zou , Dan Xia","doi":"10.1016/j.jfluidstructs.2026.104512","DOIUrl":"10.1016/j.jfluidstructs.2026.104512","url":null,"abstract":"<div><div>To enhance the surface operation capabilities of traditional bionic underwater vehicles (BUVs) in, this study explored the feasibility of dolphins performing cross-medium standing-and-turning (SAT) behavior on the water surface from a hydrodynamics perspective. A physical model and computational model of the robotic dolphin’s surface SAT behavior were established. After numerous attempts, the surface SAT behavior of the robotic dolphin was successfully replicated through coordinated movements of the body, caudal fin, and pectoral fins, and the quantitative relationship between controllable parameters and hydrodynamic performance was investigated. By combining data analysis and flow field distribution patterns, the underlying physical mechanisms of the robotic dolphin’s surface SAT behavior were revealed. The results indicate that the turning trajectory of SAT behavior exhibits a circular characteristic, and the turning radius can be adjusted by modifying the kinematic parameters. Additionally, when the movement parameters of the body and caudal fin are fixed, and the phase difference between the two pectoral fins is <em>T</em>/2, the robotic dolphin achieves optimal turning maneuverability, with a maximum turning speed of 1.69 rad/s and a turning efficiency of up to 45.5%. Notably, by optimizing kinematic parameters, the robotic dolphin achieves cross-medium <em>in-situ</em> turning with exceptionally high maneuverability, which is indeed a very valuable discovery. The findings provide a cross-medium fluid dynamics explanation for the development of BUVs with dual underwater/surface operating capabilities.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104512"},"PeriodicalIF":3.5,"publicationDate":"2026-01-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145980244","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-12DOI: 10.1016/j.jfluidstructs.2026.104513
Hao Liu , Shaowei Wang , Moli Zhao , Peiyuan Wang , Shuai Liu , Yegao Qu
The vortex-induced vibration (VIV) dynamics of a flexible splitter beam interacting with the laminar wake flow of a circular cylinder in shear-thinning and shear-thickening fluids are investigated using a partitioned nonlinear fluid-structure interaction simulation. The flow field is modeled within an Arbitrary Lagrangian-Eulerian (ALE) framework based on the finite volume method. To capture the beam's large deformations, Reddy's higher-order shear deformation theory is employed in conjunction with von Kármán strain formulations. After validating the present method, a comprehensive analysis is conducted to investigate the effects of the following parameters, including beam characteristic length (L/H = 10 and 15), inflow velocity (0.5 m/s ≤ Ur ≤ 3 m/s), power-law index (0.6 ≤ n ≤ 1.4) and time constant (0.2 s ≤ ≤ 4 s) on the VIV characteristics (including limit-cycle oscillation, vortex shedding pattern and viscosity distribution) are discussed. Several distinct deformation regimes of elastic beams are observed: first or second mode-like vibration regimes; standing or traveling wave deflection vibration regimes; the large amplitude traveling wave symmetry vibration regimes; and periodic or quasi-periodic dual-frequency vibration regimes. These different regimes result in variations in the wake vortex modes, specifically the '2S' (two single vortices of opposite sign) and '2P' (two pairs of vortices) modes. Key findings indicate that shear-thinning fluids lowers the onset point of VIV in comparison with Newtonian fluids, while shear-thickening fluids elevates it, suggesting a viscous damping effect. Additionally, shear-thinning fluids amplify vorticity intensity and contract the wake region, while shear-thickening fluids suppress vorticity generation and significantly elongate the wake. Moreover, a higher time constant in shear-thinning fluids amplifies vibrations by enhancing vorticity persistence and energy transfer. In shear-thickening fluids, however, it suppresses VIV by promoting viscosity-dominated damping.
{"title":"Vortex-induced vibration dynamics of a splitter beam behind a cylinder in shear-thinning or shear-thickening non-Newtonian fluids","authors":"Hao Liu , Shaowei Wang , Moli Zhao , Peiyuan Wang , Shuai Liu , Yegao Qu","doi":"10.1016/j.jfluidstructs.2026.104513","DOIUrl":"10.1016/j.jfluidstructs.2026.104513","url":null,"abstract":"<div><div>The vortex-induced vibration (VIV) dynamics of a flexible splitter beam interacting with the laminar wake flow of a circular cylinder in shear-thinning and shear-thickening fluids are investigated using a partitioned nonlinear fluid-structure interaction simulation. The flow field is modeled within an Arbitrary Lagrangian-Eulerian (ALE) framework based on the finite volume method. To capture the beam's large deformations, Reddy's higher-order shear deformation theory is employed in conjunction with von Kármán strain formulations. After validating the present method, a comprehensive analysis is conducted to investigate the effects of the following parameters, including beam characteristic length (<em>L</em>/<em>H</em> = 10 and 15), inflow velocity (0.5 m/s ≤ <em>U<sub>r</sub></em> ≤ 3 m/s), power-law index (0.6 ≤ <em>n</em> ≤ 1.4) and time constant (0.2 s ≤ <span><math><mi>λ</mi></math></span> ≤ 4 s) on the VIV characteristics (including limit-cycle oscillation, vortex shedding pattern and viscosity distribution) are discussed. Several distinct deformation regimes of elastic beams are observed: first or second mode-like vibration regimes; standing or traveling wave deflection vibration regimes; the large amplitude traveling wave symmetry vibration regimes; and periodic or quasi-periodic dual-frequency vibration regimes. These different regimes result in variations in the wake vortex modes, specifically the '2S' (two single vortices of opposite sign) and '2P' (two pairs of vortices) modes. Key findings indicate that shear-thinning fluids lowers the onset point of VIV in comparison with Newtonian fluids, while shear-thickening fluids elevates it, suggesting a viscous damping effect. Additionally, shear-thinning fluids amplify vorticity intensity and contract the wake region, while shear-thickening fluids suppress vorticity generation and significantly elongate the wake. Moreover, a higher time constant in shear-thinning fluids amplifies vibrations by enhancing vorticity persistence and energy transfer. In shear-thickening fluids, however, it suppresses VIV by promoting viscosity-dominated damping.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104513"},"PeriodicalIF":3.5,"publicationDate":"2026-01-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145980248","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-11DOI: 10.1016/j.jfluidstructs.2025.104498
Masoud Hayatdavoodi , Shuijin Li
The interaction of combined waves and current with floating bodies is studied by conducting laboratory experiments and by developing theoretical models. The laboratory experiments are conducted in a wave-current tank using two floating cylinders with circular and square waterplane areas. Both freely floating and moored conditions are considered. Two theoretical models are developed to study wave-body and wave-current-body interactions: one based on the computational fluid dynamics and the other following the linear wave-current diffraction theory using the Green function method. Results from these models are compared with laboratory measurements for a range of wave and wave-current conditions. The study analyses the effect of ambient current on the wave-induced motions of floating bodies and evaluates how well the models capture the wave-current-body interactions. Additionally, the effect of the square cylinder’s sharp edges on wave-current-body interactions is analysed in comparison to the circular cylinder, along with the models’ capability to capture these effects. It is observed that the presence of the current not only causes significant drift of the freely floating cylinders, but also affects their surge and pitch oscillations, while having no notable effect on heave motion. For the conditions considered, the linear theory based on the Green function method provides overall good predictions of the floating bodies’ responses at a significantly lower computational cost compared to the computational fluid dynamics model.
{"title":"Wave-current-floating body interactions: Experiments and modelling","authors":"Masoud Hayatdavoodi , Shuijin Li","doi":"10.1016/j.jfluidstructs.2025.104498","DOIUrl":"10.1016/j.jfluidstructs.2025.104498","url":null,"abstract":"<div><div>The interaction of combined waves and current with floating bodies is studied by conducting laboratory experiments and by developing theoretical models. The laboratory experiments are conducted in a wave-current tank using two floating cylinders with circular and square waterplane areas. Both freely floating and moored conditions are considered. Two theoretical models are developed to study wave-body and wave-current-body interactions: one based on the computational fluid dynamics and the other following the linear wave-current diffraction theory using the Green function method. Results from these models are compared with laboratory measurements for a range of wave and wave-current conditions. The study analyses the effect of ambient current on the wave-induced motions of floating bodies and evaluates how well the models capture the wave-current-body interactions. Additionally, the effect of the square cylinder’s sharp edges on wave-current-body interactions is analysed in comparison to the circular cylinder, along with the models’ capability to capture these effects. It is observed that the presence of the current not only causes significant drift of the freely floating cylinders, but also affects their surge and pitch oscillations, while having no notable effect on heave motion. For the conditions considered, the linear theory based on the Green function method provides overall good predictions of the floating bodies’ responses at a significantly lower computational cost compared to the computational fluid dynamics model.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104498"},"PeriodicalIF":3.5,"publicationDate":"2026-01-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145980337","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-09DOI: 10.1016/j.jfluidstructs.2025.104499
Yuxiang Ying, Geng Guan, Tongxiao Jiang, Amin Ullah, JianZhong Lin
Microswimmers exhibit remarkable dynamic properties in fluid environments, making them important for advancing the fields of fluid mechanics and biophysics. In this study, we extended the classical squirmer model to an ellipsoidal geometry and investigated its swimming behavior in a three-dimensional square-tube flow. The results were compared with those of a spherical microswimmer. By systematically varying key parameters, including the self-propulsion strength (α), swimming type factor (β), chirality factor (χ), and flow field Reynolds number (Rem), we identified five distinct swimming modes: near-wall helical motion, near-center helical motion, steady linear motion, zigzag motion, and near-wall double-helical motion, in which the microswimmer exhibited two different swimming directions (upstream and downstream). The results show that chirality and geometric anisotropy significantly influenced the swimming behavior of the microswimmer. The formation of swimming modes is also related to the pressure distribution between the microswimmer and the wall. In addition, the swimming velocity and helical frequency of the microswimmer increased with increasing α or Rem; however, the increase in the Reynolds number did not change the swimming mode of the microswimmer. Our research is expected to promote the understanding of the motion characteristics of active matter in dynamic flows and provide valuable insights into the design of efficient and controllable artificial microswimmers for biomedical and environmental applications.
{"title":"Dynamics of elongated microswimmers in a square-tube flow","authors":"Yuxiang Ying, Geng Guan, Tongxiao Jiang, Amin Ullah, JianZhong Lin","doi":"10.1016/j.jfluidstructs.2025.104499","DOIUrl":"10.1016/j.jfluidstructs.2025.104499","url":null,"abstract":"<div><div>Microswimmers exhibit remarkable dynamic properties in fluid environments, making them important for advancing the fields of fluid mechanics and biophysics. In this study, we extended the classical squirmer model to an ellipsoidal geometry and investigated its swimming behavior in a three-dimensional square-tube flow. The results were compared with those of a spherical microswimmer. By systematically varying key parameters, including the self-propulsion strength (<em>α</em>), swimming type factor (<em>β</em>), chirality factor (<em>χ</em>), and flow field Reynolds number (<em>Re<sub>m</sub></em>), we identified five distinct swimming modes: near-wall helical motion, near-center helical motion, steady linear motion, zigzag motion, and near-wall double-helical motion, in which the microswimmer exhibited two different swimming directions (upstream and downstream). The results show that chirality and geometric anisotropy significantly influenced the swimming behavior of the microswimmer. The formation of swimming modes is also related to the pressure distribution between the microswimmer and the wall. In addition, the swimming velocity and helical frequency of the microswimmer increased with increasing <em>α</em> or <em>Re<sub>m</sub></em>; however, the increase in the Reynolds number did not change the swimming mode of the microswimmer. Our research is expected to promote the understanding of the motion characteristics of active matter in dynamic flows and provide valuable insights into the design of efficient and controllable artificial microswimmers for biomedical and environmental applications.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104499"},"PeriodicalIF":3.5,"publicationDate":"2026-01-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145929241","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-08DOI: 10.1016/j.jfluidstructs.2025.104500
Cristiano Biagioli, Francesco Serraino, Valerio Belardi, Francesco Vivio
This study investigates liquid sloshing in a rectangular tank equipped with horizontal flexible baffles to understand their influence on sloshing mitigation and intricate fluid-structure interaction (FSI) phenomena. A two-way coupled FSI model was developed using the Finite Element Method (FEM) for structural analysis and Finite Volume Method (FVM) with the Volume Of Fluid (VOF) formulation for fluid dynamics, employing a partitioned coupling strategy. Numerical decay tests explored dynamic behavior by varying baffle Young’s modulus and submergence levels. Enstrophy evolution was investigated as a robust indicator for quantifying energy dissipation associated with vortex dynamics, and a reduced-order acoustic-structural model was benchmarked as a tool for predicting fundamental frequency shifts. The FSI simulation methodology was validated against experimental results from previous literature, showing close agreement.
Key outcomes reveal that baffle stiffness critically governs system response, with appropriate flexibility significantly enhancing damping performance. For submerged baffles, increasing flexibility led to optimal damping driven by maximal vortex-induced energy loss. Conversely, shallow baffles showed superior damping with rigid configurations, primarily due to pressure drag rather than vortex dynamics. While initial conditions introduced transient nonlinearities with flexible baffles, overall trends for damping and frequency remained consistent. The simplified frequency-prediction model was reliable for practical flexibility ranges, but less accurate for extreme flexibility. Overall, this work deepens understanding of how baffle characteristics influence slosh mitigation, offering valuable guidance for anti-sloshing device engineering.
{"title":"Impact of baffle flexibility on sloshing mitigation: A parametric study using partitioned two-way fluid-structure interaction","authors":"Cristiano Biagioli, Francesco Serraino, Valerio Belardi, Francesco Vivio","doi":"10.1016/j.jfluidstructs.2025.104500","DOIUrl":"10.1016/j.jfluidstructs.2025.104500","url":null,"abstract":"<div><div>This study investigates liquid sloshing in a rectangular tank equipped with horizontal flexible baffles to understand their influence on sloshing mitigation and intricate fluid-structure interaction (FSI) phenomena. A two-way coupled FSI model was developed using the Finite Element Method (FEM) for structural analysis and Finite Volume Method (FVM) with the Volume Of Fluid (VOF) formulation for fluid dynamics, employing a partitioned coupling strategy. Numerical decay tests explored dynamic behavior by varying baffle Young’s modulus and submergence levels. Enstrophy evolution was investigated as a robust indicator for quantifying energy dissipation associated with vortex dynamics, and a reduced-order acoustic-structural model was benchmarked as a tool for predicting fundamental frequency shifts. The FSI simulation methodology was validated against experimental results from previous literature, showing close agreement.</div><div>Key outcomes reveal that baffle stiffness critically governs system response, with appropriate flexibility significantly enhancing damping performance. For submerged baffles, increasing flexibility led to optimal damping driven by maximal vortex-induced energy loss. Conversely, shallow baffles showed superior damping with rigid configurations, primarily due to pressure drag rather than vortex dynamics. While initial conditions introduced transient nonlinearities with flexible baffles, overall trends for damping and frequency remained consistent. The simplified frequency-prediction model was reliable for practical flexibility ranges, but less accurate for extreme flexibility. Overall, this work deepens understanding of how baffle characteristics influence slosh mitigation, offering valuable guidance for anti-sloshing device engineering.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104500"},"PeriodicalIF":3.5,"publicationDate":"2026-01-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145929240","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-06DOI: 10.1016/j.jfluidstructs.2025.104495
F. Paillé , Y. Haffner , C. Sicot
A method is presented to separate inertial and aerodynamic contributions to the forces measured in experiments on a non-rigid object in a flow. In particular, it can be used to remove spurious inertial contributions on aerodynamic loads measured with a balance. The method builds on a multiple-input/multiple-output framework and uses conditional spectral analysis in order to provide frequency response functions, or alternatively impulse response functions, to link the inputs quantifying inertia on the object (any kind of acceleration measurements) and the unknown aerodynamic forces on the object to the outputs quantifying total forces on the object (aerodynamic balance or any kind of force measurements). The method provides an efficient way of separating inertial and aerodynamic force contributions on objects in a flow from relatively few acceleration measurements and total force measurements.
This methodology is assessed on a wall-mounted cylinder in a turbulent boundary layer having two principal bending modes contributing to important inertial forces. It performs well to separate the inertial force contributions of the different bending modes from the pure aerodynamic force contributions which align very closely to the reference aerodynamic pressure forces. Especially, the method allows to separate unambiguously the inertial and aerodynamic force contributions even when structural and aerodynamic resonances have matching frequencies. A second test-case of a model of high-rise building with more complex structural dynamics and less effort put in manufacturing is presented. The method performs also well but with a bit more discrepancies to the reference aerodynamic pressure forces. In this case, part of the inertial forces are not correctly accounted for depending on the relevance of the location and number of acceleration measurements on the object, and on the complexity of the structural dynamics of the object. Leads are provided and discussed to tackle these relative limitations.
{"title":"Direct measurements of aerodynamic and inertial contributions to unsteady forces on non-rigid objects in a flow","authors":"F. Paillé , Y. Haffner , C. Sicot","doi":"10.1016/j.jfluidstructs.2025.104495","DOIUrl":"10.1016/j.jfluidstructs.2025.104495","url":null,"abstract":"<div><div>A method is presented to separate inertial and aerodynamic contributions to the forces measured in experiments on a non-rigid object in a flow. In particular, it can be used to remove spurious inertial contributions on aerodynamic loads measured with a balance. The method builds on a multiple-input/multiple-output framework and uses conditional spectral analysis in order to provide frequency response functions, or alternatively impulse response functions, to link the inputs quantifying inertia on the object (any kind of acceleration measurements) and the unknown aerodynamic forces on the object to the outputs quantifying total forces on the object (aerodynamic balance or any kind of force measurements). The method provides an efficient way of separating inertial and aerodynamic force contributions on objects in a flow from relatively few acceleration measurements and total force measurements.</div><div>This methodology is assessed on a wall-mounted cylinder in a turbulent boundary layer having two principal bending modes contributing to important inertial forces. It performs well to separate the inertial force contributions of the different bending modes from the pure aerodynamic force contributions which align very closely to the reference aerodynamic pressure forces. Especially, the method allows to separate unambiguously the inertial and aerodynamic force contributions even when structural and aerodynamic resonances have matching frequencies. A second test-case of a model of high-rise building with more complex structural dynamics and less effort put in manufacturing is presented. The method performs also well but with a bit more discrepancies to the reference aerodynamic pressure forces. In this case, part of the inertial forces are not correctly accounted for depending on the relevance of the location and number of acceleration measurements on the object, and on the complexity of the structural dynamics of the object. Leads are provided and discussed to tackle these relative limitations.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104495"},"PeriodicalIF":3.5,"publicationDate":"2026-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145929239","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-06DOI: 10.1016/j.jfluidstructs.2026.104501
Rongxin Chen , Hui Zhong , Bozhan Hai , Qingrui Song , Wei Zhang , Guofu Lian
Stick-slip behavior during friction is a critical factor contributing to the degradation of PDMS material performance. To mitigate this phenomenon, this study investigates the effects of silicone oil with varying parameters on the frictional and mechanical properties of PDMS sponges. Friction experiments were conducted by introducing silicone oil fluids, and the influence of silicone oil on the friction coefficient and stick-slip behavior was analyzed. Additionally, the nominal modulus of elasticity of PDMS sponges was measured to explore the interrelationship among elasticity, friction coefficient, and stick-slip behavior. The results demonstrate that as the viscosity of silicone oil increases, the stick-slip time (∆t) of PDMS sponge decreases, the difference between static and kinetic friction coefficients (∆μ) diminishes, and the modulus of elasticity of PDMS sponge increases. High-viscosity silicone oil effectively reduces both stick-slip behavior and the friction coefficient of PDMS sponge. At constant viscosity, an increase in the volume of silicone oil leads to a reduction in the friction coefficient of PDMS sponge but simultaneously enhances the likelihood of stick-slip behavior while decreasing the nominal modulus of elasticity. By controlling the liquid parameters of silicone oil, the friction coefficient and stick-slip behavior of PDMS sponges can be modulated. This study explores the formation mechanism of the viscous-slip behavior and proposes a method to control the viscous-slip behavior by different liquids. This can provide theoretical guidance for the regulation of viscous-slip behavior in other polymers.
{"title":"Mechanism and regulation of silicone oil fluid volume on the stick-slip behavior of PDMS sponges","authors":"Rongxin Chen , Hui Zhong , Bozhan Hai , Qingrui Song , Wei Zhang , Guofu Lian","doi":"10.1016/j.jfluidstructs.2026.104501","DOIUrl":"10.1016/j.jfluidstructs.2026.104501","url":null,"abstract":"<div><div>Stick-slip behavior during friction is a critical factor contributing to the degradation of PDMS material performance. To mitigate this phenomenon, this study investigates the effects of silicone oil with varying parameters on the frictional and mechanical properties of PDMS sponges. Friction experiments were conducted by introducing silicone oil fluids, and the influence of silicone oil on the friction coefficient and stick-slip behavior was analyzed. Additionally, the nominal modulus of elasticity of PDMS sponges was measured to explore the interrelationship among elasticity, friction coefficient, and stick-slip behavior. The results demonstrate that as the viscosity of silicone oil increases, the stick-slip time (<em>∆t</em>) of PDMS sponge decreases, the difference between static and kinetic friction coefficients (<em>∆μ</em>) diminishes, and the modulus of elasticity of PDMS sponge increases. High-viscosity silicone oil effectively reduces both stick-slip behavior and the friction coefficient of PDMS sponge. At constant viscosity, an increase in the volume of silicone oil leads to a reduction in the friction coefficient of PDMS sponge but simultaneously enhances the likelihood of stick-slip behavior while decreasing the nominal modulus of elasticity. By controlling the liquid parameters of silicone oil, the friction coefficient and stick-slip behavior of PDMS sponges can be modulated. This study explores the formation mechanism of the viscous-slip behavior and proposes a method to control the viscous-slip behavior by different liquids. This can provide theoretical guidance for the regulation of viscous-slip behavior in other polymers.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104501"},"PeriodicalIF":3.5,"publicationDate":"2026-01-06","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145929238","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2026-01-05DOI: 10.1016/j.jfluidstructs.2025.104496
Elias Farah , Abdellatif Ouahsine , Patrick G. Verdin , Badr Kaoui
The direct-forcing immersed boundary method (DF-IBM) algorithm previously developed by the authors is extended by coupling the Navier-Stokes equations with the Newton-Euler equations for rigid body dynamics within the DF-IBM framework. This coupling broadens the applicability of the previous development, from stationary or prescribed motion to flow-induced (free) motion cases. To address fluid-rigid body interactions under a partitioned approach, an implicit coupling algorithm is developed to handle strongly coupled interface conditions. Stability and convergence issues, particularly stemming from critical solid-fluid density ratios and from the rigid body approximation of internal mass effects in rotational dynamics, are mitigated using a fixed relaxation technique for the rigid body kinematics to ensure numerical robustness. Additionally, the proposed algorithm leverages the previously developed DF-IBM formulation and the predictor-corrector strategy of the pressure implicit with splitting of operators (PISO) algorithm by omitting the momentum predictor step and the costly corrector loops from the implicit iterations. The method is validated against several benchmark cases, demonstrating robustness, stability, and efficiency in capturing complex fluid-rigid body interactions across a range of challenging scenarios.
{"title":"Stable fluid-rigid body interaction algorithm using the direct-forcing immersed boundary method (DF-IBM)","authors":"Elias Farah , Abdellatif Ouahsine , Patrick G. Verdin , Badr Kaoui","doi":"10.1016/j.jfluidstructs.2025.104496","DOIUrl":"10.1016/j.jfluidstructs.2025.104496","url":null,"abstract":"<div><div>The direct-forcing immersed boundary method (DF-IBM) algorithm previously developed by the authors is extended by coupling the Navier-Stokes equations with the Newton-Euler equations for rigid body dynamics within the DF-IBM framework. This coupling broadens the applicability of the previous development, from stationary or prescribed motion to flow-induced (free) motion cases. To address fluid-rigid body interactions under a partitioned approach, an implicit coupling algorithm is developed to handle strongly coupled interface conditions. Stability and convergence issues, particularly stemming from critical solid-fluid density ratios and from the rigid body approximation of internal mass effects in rotational dynamics, are mitigated using a fixed relaxation technique for the rigid body kinematics to ensure numerical robustness. Additionally, the proposed algorithm leverages the previously developed DF-IBM formulation and the predictor-corrector strategy of the pressure implicit with splitting of operators (PISO) algorithm by omitting the momentum predictor step and the costly corrector loops from the implicit iterations. The method is validated against several benchmark cases, demonstrating robustness, stability, and efficiency in capturing complex fluid-rigid body interactions across a range of challenging scenarios.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"142 ","pages":"Article 104496"},"PeriodicalIF":3.5,"publicationDate":"2026-01-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145898054","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}