TPMS–Gyroid cellular materials demonstrate excellent performance in terms of specific strength and energy absorption, making them ideal candidate materials for lightweight protective structure design. The mechanical response of Gyroid cellular material under quasi-static compression, direct impact, and mass impact was experimentally investigated in this study. Constitutive models were employed to characterize the mechanical response and power-law relationships between their material parameters and the relative density were obtained. Cellular specimens were fabricated from PLA and tested by using the Taylor–Hopkinson pressure bar experimental technique combined with high-speed photography. In experimental tests, two deformation patterns were observed: a topology-dominated, random, layered collapse under quasi-static loading and an inertia-dominated, layer-by-layer collapse under dynamic impact. The initial crush stress and strain-hardening parameter, and their power-law density dependence, were determined. Experimental tests involving both large-mass, low-velocity and small-mass, high-velocity impacts confirmed that the dynamic constitutive model of Gyroid cellular material demonstrated excellent predictive performance. Therefore, the feasibility and reliability of the constitutive relationship for Gyroid cellular materials were verified, and the resulting shock models can guide the design of protective structures in engineering practice.
{"title":"Quasi-static and dynamic compression behavior of 3D-printed TPMS–Gyroid cellular material","authors":"Wenfang Yuan , Kefeng Peng , Yuying Ma , Yuxuan Zheng , Baixue Chang , Zhijun Zheng","doi":"10.1016/j.tws.2026.114681","DOIUrl":"10.1016/j.tws.2026.114681","url":null,"abstract":"<div><div>TPMS–Gyroid cellular materials demonstrate excellent performance in terms of specific strength and energy absorption, making them ideal candidate materials for lightweight protective structure design. The mechanical response of Gyroid cellular material under quasi-static compression, direct impact, and mass impact was experimentally investigated in this study. Constitutive models were employed to characterize the mechanical response and power-law relationships between their material parameters and the relative density were obtained. Cellular specimens were fabricated from PLA and tested by using the Taylor–Hopkinson pressure bar experimental technique combined with high-speed photography. In experimental tests, two deformation patterns were observed: a topology-dominated, random, layered collapse under quasi-static loading and an inertia-dominated, layer-by-layer collapse under dynamic impact. The initial crush stress and strain-hardening parameter, and their power-law density dependence, were determined. Experimental tests involving both large-mass, low-velocity and small-mass, high-velocity impacts confirmed that the dynamic constitutive model of Gyroid cellular material demonstrated excellent predictive performance. Therefore, the feasibility and reliability of the constitutive relationship for Gyroid cellular materials were verified, and the resulting shock models can guide the design of protective structures in engineering practice.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114681"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147387271","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-07DOI: 10.1016/j.tws.2026.114640
Tao Du , Faqi Liu , Hua Yang , Yinglong Li
The emphasis of this paper is on the buckling behaviour of high-strength concrete-filled high-strength steel tubular (HCFHST) columns after exposure to fire. Nine slender HCFHST specimens were subjected to ISO 834 standard fire and axial load after cooling. The failure mode, deformation, buckling capacity, and strain of the specimens were monitored and reported. With a reduction close to that in cross-sectional capacity, the buckling capacity of specimens with a slenderness ratio of 53 decreases by 32.6% and 48.1% following exposure to fire for 45 min and 90 min, respectively. Furthermore, the experimental results indicate that the effects of fire duration and slenderness ratio on buckling capacity were essentially found to be uncoupled within the experimental parameters. A thermo-mechanical coupled finite element model was established using ABAQUS and confirmed to be reliable through comparison with the test results. A parametric analysis was carried out to investigate the effects of a wider range of parameters, including fire duration, cross-sectional diameter, slenderness ratio, steel ratio, and material strength, on the residual buckling resistance. Finally, the historical peak temperatures and the reduction in material residual performance were incorporated into the existing ambient-temperature resistance design methods. The methods can be used to predict the residual buckling resistance of slender HCFHST columns, assess their post-fire safety, and provide a basis for subsequent strengthening.
{"title":"Buckling behaviour of high-strength concrete-filled high-strength steel tubular columns after fire exposure","authors":"Tao Du , Faqi Liu , Hua Yang , Yinglong Li","doi":"10.1016/j.tws.2026.114640","DOIUrl":"10.1016/j.tws.2026.114640","url":null,"abstract":"<div><div>The emphasis of this paper is on the buckling behaviour of high-strength concrete-filled high-strength steel tubular (HCFHST) columns after exposure to fire. Nine slender HCFHST specimens were subjected to ISO 834 standard fire and axial load after cooling. The failure mode, deformation, buckling capacity, and strain of the specimens were monitored and reported. With a reduction close to that in cross-sectional capacity, the buckling capacity of specimens with a slenderness ratio of 53 decreases by 32.6% and 48.1% following exposure to fire for 45 min and 90 min, respectively. Furthermore, the experimental results indicate that the effects of fire duration and slenderness ratio on buckling capacity were essentially found to be uncoupled within the experimental parameters. A thermo-mechanical coupled finite element model was established using ABAQUS and confirmed to be reliable through comparison with the test results. A parametric analysis was carried out to investigate the effects of a wider range of parameters, including fire duration, cross-sectional diameter, slenderness ratio, steel ratio, and material strength, on the residual buckling resistance. Finally, the historical peak temperatures and the reduction in material residual performance were incorporated into the existing ambient-temperature resistance design methods. The methods can be used to predict the residual buckling resistance of slender HCFHST columns, assess their post-fire safety, and provide a basis for subsequent strengthening.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114640"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147387273","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-11DOI: 10.1016/j.tws.2026.114658
Yuelin Song , Zhi Xu , Chenyang Liu , Ziya Peng , Shanyu Xu , Cheng Zhao , Jiping Zhang
This research explores the characteristics of low-cycle fatigue crack growth in stiffened plate structures from the perspective of cumulative plastic damage. A novel predictive approach for fatigue crack growth rates is proposed, which integrates a correction factor to account for welding residual stress effects and utilizes accumulated plastic dissipation energy at a critical distance ahead of the crack tip as the driving parameter. The stiffened plate specimen with a central stiffener is fabricated to examine crack propagation behavior, focusing on single-sided and double-sided crack positions relative to the stiffener. A numerical program is developed to simulate simultaneous crack propagation in the plate and stiffener, enabling evaluation of cumulative plastic damage under cyclic stress. The proposed method demonstrates high accuracy in predicting fatigue crack growth rates for welded stiffened plates, as evidenced by strong agreement between predictions and experimental data.
{"title":"A low-cycle fatigue crack growth prediction method for ship stiffened plates considering accumulative plastic damage","authors":"Yuelin Song , Zhi Xu , Chenyang Liu , Ziya Peng , Shanyu Xu , Cheng Zhao , Jiping Zhang","doi":"10.1016/j.tws.2026.114658","DOIUrl":"10.1016/j.tws.2026.114658","url":null,"abstract":"<div><div>This research explores the characteristics of low-cycle fatigue crack growth in stiffened plate structures from the perspective of cumulative plastic damage. A novel predictive approach for fatigue crack growth rates is proposed, which integrates a correction factor to account for welding residual stress effects and utilizes accumulated plastic dissipation energy at a critical distance ahead of the crack tip as the driving parameter. The stiffened plate specimen with a central stiffener is fabricated to examine crack propagation behavior, focusing on single-sided and double-sided crack positions relative to the stiffener. A numerical program is developed to simulate simultaneous crack propagation in the plate and stiffener, enabling evaluation of cumulative plastic damage under cyclic stress. The proposed method demonstrates high accuracy in predicting fatigue crack growth rates for welded stiffened plates, as evidenced by strong agreement between predictions and experimental data.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114658"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147387276","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-21DOI: 10.1016/j.tws.2026.114698
Dandan Xia, Wanghua Yu, Ziyong Lin, Li Lin
Aerodynamic forces and coefficients are essential for explaining the mechanism and suppression of the vortex-induced vibrations (VIVs) of bridge decks in large-span bridges. However, in a wind-tunnel test, the aerodynamic force usually cannot be directly measured. In this research, a modified particle filter with unknown inputs that combines a particle filter algorithm and a Kalman filter (PKF-UI) is proposed to identify the aerodynamic coefficients and forces of VIVs. The effectiveness of the proposed PKF-UI method is firstly verified using three-degree-of-freedom nonlinear structures. The effects of the number of particles and noise level are discussed. The results show that the proposed method can effectively identify both structural parameters and unknown inputs. With the addition of 10 % white noise for the measurement, the identified structural parameter errors are 10 %, indicating that such a method can be applied effectively to the experimental data. Wind-tunnel tests are conducted on the bridge deck of a large-span bridge, and VIVs are obtained. With the utilization of the proposed method, the accelerations and displacements, which can be measured in the experiment, are fused to identify the aerodynamic forces and coefficients in the VIV lock-in regions.
{"title":"Identification of the aerodynamic coefficients and forces of vortex-induced vibration of bridge decks based on the particle filter algorithm","authors":"Dandan Xia, Wanghua Yu, Ziyong Lin, Li Lin","doi":"10.1016/j.tws.2026.114698","DOIUrl":"10.1016/j.tws.2026.114698","url":null,"abstract":"<div><div>Aerodynamic forces and coefficients are essential for explaining the mechanism and suppression of the vortex-induced vibrations (VIVs) of bridge decks in large-span bridges. However, in a wind-tunnel test, the aerodynamic force usually cannot be directly measured. In this research, a modified particle filter with unknown inputs that combines a particle filter algorithm and a Kalman filter (PKF-UI) is proposed to identify the aerodynamic coefficients and forces of VIVs. The effectiveness of the proposed PKF-UI method is firstly verified using three-degree-of-freedom nonlinear structures. The effects of the number of particles and noise level are discussed. The results show that the proposed method can effectively identify both structural parameters and unknown inputs. With the addition of 10 % white noise for the measurement, the identified structural parameter errors are 10 %, indicating that such a method can be applied effectively to the experimental data. Wind-tunnel tests are conducted on the bridge deck of a large-span bridge, and VIVs are obtained. With the utilization of the proposed method, the accelerations and displacements, which can be measured in the experiment, are fused to identify the aerodynamic forces and coefficients in the VIV lock-in regions.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114698"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147386454","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-27DOI: 10.1016/j.tws.2026.114736
Hao Miao, Peng Jiao, Baoxin Nie, Zhihuan Ding, Zhiping Chen
Thin-walled composite cylindrical shells hold significant importance in aerospace applications. The utilization of variable-stiffness composites (VSC) with curvilinear fibers is gaining increasing attention for buckling design of cylindrical shells. Given their substantially greater complexity in both fiber orientation distribution and thickness variation compared to conventional straight-fiber composites, nonlinear buckling analysis of VSC structure via the finite element method incurs considerably higher computational demands. To enhance the computational efficiency, an IGA-based framework aiming at buckling prediction of VSC cylindrical shells with non-uniform thickness is established in this paper for the first time. To address the practical limitations of existing IGA surface reconstruction methods, we propose a novel cylindrical shell modeling approach that integrates NURBS surface fitting with the Inverse Distance Weighting (IDW) method, enabling effective reconstruction of VSC cylindrical shells. Isogeometric shell elements based on 7-parameter solid shell theory incorporating artificial damping are used for nonlinear buckling analysis of VSC shell structures. Four representative case studies validate the accuracy and computational efficiency of the proposed element and framework. Results demonstrate that the IGA elements consistently achieve significantly higher computational efficiency than conventional shell elements. The proposed framework offers a novel approach for the application of IGA in nonlinear buckling analysis of composite structures.
{"title":"Isogeometric solid-shell framework for nonlinear buckling analysis of variable-stiffness composite cylindrical shells incorporating measured imperfections and thickness variations","authors":"Hao Miao, Peng Jiao, Baoxin Nie, Zhihuan Ding, Zhiping Chen","doi":"10.1016/j.tws.2026.114736","DOIUrl":"10.1016/j.tws.2026.114736","url":null,"abstract":"<div><div>Thin-walled composite cylindrical shells hold significant importance in aerospace applications. The utilization of variable-stiffness composites (VSC) with curvilinear fibers is gaining increasing attention for buckling design of cylindrical shells. Given their substantially greater complexity in both fiber orientation distribution and thickness variation compared to conventional straight-fiber composites, nonlinear buckling analysis of VSC structure via the finite element method incurs considerably higher computational demands. To enhance the computational efficiency, an IGA-based framework aiming at buckling prediction of VSC cylindrical shells with non-uniform thickness is established in this paper for the first time. To address the practical limitations of existing IGA surface reconstruction methods, we propose a novel cylindrical shell modeling approach that integrates NURBS surface fitting with the Inverse Distance Weighting (IDW) method, enabling effective reconstruction of VSC cylindrical shells. Isogeometric shell elements based on 7-parameter solid shell theory incorporating artificial damping are used for nonlinear buckling analysis of VSC shell structures. Four representative case studies validate the accuracy and computational efficiency of the proposed element and framework. Results demonstrate that the IGA elements consistently achieve significantly higher computational efficiency than conventional shell elements. The proposed framework offers a novel approach for the application of IGA in nonlinear buckling analysis of composite structures.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114736"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147386618","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-17DOI: 10.1016/j.tws.2026.114677
X.M. Liu , Y.X. Hao , W. Zhang , H.D. Xia , S.W. Yang , Y.T. Cao
Recently, variable-stiffness bistable laminates with curved fibers have gained attention in deformation structure research. Compared to straight-fiber bistable laminates, they offer reduced weight, adjustable stiffness, and a broader range of stable configurations. This study explores the stable-state configuration, natural frequency, and nonlinear vibration-active control using active methods for a bistable composite laminate with variable stiffness (VSBCL) simply supported at its four corners. Using a 17-parameter polynomial configuration function that accounts for the local influence and boundary effects of smart piezoelectric materials on the stable-state configuration of bistable structures, the configuration equation for the system is formulated using the von Karman geometric nonlinear strain-displacement relation and the energy principle. Furthermore, a nonlinear ordinary differential equation incorporating electromechanical coupling is derived for the system. Using this equation, the characteristics of the stable-state configuration under various fiber curvature-laying paths are examined and compared with finite-element analysis results. The natural vibration characteristics are then discussed. Employing fuzzy control theory, a fuzzy controller with VSCBL curvature as the key parameter is designed. Its performance and reliability are further validated through a comparative analysis with the traditional PID controller. Then, the nonlinear dynamic behavior and fuzzy control of the bistable laminated structure are investigated under various loading conditions, including step, decreasing, increasing, and sinusoidal loads. Numerical simulations under multiple conditions show that the proposed fuzzy control strategy greatly improves structural response regulation, providing a practical method for actively controlling a vibrating variable-stiffness bistable composite laminate.
{"title":"Intelligent vibration control of variable stiffness bistable composites laminate for curvilinear fiber trajectory with asymmetric laying strategy","authors":"X.M. Liu , Y.X. Hao , W. Zhang , H.D. Xia , S.W. Yang , Y.T. Cao","doi":"10.1016/j.tws.2026.114677","DOIUrl":"10.1016/j.tws.2026.114677","url":null,"abstract":"<div><div>Recently, variable-stiffness bistable laminates with curved fibers have gained attention in deformation structure research. Compared to straight-fiber bistable laminates, they offer reduced weight, adjustable stiffness, and a broader range of stable configurations. This study explores the stable-state configuration, natural frequency, and nonlinear vibration-active control using active methods for a bistable composite laminate with variable stiffness (VSBCL) simply supported at its four corners. Using a 17-parameter polynomial configuration function that accounts for the local influence and boundary effects of smart piezoelectric materials on the stable-state configuration of bistable structures, the configuration equation for the system is formulated using the von Karman geometric nonlinear strain-displacement relation and the energy principle. Furthermore, a nonlinear ordinary differential equation incorporating electromechanical coupling is derived for the system. Using this equation, the characteristics of the stable-state configuration under various fiber curvature-laying paths are examined and compared with finite-element analysis results. The natural vibration characteristics are then discussed. Employing fuzzy control theory, a fuzzy controller with VSCBL curvature as the key parameter is designed. Its performance and reliability are further validated through a comparative analysis with the traditional PID controller. Then, the nonlinear dynamic behavior and fuzzy control of the bistable laminated structure are investigated under various loading conditions, including step, decreasing, increasing, and sinusoidal loads. Numerical simulations under multiple conditions show that the proposed fuzzy control strategy greatly improves structural response regulation, providing a practical method for actively controlling a vibrating variable-stiffness bistable composite laminate.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114677"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147386817","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-24DOI: 10.1016/j.tws.2026.114671
Hao Zhang , Yiwei Chen , Wenzhe Song , Jing-Hua Zheng , Congze Fan , Zhongde Shan
Additive manufacturing of continuous fiber reinforced polymer composites enables precise fiber placement and design flexibility, making it a key technology for fabricating aerospace and automotive components. Evaluating the interlaminar fracture toughness of additively manufactured composites is crucial, as low resistance to opening-mode delamination can compromise interlayer fusion quality and impair the reliability of high-precision applications. This study employed Response Surface Methodology (RSM) to correlate nozzle temperature, printing speed, and layer thickness with the Mode I interlaminar fracture toughness (GIC) of additively manufactured CGF/PEEK composites through Double Cantilever Beam (DCB) tests. Analysis of Variance (ANOVA) and univariate analysis were employed to evaluate the effects of individual factors and their interactions, revealing statistically significant influences on fracture toughness. Results showed that layer thickness had the most significant effect on GIC. Reducing the layer thickness from 0.24 mm to 0.16 mm increased the average GIC from 57.2 J/m2 to 533.2 J/m2. Mechanistically, thinner layers facilitated deeper thermal penetration and polymer chain entanglement while suppressing interlaminar voids. These conditions facilitated robust energy-dissipation mechanisms, including fiber bridging and microscale tearing, during the fracture process. To further elucidate the interlaminar behavior of CGF/PEEK, the fusion process and failure characteristics were analyzed, leading to the development of a mechanistic model that demonstrates high predictive accuracy (R2≈0.972). This study establishes a processing foundation for producing additively manufactured CGF/PEEK components with high interlaminar fracture toughness suitable for aerospace applications.
{"title":"Effects of processing parameters on the Mode I interlaminar fracture toughness of additively manufactured continuous glass fiber reinforced PEEK composites","authors":"Hao Zhang , Yiwei Chen , Wenzhe Song , Jing-Hua Zheng , Congze Fan , Zhongde Shan","doi":"10.1016/j.tws.2026.114671","DOIUrl":"10.1016/j.tws.2026.114671","url":null,"abstract":"<div><div>Additive manufacturing of continuous fiber reinforced polymer composites enables precise fiber placement and design flexibility, making it a key technology for fabricating aerospace and automotive components. Evaluating the interlaminar fracture toughness of additively manufactured composites is crucial, as low resistance to opening-mode delamination can compromise interlayer fusion quality and impair the reliability of high-precision applications. This study employed Response Surface Methodology (RSM) to correlate nozzle temperature, printing speed, and layer thickness with the Mode I interlaminar fracture toughness (<em>G<sub>IC</sub></em>) of additively manufactured CGF/PEEK composites through Double Cantilever Beam (DCB) tests. Analysis of Variance (ANOVA) and univariate analysis were employed to evaluate the effects of individual factors and their interactions, revealing statistically significant influences on fracture toughness. Results showed that layer thickness had the most significant effect on <em>G<sub>IC</sub></em>. Reducing the layer thickness from 0.24 mm to 0.16 mm increased the average <em>G<sub>IC</sub></em> from 57.2 J/m<sup>2</sup> to 533.2 J/m<sup>2</sup>. Mechanistically, thinner layers facilitated deeper thermal penetration and polymer chain entanglement while suppressing interlaminar voids. These conditions facilitated robust energy-dissipation mechanisms, including fiber bridging and microscale tearing, during the fracture process. To further elucidate the interlaminar behavior of CGF/PEEK, the fusion process and failure characteristics were analyzed, leading to the development of a mechanistic model that demonstrates high predictive accuracy (<em>R</em><sup>2</sup>≈0.972). This study establishes a processing foundation for producing additively manufactured CGF/PEEK components with high interlaminar fracture toughness suitable for aerospace applications.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114671"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147386974","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-24DOI: 10.1016/j.tws.2026.114719
Zhongkai Ji , Dawei Li , Xiaoya Zhai , Jie Gao , Yunlong Tang , Ning Dai , Wenhe Liao , Yong Zhao , Yi Min Xie
Mechanical metamaterials and metastructures exhibit unconventional mechanical and functional properties not found in conventional materials. The unique characteristics originate from special geometric and topological arrangements of their constituent unit cells. Anisotropy is a fundamental physical property and is instrumental in tailoring mechanical responses. Its strategic implementation is a key determinant for achieving structure-function integration, expanding the accessible design space, and addressing multi-physics coupling requirements. Consequently, the precise orchestration of material architecture to elicit targeted functionalities has become a central theme in advanced materials research. Advanced computational design and additive manufacturing are pivotal in creating bio-inspired metamaterials, mimicking the complex anisotropy of natural structures to achieve integrated functionalities. This review summarizes recent advancements in anisotropic design, covering its conceptual evolution and classification. It analyzes unit-cell design methodologies, highlighting the shift toward intelligent, data-driven algorithms. The review explores macroscopic deformation in metastructures, controlled by spatially modulating unit-cell properties. Finally, this work synthesizes key strategies and evaluates future trajectories, aiming to establish a theoretical foundation and propose new paradigms. These efforts are intended to accelerate the discovery and implementation of next-generation metamaterials and metastructures.
{"title":"Designing anisotropic mechanical metamaterials and metastructures: a review","authors":"Zhongkai Ji , Dawei Li , Xiaoya Zhai , Jie Gao , Yunlong Tang , Ning Dai , Wenhe Liao , Yong Zhao , Yi Min Xie","doi":"10.1016/j.tws.2026.114719","DOIUrl":"10.1016/j.tws.2026.114719","url":null,"abstract":"<div><div>Mechanical metamaterials and metastructures exhibit unconventional mechanical and functional properties not found in conventional materials. The unique characteristics originate from special geometric and topological arrangements of their constituent unit cells. Anisotropy is a fundamental physical property and is instrumental in tailoring mechanical responses. Its strategic implementation is a key determinant for achieving structure-function integration, expanding the accessible design space, and addressing multi-physics coupling requirements. Consequently, the precise orchestration of material architecture to elicit targeted functionalities has become a central theme in advanced materials research. Advanced computational design and additive manufacturing are pivotal in creating bio-inspired metamaterials, mimicking the complex anisotropy of natural structures to achieve integrated functionalities. This review summarizes recent advancements in anisotropic design, covering its conceptual evolution and classification. It analyzes unit-cell design methodologies, highlighting the shift toward intelligent, data-driven algorithms. The review explores macroscopic deformation in metastructures, controlled by spatially modulating unit-cell properties. Finally, this work synthesizes key strategies and evaluates future trajectories, aiming to establish a theoretical foundation and propose new paradigms. These efforts are intended to accelerate the discovery and implementation of next-generation metamaterials and metastructures.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114719"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147386978","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-02-26DOI: 10.1016/j.tws.2026.114715
Chenmin Zhao , Bing Wang , Chenglong Guan , Guofu Lian
A composite tape-spring (CTS) structure is a thin-walled structure with a curved cross-section. Owing to its curved cross-section being capable of flattening, the CTS is well-suited for folding. Its ability to fold under large displacement makes it attractive as a hinge safety component. Compared with the traditional lock-link connection, its weight, complexity and maintenance can be reduced. Among them, the internal stress level of the CTS determines its folding mechanism, while the traditional composite manufacturing method is tricky to tailor the internal stress. In this paper, we developed a biaxial elastic fibre prestraining method to design prestrained CTS. The biaxial fibre tensile rig was designed to apply tension in the warp and weft directions of the plain-weave carbon prepreg, and the tension constant during the curing process. The FEA and theoretical were established and calibrated by the experimental data. The peak strain of the folding band was studied to evaluate the effect of prestrain on the folding strain. It is found that elastic fibre prestraining can effectively adjust the internal strain/stress level of the prestrained CTS, and can reduce the maximum tensile strain, thereby improving the load-carrying capacity. These findings will contribute to the structural design of foldable mechanical hinges.
{"title":"Folding mechanism within a prestrained composite tape-spring structure","authors":"Chenmin Zhao , Bing Wang , Chenglong Guan , Guofu Lian","doi":"10.1016/j.tws.2026.114715","DOIUrl":"10.1016/j.tws.2026.114715","url":null,"abstract":"<div><div>A composite tape-spring (CTS) structure is a thin-walled structure with a curved cross-section. Owing to its curved cross-section being capable of flattening, the CTS is well-suited for folding. Its ability to fold under large displacement makes it attractive as a hinge safety component. Compared with the traditional lock-link connection, its weight, complexity and maintenance can be reduced. Among them, the internal stress level of the CTS determines its folding mechanism, while the traditional composite manufacturing method is tricky to tailor the internal stress. In this paper, we developed a biaxial elastic fibre prestraining method to design prestrained CTS. The biaxial fibre tensile rig was designed to apply tension in the warp and weft directions of the plain-weave carbon prepreg, and the tension constant during the curing process. The FEA and theoretical were established and calibrated by the experimental data. The peak strain of the folding band was studied to evaluate the effect of prestrain on the folding strain. It is found that elastic fibre prestraining can effectively adjust the internal strain/stress level of the prestrained CTS, and can reduce the maximum tensile strain, thereby improving the load-carrying capacity. These findings will contribute to the structural design of foldable mechanical hinges.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114715"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147386981","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"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 : 2026-05-01Epub Date: 2026-01-26DOI: 10.1016/j.tws.2026.114583
Wei Yi, Yinian Wu, Shuxin Huang, Qiuhua Rao, Jiawei Liu, Kai Shen, Shaobo Jin
Accurate determination of stress intensity factors (SIFs) for a curved crack in orthotropic materials is critically important for assessing the stability of engineering structures and predicting the formation of fracture networks in shale-gas and geothermal development. Although the semi-analytical solutions for curved crack in anisotropic materials are well-established, fully analytical solutions for elliptical arc cracks in orthotropic materials remain scarce. In this study, we develop a closed-form analytical solution for the SIFs of an elliptical arc crack embedded in an orthotropic infinite plane under remote loading, under the condition that the material exhibits equal characteristic roots. The proposed method integrates affine transformation, conformal mapping, and complex variable theory to transform the original orthotropic problem into an equivalent isotropic one, whereby explicit expressions for the complex potentials and SIFs are systematically derived. The accuracy and robustness of the solution are validated through comparison with existing exact results for circular arc crack and finite element results for elliptical arc crack. Furthermore, the presented analytical framework can be extended to analyze other types of crack configurations such as branched cracks in orthotropic materials with equal characteristic roots, providing a theoretical foundation for advanced fracture mechanics assessments in anisotropic solids.
{"title":"An analytical solution for elliptical arc crack in orthotropic materials with equal characteristic roots","authors":"Wei Yi, Yinian Wu, Shuxin Huang, Qiuhua Rao, Jiawei Liu, Kai Shen, Shaobo Jin","doi":"10.1016/j.tws.2026.114583","DOIUrl":"10.1016/j.tws.2026.114583","url":null,"abstract":"<div><div>Accurate determination of stress intensity factors (SIFs) for a curved crack in orthotropic materials is critically important for assessing the stability of engineering structures and predicting the formation of fracture networks in shale-gas and geothermal development. Although the semi-analytical solutions for curved crack in anisotropic materials are well-established, fully analytical solutions for elliptical arc cracks in orthotropic materials remain scarce. In this study, we develop a closed-form analytical solution for the SIFs of an elliptical arc crack embedded in an orthotropic infinite plane under remote loading, under the condition that the material exhibits equal characteristic roots. The proposed method integrates affine transformation, conformal mapping, and complex variable theory to transform the original orthotropic problem into an equivalent isotropic one, whereby explicit expressions for the complex potentials and SIFs are systematically derived. The accuracy and robustness of the solution are validated through comparison with existing exact results for circular arc crack and finite element results for elliptical arc crack. Furthermore, the presented analytical framework can be extended to analyze other types of crack configurations such as branched cracks in orthotropic materials with equal characteristic roots, providing a theoretical foundation for advanced fracture mechanics assessments in anisotropic solids.</div></div>","PeriodicalId":49435,"journal":{"name":"Thin-Walled Structures","volume":"224 ","pages":"Article 114583"},"PeriodicalIF":6.6,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"147387269","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}