Pub Date : 2025-12-01DOI: 10.1016/j.finmec.2025.100341
Yuling Wei , Fei Pan , Jintao Du , Jinwu Xiang , Yuli Chen
Non-pneumatic tires (NPTs) represent a revolutionary advancement in the tire industry, owing to their puncture-proof nature and high design flexibility. To achieve both high load-bearing capability and low, evenly distributed ground pressure, the shear band structure of NPTs must balance high compressive stiffness with shear flexibility. To address this challenge, this work proposes a novel shear band structure based on tensegrity metamaterials. By adjusting the stiffness of two types of springs, the proposed shear band enables independent control of its compressive and shear stiffness. The shear band is subsequently integrated with various types of spokes, and the effects of multiple design parameters on the tire’s load-bearing capacity, peak material stress, and contact pressure are systematically analyzed. To achieve performance customization, a Bayesian optimization framework is developed to autonomously explore parameter sets that satisfy performance requirements while minimizing stress and contact pressure. Finally, the feasibility of the tensegrity metamaterial-based shear band design is validated through its successful integration into a four-wheel-drive vehicle model. The proposed shear band offers a new approach for the customized performance and practical application of NPTs.
{"title":"Tensegrity metamaterial-based shear band structure for non-pneumatic tires","authors":"Yuling Wei , Fei Pan , Jintao Du , Jinwu Xiang , Yuli Chen","doi":"10.1016/j.finmec.2025.100341","DOIUrl":"10.1016/j.finmec.2025.100341","url":null,"abstract":"<div><div>Non-pneumatic tires (NPTs) represent a revolutionary advancement in the tire industry, owing to their puncture-proof nature and high design flexibility. To achieve both high load-bearing capability and low, evenly distributed ground pressure, the shear band structure of NPTs must balance high compressive stiffness with shear flexibility. To address this challenge, this work proposes a novel shear band structure based on tensegrity metamaterials. By adjusting the stiffness of two types of springs, the proposed shear band enables independent control of its compressive and shear stiffness. The shear band is subsequently integrated with various types of spokes, and the effects of multiple design parameters on the tire’s load-bearing capacity, peak material stress, and contact pressure are systematically analyzed. To achieve performance customization, a Bayesian optimization framework is developed to autonomously explore parameter sets that satisfy performance requirements while minimizing stress and contact pressure. Finally, the feasibility of the tensegrity metamaterial-based shear band design is validated through its successful integration into a four-wheel-drive vehicle model. The proposed shear band offers a new approach for the customized performance and practical application of NPTs.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100341"},"PeriodicalIF":3.5,"publicationDate":"2025-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145623979","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-11-14DOI: 10.1016/j.finmec.2025.100340
Kai Pfitzer , Lucas Rath , Sebastian Kolmeder , Burkhard Corves , Günther Prokop
Friction is an important phenomenon in the modeling of mechanical systems. To represent the dynamic properties of friction, bristle models such as the LuGre model are used mostly in the one-dimensional case. Since friction is a nonlinear phenomenon and the respective frictional degrees of freedom influence each other, independent modeling in the spatial dimensions is physically inadmissible. The two-dimensional description of friction in bristle models proves to be complex and has already been considered in some works, but without intuitive illustration and interpretation. In this paper, an intuitive derivation of the general bristle friction model is presented, summarizing validated existing model derivations. In addition, a geometric interpretation is given using a proposed mechanical equivalence model. Subsequently, all model parameters are discussed, which highlights the potential for extensions and the benefits of flexible parametrization. Based on the general form of the bristle friction model, the special case of the two-dimensional LuGre model is derived. Furthermore, the derived two-dimensional LuGre model is applied in a simple, two-dimensional friction system and the static and dynamic properties are visualized and discussed.
{"title":"A general mechanical formulation of two-dimensional bristle friction models with a focus on the LuGre model and its dynamics","authors":"Kai Pfitzer , Lucas Rath , Sebastian Kolmeder , Burkhard Corves , Günther Prokop","doi":"10.1016/j.finmec.2025.100340","DOIUrl":"10.1016/j.finmec.2025.100340","url":null,"abstract":"<div><div>Friction is an important phenomenon in the modeling of mechanical systems. To represent the dynamic properties of friction, bristle models such as the LuGre model are used mostly in the one-dimensional case. Since friction is a nonlinear phenomenon and the respective frictional degrees of freedom influence each other, independent modeling in the spatial dimensions is physically inadmissible. The two-dimensional description of friction in bristle models proves to be complex and has already been considered in some works, but without intuitive illustration and interpretation. In this paper, an intuitive derivation of the general bristle friction model is presented, summarizing validated existing model derivations. In addition, a geometric interpretation is given using a proposed mechanical equivalence model. Subsequently, all model parameters are discussed, which highlights the potential for extensions and the benefits of flexible parametrization. Based on the general form of the bristle friction model, the special case of the two-dimensional LuGre model is derived. Furthermore, the derived two-dimensional LuGre model is applied in a simple, two-dimensional friction system and the static and dynamic properties are visualized and discussed.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100340"},"PeriodicalIF":3.5,"publicationDate":"2025-11-14","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145578926","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-11-04DOI: 10.1016/j.finmec.2025.100339
Mohammad Javad Zarei , Shahabeddin Hatami , Mojtaba Gorji Azandariani , Mohammad Gholami
The gap in the literature lies in the limited understanding of the mechanical behavior of cylindrical sandwich shells with truss cores (CSSTC), particularly under uniaxial compression and bending loads, and the critical role of shell/core debonding. This study presents a novel finite element-based investigation into the failure mechanisms of cylindrical sandwich shells with truss cores (CSSTCs), emphasizing shell/core debonding under combined bending and compressive loads. Unlike previous studies that commonly assume perfect bonding, this research introduces an innovative adhesive layer between the face sheets and the core, modeled using a cohesive surface contact approach to capture debonding initiation and progression. The novelty of this work lies in systematically evaluating how adhesive stiffness influences critical loads, buckling behavior, and overall structural integrity, offering a realistic simulation of partial bonding conditions. This study numerically investigates the bending and compressive failure modes of cylindrical sandwich shells with truss cores (CSSTCs), considering shell/core debonding. Finite element simulations using ABAQUS software were conducted to analyze buckling modes and critical damage forces. Key factors such as element shape and meshing techniques were evaluated to ensure accurate modeling. A novel method was developed to enhance critical load capacity by integrating an innovative adhesive layer between the cylindrical shells (CSs) and the core, aiming to achieve structural robustness comparable to fully bonded configurations. Aluminum was used as the core and face sheet material in the detailed modeling of sandwich structures. The study employed cohesive surface contact to simulate debonding in the numerical models. Mesh convergence analysis demonstrated the significant influence of mesh orientation and element shape on modeling accuracy and convergence rates. Numerical results revealed buckling modes and critical loads for cylindrical shells and sandwich structures under various loading conditions. Furthermore, the study examined the effect of adhesive stiffness on critical moments during pure bending, highlighting its crucial role in structural performance.
{"title":"Failure mode analysis of cylindrical sandwich shells with truss core considering shell/core debonding under bending/compressive loading","authors":"Mohammad Javad Zarei , Shahabeddin Hatami , Mojtaba Gorji Azandariani , Mohammad Gholami","doi":"10.1016/j.finmec.2025.100339","DOIUrl":"10.1016/j.finmec.2025.100339","url":null,"abstract":"<div><div>The gap in the literature lies in the limited understanding of the mechanical behavior of cylindrical sandwich shells with truss cores (CSSTC), particularly under uniaxial compression and bending loads, and the critical role of shell/core debonding. This study presents a novel finite element-based investigation into the failure mechanisms of cylindrical sandwich shells with truss cores (CSSTCs), emphasizing shell/core debonding under combined bending and compressive loads. Unlike previous studies that commonly assume perfect bonding, this research introduces an innovative adhesive layer between the face sheets and the core, modeled using a cohesive surface contact approach to capture debonding initiation and progression. The novelty of this work lies in systematically evaluating how adhesive stiffness influences critical loads, buckling behavior, and overall structural integrity, offering a realistic simulation of partial bonding conditions. This study numerically investigates the bending and compressive failure modes of cylindrical sandwich shells with truss cores (CSSTCs), considering shell/core debonding. Finite element simulations using ABAQUS software were conducted to analyze buckling modes and critical damage forces. Key factors such as element shape and meshing techniques were evaluated to ensure accurate modeling. A novel method was developed to enhance critical load capacity by integrating an innovative adhesive layer between the cylindrical shells (CSs) and the core, aiming to achieve structural robustness comparable to fully bonded configurations. Aluminum was used as the core and face sheet material in the detailed modeling of sandwich structures. The study employed cohesive surface contact to simulate debonding in the numerical models. Mesh convergence analysis demonstrated the significant influence of mesh orientation and element shape on modeling accuracy and convergence rates. Numerical results revealed buckling modes and critical loads for cylindrical shells and sandwich structures under various loading conditions. Furthermore, the study examined the effect of adhesive stiffness on critical moments during pure bending, highlighting its crucial role in structural performance.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100339"},"PeriodicalIF":3.5,"publicationDate":"2025-11-04","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145528684","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-10-24DOI: 10.1016/j.finmec.2025.100338
Xuefei Ma , Qianqian Zhou , Li Yang , Yichun Zhou
The growth of the thermally grown oxide (TGO), formed during the oxidation of thermal barrier coatings (TBCs) in advanced gas turbine engines, exhibits a pronounced size effect as the thickness approaches its grain size. Addressing the gap in current coupling theories for capturing scale-dependent oxidation behavior, this study further develops an enhanced theoretical framework that integrates large deformation mechanical-thermal-chemical coupling, incorporating strain gradient effects. By utilizing the Green strain as an independent field variable, numerical solutions were obtained using a mixed finite element method. The growth kinetics of the TGO are investigated under isothermal conditions. Numerical results indicate that the strain gradient effect increases the compressive stress within the TGO growth region by 77.8 % and promotes a more uniform stress distribution with increasing scale parameters. Consequently, the growth rate and non-uniform expansion of the TGO are substantially mitigated, as the stress-induced inhibition effect is more effectively utilized. With suppressed non-uniform expansion of the TGO, the susceptibility of the coating to surface wrinkling diminishes with larger scale parameters. This research is instrumental in elucidating the oxidation dynamics of TBCs.
{"title":"A large-deformation mechanical-thermal-chemical coupling model for thermal barrier coatings incorporating strain gradient effects","authors":"Xuefei Ma , Qianqian Zhou , Li Yang , Yichun Zhou","doi":"10.1016/j.finmec.2025.100338","DOIUrl":"10.1016/j.finmec.2025.100338","url":null,"abstract":"<div><div>The growth of the thermally grown oxide (TGO), formed during the oxidation of thermal barrier coatings (TBCs) in advanced gas turbine engines, exhibits a pronounced size effect as the thickness approaches its grain size. Addressing the gap in current coupling theories for capturing scale-dependent oxidation behavior, this study further develops an enhanced theoretical framework that integrates large deformation mechanical-thermal-chemical coupling, incorporating strain gradient effects. By utilizing the Green strain as an independent field variable, numerical solutions were obtained using a mixed finite element method. The growth kinetics of the TGO are investigated under isothermal conditions. Numerical results indicate that the strain gradient effect increases the compressive stress within the TGO growth region by 77.8 % and promotes a more uniform stress distribution with increasing scale parameters. Consequently, the growth rate and non-uniform expansion of the TGO are substantially mitigated, as the stress-induced inhibition effect is more effectively utilized. With suppressed non-uniform expansion of the TGO, the susceptibility of the coating to surface wrinkling diminishes with larger scale parameters. This research is instrumental in elucidating the oxidation dynamics of TBCs.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100338"},"PeriodicalIF":3.5,"publicationDate":"2025-10-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145424848","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-10-21DOI: 10.1016/j.finmec.2025.100337
S․ S. R․ Koloor , A. Farokhi Nejad , N. Yidris , S.M. Sapuan , M.R. Abdullah , M.N. Tamin
Carbon fibers’ exceptional mechanical properties make them the major load-bearing component of CFRP composites, which are rapidly being used in modern aerospace applications. Design of multi-directionally (MD) laminated composite structures for specific operational load requires the exact determination and force analysis of 0°-laminas and their arrangement in the lamina assembly process. The significant property variation between carbon fibers and matrix components indicates that the mechanical behavior of the 0°-laminas is attributed largely to the fiber-bundle at the mesoscale. The elastic properties of fiber have been obtained through standard tests, however, many challenges are encountered in the characterization of fiber damage and fracture processes. In this research, a new experiment is introduced where tensile tests are performed on single edge-notch 0°-CFRP composite monitored by 3D digital image correlation (DIC), to demonstrate the mechanism of deformation and failure and determine the exact elastic-damage properties. A hybrid experimental-computational approach is developed where finite element models representing the experiment, are used to obtain and validate the damage evolution characteristics of fibers in CFRP lamina. In addition, test and simulation results are utilized to describe the mechanism and mechanics of deformation and damage of the composite structure.
{"title":"Elastic-damage characterization of fibre-bundle lamina of CFRP composite through 3D digital image correlation and finite element method","authors":"S․ S. R․ Koloor , A. Farokhi Nejad , N. Yidris , S.M. Sapuan , M.R. Abdullah , M.N. Tamin","doi":"10.1016/j.finmec.2025.100337","DOIUrl":"10.1016/j.finmec.2025.100337","url":null,"abstract":"<div><div>Carbon fibers’ exceptional mechanical properties make them the major load-bearing component of CFRP composites, which are rapidly being used in modern aerospace applications. Design of multi-directionally (MD) laminated composite structures for specific operational load requires the exact determination and force analysis of 0°-laminas and their arrangement in the lamina assembly process. The significant property variation between carbon fibers and matrix components indicates that the mechanical behavior of the 0°-laminas is attributed largely to the fiber-bundle at the mesoscale. The elastic properties of fiber have been obtained through standard tests, however, many challenges are encountered in the characterization of fiber damage and fracture processes. In this research, a new experiment is introduced where tensile tests are performed on single edge-notch 0°-CFRP composite monitored by 3D digital image correlation (DIC), to demonstrate the mechanism of deformation and failure and determine the exact elastic-damage properties. A hybrid experimental-computational approach is developed where finite element models representing the experiment, are used to obtain and validate the damage evolution characteristics of fibers in CFRP lamina. In addition, test and simulation results are utilized to describe the mechanism and mechanics of deformation and damage of the composite structure.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100337"},"PeriodicalIF":3.5,"publicationDate":"2025-10-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145424849","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-10-05DOI: 10.1016/j.finmec.2025.100336
Dong Li, Jun-Jiang Xiong
This paper examines thermo-mechanical coupling behaviours and damage mechanisms of 3D4D (three-dimensional four-directional) braided composites subjected to longitudinal and transverse tensile at room and elevated temperatures. New nonlinear constitution model of 3D braided composites is derived in consideration of thermo-mechanical coupling effect, non-linear shear constitutive relationship of fibre yarn and elastoplastic deformation characteristics of matrix, and novel mixed criterion is then presented based on von-Mises rule, 3D Hashin criterion, B-K energy and quads damage model. After this, an improved progressive damage algorithm is devised for modelling progressive thermo-mechanical coupling damage process of 3D braided composites. Quasi-static longitudinal and transverse tensile tests are respectively performed on 3D4D braided composites at RT (room temperature) and 85 , and nonlinear thermo-mechanical coupling behaviours are analyzed and discussed from experiment results. In order to verify the model and algorithm mentioned previously, a high-fidelity full-scale mesoscale finite element (HFFSMFE) model is generated and integrated with improved algorithm for modelling progressive damage process of 3D4D braided composites subjected to longitudinal and transverse tensile at both temperatures, and numerical predictions agree well with experimental findings, demonstrating the apt and effective usage of new model proposed in the paper.
{"title":"Nonlinear thermo-mechanical coupling behaviours and damage mechanisms of 3D braided composites subjected to longitudinal and transverse tensile at room and elevated temperatures","authors":"Dong Li, Jun-Jiang Xiong","doi":"10.1016/j.finmec.2025.100336","DOIUrl":"10.1016/j.finmec.2025.100336","url":null,"abstract":"<div><div>This paper examines thermo-mechanical coupling behaviours and damage mechanisms of 3D4D (three-dimensional four-directional) braided composites subjected to longitudinal and transverse tensile at room and elevated temperatures. New nonlinear constitution model of 3D braided composites is derived in consideration of thermo-mechanical coupling effect, non-linear shear constitutive relationship of fibre yarn and elastoplastic deformation characteristics of matrix, and novel mixed criterion is then presented based on von-Mises rule, 3D Hashin criterion, B-K energy and quads damage model. After this, an improved progressive damage algorithm is devised for modelling progressive thermo-mechanical coupling damage process of 3D braided composites. Quasi-static longitudinal and transverse tensile tests are respectively performed on 3D4D braided composites at RT (room temperature) and 85 <span><math><mrow><msup><mrow></mrow><mo>∘</mo></msup><mi>C</mi></mrow></math></span>, and nonlinear thermo-mechanical coupling behaviours are analyzed and discussed from experiment results. In order to verify the model and algorithm mentioned previously, a high-fidelity full-scale mesoscale finite element (HFFSMFE) model is generated and integrated with improved algorithm for modelling progressive damage process of 3D4D braided composites subjected to longitudinal and transverse tensile at both temperatures, and numerical predictions agree well with experimental findings, demonstrating the apt and effective usage of new model proposed in the paper.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100336"},"PeriodicalIF":3.5,"publicationDate":"2025-10-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145332612","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-10-03DOI: 10.1016/j.finmec.2025.100335
Chuanqing Chen , Yulong He , Yuli Chen , Guoxing Lu , Ming-Hui Lu , Xin Li
Mechanical metamaterials, with their unique properties, have been increasingly investigated as lightweight, high‑strength impact‑resistant solutions for aerospace, military, transportation, and biomedical applications. In this paper, recent advanced studies in mechanical metamaterials under impact loads are briefly reviewed. On the basis of structural form, four primary types of metamaterials are categorized: mass-spring system, rod/beam-based, plate/shell-based and other specialized types of metamaterials. Additionally, their intended energy-absorption mechanisms and loading-rate‑dependent mechanical responses are discussed. Finally, potential future research directions are proposed, including studies of strain rate and inertial effects, stress wave propagation, localized impact, size effect and multi-scale effect, multifunctional design and AI-assisted on-demand design. This paper highlights key strategies and areas for innovation in the development of next-generation impact-resistant mechanical metamaterials.
{"title":"Impact dynamics of mechanical metamaterials: A short review and perspective","authors":"Chuanqing Chen , Yulong He , Yuli Chen , Guoxing Lu , Ming-Hui Lu , Xin Li","doi":"10.1016/j.finmec.2025.100335","DOIUrl":"10.1016/j.finmec.2025.100335","url":null,"abstract":"<div><div>Mechanical metamaterials, with their unique properties, have been increasingly investigated as lightweight, high‑strength impact‑resistant solutions for aerospace, military, transportation, and biomedical applications. In this paper, recent advanced studies in mechanical metamaterials under impact loads are briefly reviewed. On the basis of structural form, four primary types of metamaterials are categorized: mass-spring system, rod/beam-based, plate/shell-based and other specialized types of metamaterials. Additionally, their intended energy-absorption mechanisms and loading-rate‑dependent mechanical responses are discussed. Finally, potential future research directions are proposed, including studies of strain rate and inertial effects, stress wave propagation, localized impact, size effect and multi-scale effect, multifunctional design and AI-assisted on-demand design. This paper highlights key strategies and areas for innovation in the development of next-generation impact-resistant mechanical metamaterials.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100335"},"PeriodicalIF":3.5,"publicationDate":"2025-10-03","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145266600","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-09-27DOI: 10.1016/j.finmec.2025.100334
Qingliang Zeng , Zhaoji Li , Peng Liu , Naihao Gong , Lirong Wan
Thin-walled tubes with various design strategies as energy absorbers have been widely proposed and applied in the engineering fields. However, the comparison of the crashworthy performance of tubes with various cross-sectional topologies under axial compression remains scarce. In this paper, twelve types of thin-walled tubes (e.g., single-celled, bi-tubular and hierarchical square, hexagonal and circular tubes), which have the identical material, height, apparent area and mass, have been fairly compared. Validation is accomplished through axial quasi-static crushing tests, ensuring the accuracy of the finite element models. The crushing behaviors of all tubes studied are investigated using six crashworthiness indicators. The results show that thin-walled tubes with hierarchical features primarily deform in the preferrable stable deformation mode, with more lobes and higher energy dissipation. Then, hierarchical features can reduce the fluctuations and enhance the load-carrying capacity. In addition, the mean crushing force (MCF) and specific energy absorption (SEA) of bi-tubular tubes also do not increase significantly compared with single-celled tubes. Specifically, the increases in SEA from square tubes to circular tubes for single-celled, bi-tubular and edge-based hierarchical are 65.4 %, 75.0 % and 49.6 %, respectively. Furthermore, all tubes studied are comprehensively evaluated by applying the technique for order preference by similarity to an ideal solution (TOPSIS) method. Considering the effect of dimension, four non-dimensional indicators are selected, namely ESR, EEA, CFE and ULC. EH_C has the best overall performance among all the tubes studied.
{"title":"Axially crashworthy performance of thin-walled tubes with various configurations under the same scale","authors":"Qingliang Zeng , Zhaoji Li , Peng Liu , Naihao Gong , Lirong Wan","doi":"10.1016/j.finmec.2025.100334","DOIUrl":"10.1016/j.finmec.2025.100334","url":null,"abstract":"<div><div>Thin-walled tubes with various design strategies as energy absorbers have been widely proposed and applied in the engineering fields. However, the comparison of the crashworthy performance of tubes with various cross-sectional topologies under axial compression remains scarce. In this paper, twelve types of thin-walled tubes (e.g., single-celled, bi-tubular and hierarchical square, hexagonal and circular tubes), which have the identical material, height, apparent area and mass, have been fairly compared. Validation is accomplished through axial quasi-static crushing tests, ensuring the accuracy of the finite element models. The crushing behaviors of all tubes studied are investigated using six crashworthiness indicators. The results show that thin-walled tubes with hierarchical features primarily deform in the preferrable stable deformation mode, with more lobes and higher energy dissipation. Then, hierarchical features can reduce the fluctuations and enhance the load-carrying capacity. In addition, the mean crushing force (<em>MCF</em>) and specific energy absorption (<em>SEA</em>) of bi-tubular tubes also do not increase significantly compared with single-celled tubes. Specifically, the increases in <em>SEA</em> from square tubes to circular tubes for single-celled, bi-tubular and edge-based hierarchical are 65.4 %, 75.0 % and 49.6 %, respectively. Furthermore, all tubes studied are comprehensively evaluated by applying the technique for order preference by similarity to an ideal solution (TOPSIS) method. Considering the effect of dimension, four non-dimensional indicators are selected, namely <em>ESR, EEA, CFE</em> and <em>ULC</em>. EH_C has the best overall performance among all the tubes studied.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100334"},"PeriodicalIF":3.5,"publicationDate":"2025-09-27","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145227380","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-09-25DOI: 10.1016/j.finmec.2025.100333
Mahdi Ghamari , Pouria Oliazadeh , Mohammad Hossein Farshidianfar
Laser welding is widely adopted for its high speed, precision, and automation capabilities, delivering superior microstructural properties in material joining. However, suboptimal welding parameters can cause defects, necessitating accurate and computationally efficient simulation models. This study introduces a novel simplified numerical model for laser welding that optimizes the prediction of molten pool geometry while minimizing computational cost. By integrating a phase-change model with a calibrated Gaussian heat source, the approach balances accuracy and efficiency, addressing the limitations of complex fluid dynamics models and oversimplified temperature-based simulations. The model was validated against seven experimental cases involving Ti6Al4V and stainless steel 316 L, achieving zero error in melt pool depth prediction and maximum errors in top and bottom widths of <0.2 mm. This computationally efficient model enables rapid parameter optimization, making it ideal for large-scale industrial applications, including residual stress and distortion analysis. By offering a practical alternative to high-cost simulations, this work advances laser welding simulation for precision manufacturing and supports broader adoption in industries such as automotive and railway.
{"title":"Simplified numerical modeling with experimental validation of molten pool geometry in laser welding","authors":"Mahdi Ghamari , Pouria Oliazadeh , Mohammad Hossein Farshidianfar","doi":"10.1016/j.finmec.2025.100333","DOIUrl":"10.1016/j.finmec.2025.100333","url":null,"abstract":"<div><div>Laser welding is widely adopted for its high speed, precision, and automation capabilities, delivering superior microstructural properties in material joining. However, suboptimal welding parameters can cause defects, necessitating accurate and computationally efficient simulation models. This study introduces a novel simplified numerical model for laser welding that optimizes the prediction of molten pool geometry while minimizing computational cost. By integrating a phase-change model with a calibrated Gaussian heat source, the approach balances accuracy and efficiency, addressing the limitations of complex fluid dynamics models and oversimplified temperature-based simulations. The model was validated against seven experimental cases involving Ti6Al4V and stainless steel 316 L, achieving zero error in melt pool depth prediction and maximum errors in top and bottom widths of <0.2 mm. This computationally efficient model enables rapid parameter optimization, making it ideal for large-scale industrial applications, including residual stress and distortion analysis. By offering a practical alternative to high-cost simulations, this work advances laser welding simulation for precision manufacturing and supports broader adoption in industries such as automotive and railway.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100333"},"PeriodicalIF":3.5,"publicationDate":"2025-09-25","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145332611","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
Pub Date : 2025-09-23DOI: 10.1016/j.finmec.2025.100332
Mohsen Mansouri, Mehdi Ganjiani
This study presents an experimental and numerical investigation into the influence of stress triaxiality, Lode angle parameter, and ductile fracture behavior in Al 6061-T6 aluminum alloy. To explore negative stress triaxiality conditions, uniaxial tensile and compressive tests were conducted on geometrically tailored specimens, including dumbbell-shaped and rectangular samples with elliptical curved holes. Negative triaxiality values ranging from –0.355 to –0.554 were successfully achieved. A hybrid experimental–numerical approach was adopted to characterize the fracture behavior. In the numerical approach, the Ganjiani fracture model incorporating damage parameters, was implemented in finite element simulations using Abaqus via custom VUHARD and VUSDFLD subroutines. Comparative analysis of experimental and numerical results revealed good agreement in fracture strain predictions. Numerical evaluations indicated that the fracture occurs at the site where maximum plastic strain is observed. The results confirm that stress triaxiality significantly influences ductile fracture, and notably, the variation in fracture strain exhibits different trends under positive and negative triaxiality conditions.
{"title":"Effect of stress state on the fracture behavior of Al6061-T6 via combined experimental and numerical approaches","authors":"Mohsen Mansouri, Mehdi Ganjiani","doi":"10.1016/j.finmec.2025.100332","DOIUrl":"10.1016/j.finmec.2025.100332","url":null,"abstract":"<div><div>This study presents an experimental and numerical investigation into the influence of stress triaxiality, Lode angle parameter, and ductile fracture behavior in Al 6061-T6 aluminum alloy. To explore negative stress triaxiality conditions, uniaxial tensile and compressive tests were conducted on geometrically tailored specimens, including dumbbell-shaped and rectangular samples with elliptical curved holes. Negative triaxiality values ranging from –0.355 to –0.554 were successfully achieved. A hybrid experimental–numerical approach was adopted to characterize the fracture behavior. In the numerical approach, the Ganjiani fracture model incorporating damage parameters, was implemented in finite element simulations using Abaqus via custom VUHARD and VUSDFLD subroutines. Comparative analysis of experimental and numerical results revealed good agreement in fracture strain predictions. Numerical evaluations indicated that the fracture occurs at the site where maximum plastic strain is observed. The results confirm that stress triaxiality significantly influences ductile fracture, and notably, the variation in fracture strain exhibits different trends under positive and negative triaxiality conditions.</div></div>","PeriodicalId":93433,"journal":{"name":"Forces in mechanics","volume":"21 ","pages":"Article 100332"},"PeriodicalIF":3.5,"publicationDate":"2025-09-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145227377","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}