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【新文速递】2025年4月14日固体力学SCI期刊最新文章

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今日更新:International Journal of Solids and Structures 4 篇,Journal of the Mechanics and Physics of Solids 1 篇,Mechanics of Materials 1 篇

International Journal of Solids and Structures

Numerical study on crack tip fields in liquid crystal elastomers

Qiang Guo, Rong Long, Shengqiang Cai

doi:10.1016/j.ijsolstr.2025.113389

液晶弹性体裂纹尖端场的数值研究

This study presents a numerical investigation into the crack tip fields in liquid crystal elastomers (LCEs) using finite element simulations. LCEs exhibit unique mechanical behaviors, such as soft elasticity and directionally adjustable anisotropy, due to the coupling between the deformation of polymer networks and the rotation of liquid crystal mesogens. The numerical simulations focus on a rectangular LCE plate with a small central crack, subjected to uniform stretching. Simulation results reveal the presence of a uniaxial stress state near the crack tip and a universal stress singularity obeying a power law with an exponent of −1. Along the circumferential direction around the crack tip, the stress distribution exhibits a prominent polarization, with the polarization direction precisely aligned with the initial mesogen orientation. For the mesogen reorientation at the crack tip, two types of mesogen rotation—rigid body rotation with the polymer network and relative rotation due to network stretching—are distinguished. The rigid body rotation is found to cause significant heterogeneity in mesogen orientation at the crack tip, but the relative rotation tends to make the mesogen orientation more uniform, generally aligning with the direction of applied stretch. The final mesogen orientation, determined by the initial orientation and rotation, is closely related to the magnitude of the stress field at the crack tip. These findings provide valuable insights into the fracture behavior of LCEs and can serve as a foundation for future experimental and theoretical studies.

本文采用有限元方法对液晶弹性体裂纹尖端场进行了数值模拟研究。由于聚合物网络的变形和液晶介元的旋转之间的耦合,LCEs表现出独特的力学行为,如软弹性和方向可调的各向异性。数值模拟的重点是一个具有小中心裂纹的矩形LCE板,受到均匀拉伸。模拟结果表明,裂纹尖端附近存在单轴应力状态,应力奇异服从指数为- 1的幂律。沿裂纹尖端周围的周向,应力分布呈现出明显的极化,极化方向与初始细观取向精确对齐。对于裂纹尖端的介观重定向,区分了两种类型的介观旋转——聚合物网络的刚体旋转和网络拉伸引起的相对旋转。研究发现,刚体旋转会导致裂纹尖端细观取向的显著不均匀性,但相对旋转会使细观取向更加均匀,通常与施加拉伸的方向一致。最终的细观取向由初始取向和旋转决定,与裂纹尖端应力场的大小密切相关。这些发现为LCEs的断裂行为提供了有价值的见解,可以为未来的实验和理论研究奠定基础。


Analytical solution for adhesive contact of magneto-electro-elastic composites under an axisymmetric power-law indenter: A Maugis–Dugdale framework

Qing-Hui Luo, Yue-Ting Zhou

doi:10.1016/j.ijsolstr.2025.113391

轴对称幂律压头下磁-电弹性复合材料粘接接触的解析解:一个Maugis-Dugdale框架

Switchable adhesion in response to external stimuli plays a critical role in various applications such as transfer printing, climbing robots and soft gripper. Multiferroic composites can give specific responses to mechanical-electro-magnetic loadings due to their multi-field coupling effects, which offer new routines to achieve tunable adhesion. In this work, the classical Maugis-Dugdale (M−D) adhesion model is extended to address the axisymmetric adhesive contact problem between a multiferroic composite half-space and an axisymmetric power-law indenter with real shape index n. By virtue of the superposition principle and Griffith energy balance, analytical solutions of the physical quantities at the contact surface and the relationships among the indentation force, contact radius and indentation depth for M−D-n model are obtained. The Derjaguin–Muller–Toporov (DMT)-n solutions applicable to multiferroic composites are derived from the corresponding M−D-n solutions as the limiting cases, which are new to literature and acquired in this work for the first time. The effects of the electromagnetic properties and profile of the indenter on adhesion behaviors are discussed. It is found that the electromagnetic properties of the indenter have hardly influence on adhesion behaviors in the absence of electromagnetic loadings, which means that one can replace the multi-field coupling adhesion solutions with the purely elastic adhesion solutions in nanoindentation characterization of multiferroic composites under this circumstance. The profile of the indenter has a prominent effect on the transition behavior from DMT-n solution to JKR-n solution. The adhesion enhancing effect induced by the electromagnetic loadings diminishes with increasing the shape index of the indenter and the magnitude of the generalized Tabor parameter. The results obtained from this work not only lay the theoretical basis for nanoindentation technique in characterizing material properties of multiferroic composites, but also possess potential application value in switchable adhesion.

响应外部刺 激的可切换粘附在各种应用中起着至关重要的作用,例如转移印刷,攀爬机器人和软抓取器。多铁复合材料由于其多场耦合效应,可以对机械-电磁载荷做出特定的响应,这为实现可调粘附提供了新的途径。本文将经典的Maugis-Dugdale (M−D)粘接模型扩展到多铁复合材料半空间与实形状指数n的轴对称幂律压头之间的轴对称粘接接触问题。利用叠加原理和Griffith能量平衡,得到了M−D-n模型的接触面物理量以及压痕力、接触半径和压痕深度之间的关系的解析解。以M−D-n解为极限情况,导出了适用于多铁复合材料的Derjaguin-Muller-Toporov (DMT)-n解,这是文献中首次获得的新解。讨论了压头的电磁特性和形状对粘接性能的影响。研究发现,在没有电磁载荷的情况下,压头的电磁特性对黏附行为几乎没有影响,这意味着在这种情况下,多铁复合材料的纳米压痕表征可以用纯弹性黏附溶液代替多场耦合黏附溶液。压头的形状对DMT-n溶液到JKR-n溶液的过渡行为有显著影响。随着压头形状指数的增大和广义Tabor参数的增大,电磁载荷对压头黏附力的增强作用逐渐减弱。本研究结果不仅为纳米压痕技术表征多铁复合材料的材料性能奠定了理论基础,而且在可切换粘附方面具有潜在的应用价值。


Angle-dependent peeling behavior of compliant nanofilms on planar substrates

Xuebo Yuan

doi:10.1016/j.ijsolstr.2025.113380

平面基底上柔顺纳米膜的角度依赖性剥离行为

The peeling of compliant nanofilms from supporting substrates is essential in mechanical exfoliation techniques, biomimetic adhesives, and nanoelectromechanical systems. Prior to the steady state, the peeling force typically increases in the initial stage and then decreases nonlinearly in the transition stage. However, existing mechanics models rarely capture the effects of the film’s tensile stiffness and peeling angle on these two stages, particularly the initial peeling stiffness and peak peeling force. Though extending a recent model (Yuan et al., 2024) by accurately incorporating the film’s in-plane deformation and arbitrary peeling angle, this work establishes a comprehensive large-deformation model using the energy-variational method. The proposed model effectively predicts the entire peeling process across different peeling angles and is validated by molecular dynamics simulations. For relatively large peeling angle, the film’s tensile stiffness exhibits minor effect on the peeling behavior. The influences of the peeling angle on the peeling process, peeling stiffness, and peak peeling force are analyzed in detail. Through dimensional analysis, an explicit scaling relation for the peak peeling force is derived, accounting for system parameters such as peeling angle, film stiffness, structural parameters, and interfacial properties. This work provides a comprehensive model for the peeling behavior of nanofilm-substrate systems, offering new insights into the atomic-scale interface mechanics of two-dimensional materials.

从支撑基板上剥离柔顺的纳米膜在机械剥离技术、仿生粘合剂和纳米机电系统中是必不可少的。在稳定状态之前,剥落力通常在初始阶段增大,然后在过渡阶段非线性减小。然而,现有的力学模型很少能捕捉到薄膜的拉伸刚度和剥离角度对这两个阶段的影响,特别是初始剥离刚度和峰值剥离力。本文通过对Yuan等人(2024)的最新模型进行扩展,将薄膜的面内变形和任意剥离角度精确地纳入其中,利用能量变分方法建立了一个综合的大变形模型。该模型有效地预测了不同剥离角度下的整个剥离过程,并通过分子动力学模拟进行了验证。当剥离角度较大时,薄膜的拉伸刚度对剥离行为影响较小。详细分析了剥离角度对剥离过程、剥离刚度和剥离峰值力的影响。通过量纲分析,导出了考虑剥离角度、膜层刚度、结构参数和界面性能等系统参数的峰值剥离力的显式标度关系。这项工作为纳米膜-衬底系统的剥离行为提供了一个全面的模型,为二维材料的原子尺度界面力学提供了新的见解。


Optimization and experimental validation of anti-tri chiral lattice metamaterial for broadband vibration suppression

Vahid Tikani, Saeed Ziaei-Rad

doi:10.1016/j.ijsolstr.2025.113384

反三手性晶格超材料宽带振动抑制的优化与实验验证

A key challenge in metamaterials design is to optimize the anti-tri chiral structure with precise and controllable geometry, considering performance criteria. This work proposes a parametric anti-tri-chiral lattice made from Polylactic acid (PLA) polymer to open the wide bandgap for vibration suppression. Experiments and theoretical methods study anti-tri-chiral lattice to analyze the vibration attenuation features of the metamaterial. The band structure was studied in terms of the geometry parameters of the unit cell to investigate the effect of geometry changes on the bandgap size. To ensure the best geometry of the anti-tri-chiral unit cell, an automated optimization process is conducted using MATLAB and COMSOL Multiphysics based on Non-dominated Sorting Genetic Algorithm II (NSGA-II). Two optimization cases were performed with different objectives, and the results indicated that the optimized geometry yields enhanced vibration suppression capabilities and a wide complete bandgap. Finally, the anti-tri-chiral lattice is fabricated using Fused Deposition Molding (FDM), and experimental testing is performed to validate the proposed design.

在考虑性能标准的前提下,优化具有精确和可控几何形状的反三手性结构是超材料设计的一个关键挑战。本文提出了一种由聚乳酸(PLA)聚合物制成的参数化反三手性晶格,以打开宽带隙来抑制振动。实验和理论方法研究了反三手性晶格,分析了超材料的减振特性。从单晶胞的几何参数角度研究了带隙结构,探讨了几何结构变化对带隙大小的影响。为了确保反三手性单元胞的最佳几何形状,基于非支配排序遗传算法II (NSGA-II),利用MATLAB和COMSOL Multiphysics进行了自动化优化过程。采用不同的优化目标进行了两种优化情况,结果表明,优化后的几何结构具有更强的振动抑制能力和更宽的全带隙。最后,采用熔融沉积成型(FDM)技术制备了反三手性晶格,并进行了实验测试以验证所提出的设计。


Journal of the Mechanics and Physics of Solids

Construction of Isotropic Compressible Hyperelastic Constitutive Models Based Solely on Uniaxial Tests

Pengfei Yang, Peidong Lei, Bin Liu, Huajian Gao

doi:10.1016/j.jmps.2025.106150

基于单轴试验的各向同性可压缩超弹性本构模型构建

Constructing constitutive models for compressible soft materials is essential for accurately describing their highly nonlinear, large deformation mechanical behavior and volumetric deformation. However, most existing constitutive models rely on predefined assumptions about the form of the strain energy function. Constructing compressible hyperelastic constitutive models is particularly challenging because, beyond the uniaxial test, it typically requires additional more sophisticated and more costly experiments, such as biaxial, pure shear, and hydrostatic tests. In this paper, we propose an approach to constructing an isotropic compressible hyperelastic constitutive model without assuming a predefined form of the strain energy function. Instead, we derive the strain energy function directly from experimental data. Our method requires only uniaxial tests, significantly simplifying the experimental requirements and costs. This approach is achieved by utilizing the deviatoric-volumetric decomposition of the strain energy function coupled with an interpolation scheme. To validate our proposed approach, we compare our model against traditional compressible constitutive models and well-known experimental data on incompressible rubbers. Additionally, we perform experiments on compressible rubbers, including foamed silicone and foamed EPDM (ethylene propylene diene monomer), for further validation. It is found that our model perfectly predicts the uniaxial test data and accurately predicts mechanical behavior under various other loading conditions. Finally, we discuss strategies for enhancing model accuracy and its ability to decouple uniaxial behavior from compressibility. This decoupling feature is crucial for accurately capturing the distinct mechanical responses associated with different deformation modes, thereby improving the predictive capability of the constitutive model.

建立可压缩软质材料的本构模型是准确描述其高度非线性、大变形力学行为和体积变形的关键。然而,大多数现有的本构模型依赖于关于应变能函数形式的预定义假设。构建可压缩超弹性本构模型尤其具有挑战性,因为除了单轴测试之外,它通常还需要额外的更复杂和更昂贵的实验,如双轴、纯剪切和静水试验。在本文中,我们提出了一种构造各向同性可压缩超弹性本构模型的方法,而不需要假设应变能函数的预定义形式。相反,我们直接从实验数据推导出应变能函数。我们的方法只需要单轴测试,大大简化了实验要求和成本。该方法是利用应变能函数的偏差体积分解与插值方案相结合来实现的。为了验证我们提出的方法,我们将我们的模型与传统的可压缩本构模型和众所周知的不可压缩橡胶的实验数据进行了比较。此外,我们还对可压缩橡胶进行了实验,包括发泡硅胶和发泡EPDM(乙丙二烯单体),以进一步验证。结果表明,该模型能较好地预测单轴试验数据,并能较准确地预测各种载荷条件下的力学行为。最后,我们讨论了提高模型精度及其将单轴行为与可压缩性解耦的能力的策略。这种解耦特性对于准确捕捉与不同变形模式相关的不同力学响应至关重要,从而提高本构模型的预测能力。


Mechanics of Materials

On modeling fracture of soft polymers

Aditya Konale, Vikas Srivastava

doi:10.1016/j.mechmat.2025.105346

软聚合物断裂建模研究

Soft polymers are ubiquitous materials in nature and as engineering materials with properties varying from rate-independent to rate-dependent. Current fracture toughness measures are non-unique for rate-dependent soft materials for varying loading profiles and specimen geometries. Works on modeling fracture in rate-dependent soft polymers are limited to specific pre-cracked geometries. There is no generally agreed-upon model for the fracture of soft polymers. We propose and show that a critical value of stress work can be used as a measure of fracture resistance in soft polymers. We develop a damage model to predict fracture in soft polymers. In the model, the energetic part of the critical stress work is proposed as a damage initiation criterion that has the ability to capture failure surfaces. The damage growth is modeled through a generalized gradient-damage framework. The fracture model is validated for both elastomers and viscous soft polymers by comparing model predictions against experimental results for different materials (ethylene propylene diene monomer - EPDM, EPS25 vitrimer, styrene butadiene rubber - SBR, and polyborosiloxane - PBS), a variety of specimen geometries, and loading conditions. The model can predict key physical phenomena such as brittle and ductile responses and different fracture profiles. The microstructural quantities, such as subchain dissociation energy during the fracture of polymers, can be predicted from the macroscopic model parameters.

软聚合物是自然界中普遍存在的材料,也是具有从速率无关到速率相关特性的工程材料。目前的断裂韧性测量对于速率相关的软材料来说,对于不同的加载剖面和试样几何形状来说,并不是唯一的。对速率相关软聚合物的断裂建模工作仅限于特定的预裂几何形状。对于软聚合物的断裂,目前还没有一个公认的模型。我们提出并证明了应力功的临界值可以作为软聚合物抗断裂性的衡量标准。我们开发了一个损伤模型来预测软聚合物的断裂。在该模型中,临界应力功的能量部分被提出作为一种能够捕捉破坏面的损伤起裂判据。采用广义梯度损伤框架对损伤增长进行建模。通过将模型预测结果与不同材料(乙丙二烯单体EPDM、EPS25玻璃体、丁苯橡胶SBR和聚硼硅氧烷PBS)、各种试样几何形状和加载条件下的实验结果进行比较,验证了弹性体和粘性软聚合物的断裂模型。该模型可以预测脆性和韧性响应以及不同的断裂剖面等关键物理现象。从宏观模型参数可以预测聚合物断裂时的亚链解离能等微观结构量。




来源:复合材料力学仿真Composites FEM
ACTMechanicalSystemMAGNETDeform振动断裂复合材料非线性裂纹理论材料机器人分子动力学仿生试验
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首次发布时间:2025-04-24
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【新文速递】2025年4月18日复合材料SCI期刊最新文章

今日更新:Composite Structures 2 篇,Composites Part A: Applied Science and Manufacturing 4 篇,Composites Part B: Engineering 3 篇,Composites Science and Technology 1 篇Composite StructuresUltra-high temperature mechanical behavior and microstructural evolution of needle-punched carbon/carbon composites under time-varying thermo-mechanical coupling conditionsBoyi Wang, Songhe Meng, Bo Gao, Kunjie Wang, Chenghai Xudoi:10.1016/j.compstruct.2025.119192时变热-力耦合条件下针 刺碳/碳复合材料的超高温力学行为及显微组织演化Carbon/carbon (C/C) composites are extensively employed in the thermal protection systems of hypersonic vehicles, and the precise acquisition of critical process information is vital for the reliable design of such vehicles. Consequently, this research introduces a high-temperature repeated loading testing protocol for needle-punched C/C composites, aimed at characterizing the mechanical behavior of re-entry vehicles in intricate thermal–mechanical coupling environments. Initially, an ultra-high-temperature speckle pattern was prepared using plasma spraying and laser etching techniques, which is suitable for the temperature range of this study (room temperature to 2000 °C). Subsequently, under time-varying temperature and load conditions, the local strain field and tensile properties were investigated. In the single-loading test, at 1500 °C, the stress–strain curve slope decreased by up to 58 %. In the cyclic loading test, at 2000 °C, the slope increased by up to 46 % with the number of cycles, while the specimen strength decreased by up to 27.1 % compared to the standard test. By examining fracture morphology and internal structure at both macroscopic and microscopic scales, the study elucidated how interfacial performance and the level of graphitization contribute to the tensile behavior. The results indicate that as the number of loading cycles increases, the stress–strain curve slope is primarily influenced by interfacial properties and carbon fiber graphitization, with each playing a dominant role at different loading stages. Additionally, tensile strength decreases with the rise in loading cycles, positively correlating with interfacial performance and inversely with carbon fiber graphitization.碳/碳(C/C)复合材料广泛应用于高超声速飞行器的热防护系统中,关键工艺信息的精确获取对于高超声速飞行器的可靠设计至关重要。因此,本研究引入了针刺C/C复合材料的高温重复加载测试方案,旨在表征再入飞行器在复杂热-力学耦合环境中的力学行为。首先,采用等离子喷涂和激光刻蚀技术制备了超高温散斑图,该散斑图适用于本研究的温度范围(室温至2000 °C)。然后,在时变的温度和载荷条件下,研究了局部应变场和拉伸性能。在单加载试验中,在1500 °C时,应力-应变曲线斜率下降高达58 %。在2000 °C循环加载试验中,与标准试验相比,随着循环次数的增加,边坡增加高达46 %,而试件强度下降高达27.1 %。通过在宏观和微观尺度上检查断裂形态和内部结构,该研究阐明了界面性能和石墨化水平如何影响拉伸行为。结果表明:随着加载循环次数的增加,应力-应变曲线斜率主要受界面性能和碳纤维石墨化程度的影响,且在不同加载阶段,界面性能和碳纤维石墨化程度分别起主导作用;拉伸强度随加载次数的增加而降低,与界面性能呈正相关,与碳纤维石墨化成反比。Multi-body dynamic transfer matrix modeling and validation for full-scale wind turbine blades in biaxial fatigue testing systemsYi Ma, Aiguo Zhou, Yutian Zhu, Jinlei Shi, Shiwen Zhao, Jianzhong Wudoi:10.1016/j.compstruct.2025.119205全尺寸风电叶片双轴疲劳试验系统多体动态传递矩阵建模与验证Continuous advancements in wind turbine technology, driven by the pursuit of increased power generation and extended blade dimensions, have heightened the demand for reliable biaxial fatigue testing of full-scale blades. Such testing is critical for evaluating long-term structural integrity under realistic loading conditions. This study presents a novel multi-body dynamic transfer matrix methodology to address the modeling and analysis challenges inherent in full-scale biaxial testing systems for large wind turbine blades. The proposed approach discretizes the heterogeneous blade structure into beam elements and employs transfer matrix theory to derive system matrices encompassing spatial beam dynamics, mass distribution, damping characteristics, and elastic properties. Through the systematic formulation of the dynamic transfer equations and subsequent numerical solutions of the characteristic equations, this method enables comprehensive vibration analysis of the multi-body test system. Comparative validation through finite element simulations and experimental measurements demonstrates that the equivalent model achieves prediction discrepancies below 7% across multiple blade configurations. The developed framework provides an effective multibody transfer matrix model for investigating vibration characteristics and bending moment distributions in blade fatigue testing systems, establishing theoretical foundations for dynamic characterization and optimized design of full-scale biaxial fatigue testing platforms.风力涡轮机技术的不断进步,在追求更大的发电量和更大的叶片尺寸的驱动下,提高了对全尺寸叶片可靠的双轴疲劳测试的需求。这种测试对于评估实际荷载条件下的长期结构完整性至关重要。本研究提出了一种新的多体动态传递矩阵方法,以解决大型风力涡轮机叶片全尺寸双轴测试系统固有的建模和分析挑战。该方法将非均匀叶片结构离散为梁单元,并利用传递矩阵理论推导出包含梁空间动力学、质量分布、阻尼特性和弹性特性的系统矩阵。该方法通过系统地建立动力传递方程和随后的特征方程数值解,实现了对多体试验系统的全面振动分析。通过有限元模拟和实验测量的对比验证表明,等效模型在多种叶片配置下的预测误差低于7%。该框架为研究叶片疲劳试验系统的振动特性和弯矩分布提供了有效的多体传递矩阵模型,为全尺寸双轴疲劳试验平台的动态表征和优化设计奠定了理论基础。Composites Part A: Applied Science and ManufacturingIn-plane compression behaviors of cedarwood-inspired cores and composite sandwich structuresZhi Sun, Xin Zhou, Ruishuang Li, Yawen Zhang, Shanshan Shidoi:10.1016/j.compositesa.2025.108933杉木芯材与复合材料夹层结构的面内压缩特性The microstructures of biological tissues can effectively guide the design of composite honeycomb sandwich structures. In this study, a cedarwood-inspired honeycomb core was proposed. In-plane compression tests were conducted on honeycomb cores and sandwich specimens to analyze the deformation and failure mechanisms of the cedarwood-inspired core and to examine their effects on the mechanical properties and failure modes of the sandwich structures. The cedarwood-inspired microstructure altered the load-transfer mechanism within the core, converting concentrated loads into distributed loads and restricting the expansion of unit cell deformations in the core. Experimental results indicated that the deformation and failure modes of the cores and sandwich specimens were modified, and the mechanical properties were significantly improved using the proposed cedarwood-inspired honeycomb cores. Specifically, the peak load of the cedarwood-inspired sandwich is 31.52% higher. Additionally, a theoretical prediction model was developed to determine Young’s modulus and peak load of the cedarwood-inspired core, offering valuable guidance for the design of future honeycomb cores.生物组织的微观结构可以有效地指导复合材料蜂窝夹层结构的设计。在本研究中,提出了一种以雪松木为灵感的蜂窝芯。通过对蜂窝芯和夹层试件进行面内压缩试验,分析雪松木芯的变形破坏机理,研究其对夹层结构力学性能和破坏模式的影响。杉木结构改变了岩心内的荷载传递机制,将集中荷载转化为分布荷载,限制了岩心内单胞变形的扩展。实验结果表明,采用雪松木蜂窝岩心可以改变岩心和夹层试件的变形破坏模式,并显著改善其力学性能。具体来说,以雪松木为灵感的三明治的峰值负荷高出31.52%。此外,建立了一个理论预测模型来确定雪松木蜂窝芯的杨氏模量和峰值荷载,为未来蜂窝芯的设计提供了有价值的指导。Low-velocity impact response of carbon/epoxy laminates with interlaminar hybrid toughening via core–shell-rubber particles and non-woven thermoplastic fibre veilsMehmet Çağatay Akbolat, Sheng Wang, Kali Babu Katnam, Prasad Potluri, Constantinos Soutisdoi:10.1016/j.compositesa.2025.108944核-壳-橡胶复合增韧碳/环氧复合材料与热塑性无纺布纤维膜的低速冲击响应Advanced composites (e.g. carbon fibre-reinforced epoxies) have been increasingly used in lightweight, critical applications such as aerospace, renewable energy and defence industries due to their excellent mechanical properties including high specific strength, stiffness and fatigue properties. However, the inherent brittleness of polymer composites makes them vulnerable to low-velocity out-of-plane impact loading, threatening their structural integrity. In this context, enhancing the low-velocity impact resistance of composite laminates is crucial for maintaining their structural integrity and reliability throughout their service life. Therefore, this study explores the low-velocity out-of-plane impact resistance of composite laminates (i.e. consisting of the unidirectional non-crimp carbon fibre fabrics and low-viscous two-part epoxy resin) toughened with core–shell rubber (CSR) particles and thermoplastic veils. The CSR particles varying from 0.1 to 3µm and Polyphenylene Sulfide (PPS) fibre veils with a fibre diameter of 9 µm were used to achieve non-hybrid and hybrid toughening. The impact response of the composite laminates, manufactured with vacuum-assisted resin infusion and out-of-autoclave curing, were characterised with drop-weight low-velocity impact testing in two energy ranges: near the delamination threshold (i.e. 2 J, 3 J, 4 J) and over a broader range (i.e. 2.5 J, 5 J, 7.5 J, 10 J). The results show that the toughening mechanisms derived from the hybrid use of PPS veils and CSR particles effectively enhance the impact resistance of composite laminates up to the delamination threshold. Additionally, the hybrid approach significantly reduces the projected damage area. However, beyond the delamination threshold, the influence of these toughening mechanisms on the impact properties is found to be limited.先进复合材料(如碳纤维增强环氧树脂)由于其优异的机械性能,包括高比强度,刚度和疲劳性能,已越来越多地用于轻量化,关键应用,如航空航天,可再生能源和国防工业。然而,聚合物复合材料固有的脆性使其容易受到低速面外冲击载荷的影响,威胁其结构完整性。在这种情况下,增强复合材料层压板的抗低速冲击能力对于在其整个使用寿命中保持其结构完整性和可靠性至关重要。因此,本研究探讨了用核壳橡胶(CSR)颗粒和热塑性薄膜增韧复合层压板(即由单向无卷曲碳纤维织物和低粘性双组分环氧树脂组成)的低速抗面外冲击性能。采用0.1 ~ 3µm的CSR颗粒和直径为9µm的聚苯硫醚(PPS)纤维膜实现非杂化增韧和杂化增韧。采用真空辅助树脂注入和非高压釜固化制造的复合材料层合板的冲击响应,通过两种能量范围的落锤低速冲击测试进行了表征:在脱层阈值附近(即2 J、3 J、4 J)和更宽的范围(即2.5 J、5 J、7.5 J、10 J)。结果表明,PPS膜和CSR颗粒混合使用的增韧机制有效地提高了复合材料层合板的抗冲击能力,直至脱层阈值。此外,混合方法大大减少了预计的损伤面积。然而,在脱层阈值之外,这些增韧机制对冲击性能的影响是有限的。Enhancing interlaminar fracture toughness in CFRP composites using ethanolamine-coated CNT sheetsManoj Sehrawat, Mamta Rani, Karishma Jain, Sonu Rani, Sony Bharadwaj, Bhanu Pratap Singh, Raj Ladani, Brian G. Falzondoi:10.1016/j.compositesa.2025.108958乙醇胺涂层碳纳米管增强CFRP复合材料层间断裂韧性Traditional interleaving of carbon nanotube (CNT) sheets in CFRP composites often leads to poor resin infiltration, resulting in lower interlaminar fracture toughness. This study proposes a novel strategy to modify CNT sheets with non-covalent amine groups to enhance their interaction with the polar epoxy matrix, thereby improving wettability and infiltration. CFRP composites containing amine-modified CNT sheets exhibited a remarkable 206% increase in Mode I fracture toughness due to stronger interlaminar interactions and enhanced fibre bridging. The use of these amine-modified CNT sheets induced the transfer of nanotubes onto the carbon fibre (CF) surface, resulting in nanomodified CFs with increased active sites for matrix bonding, resulting in increased fibre bridging between the delaminated plies. The mode II fracture toughness values show a slight reduction (8.2%) with the use of ethanolamine coated CNT (EACNT) interleaves, as the toughened interlayer does not allow the crack to traverse through it, resulting in a shorter crack path. Nonetheless, this strategy offers a promising advancement towards the use of CNT sheet interleaves for the effective enhancement of CFRP composite fracture toughness.CFRP复合材料中传统的碳纳米管(CNT)片间交错排列往往导致树脂渗透性差,导致层间断裂韧性较低。本研究提出了一种用非共价胺基修饰碳纳米管片的新策略,以增强其与极性环氧基的相互作用,从而提高润湿性和渗透性。含有胺改性碳纳米管片的CFRP复合材料由于层间相互作用增强和纤维桥接增强,其I型断裂韧性提高了206%。使用这些胺改性碳纳米管片诱导纳米管转移到碳纤维(CF)表面,导致纳米改性碳纤维具有增加的基质键合活性位点,从而增加了分层层之间的纤维桥接。使用乙醇胺涂层碳纳米管(EACNT)交织层,II型断裂韧性值略有降低(8.2%),因为增韧的夹层不允许裂纹穿过它,导致更短的裂纹路径。尽管如此,该策略为使用碳纳米管片交错层有效增强CFRP复合材料断裂韧性提供了一个有希望的进展。Enhanced interfacial strength in carbon-nanotubes-reinforced Al matrix composites via an interface substitution strategyWeiwei Zhou, Zhenxing Zhou, Mingqi Dong, Yuchi Fan, Keiichi Shirasu, Go Yamamoto, Naoyuki Nomuradoi:10.1016/j.compositesa.2025.108955 通过界面取代策略提高碳纳米管增强Al基复合材料的界面强度The foremost concern when fabricating carbon nanotube (CNTs)-reinforced Al matrix composites is achieving appropriate interfacial bonding while avoiding intrinsic structural damage. In this study, an interface substitution strategy was developed for replacing the CNT-Al interface with a sandwiched CNT-ceramic-Al interface, thereby enhancing interfacial connections. A uniform, continuous SiO2 layer was deposited on the CNT surface via a sol–gel process, followed by powder metallurgy routines to fabricate SiO2@CNTs/Al composites, in which the CNTs exhibited minimal structural damage and remained well-dispersed without interfacial reactions. An in situ pullout test demonstrated a high interfacial strength of 32.5 MPa for the SiO2@CNT-Al interface, attributed to the enhanced residual compressive stress and interfacial wettability. Consequently, the composite strength was significantly enhanced with CNTs addition, aligning well with predictions from the shear lag model. This interface substitution strategy underscored the feasibility of tuning the CNT-metal interfacial states and highlighted the potential for designing advanced nanocarbon/Al composites.在制备碳纳米管增强铝基复合材料时,最重要的问题是在避免固有结构损伤的同时实现适当的界面结合。在本研究中,开发了一种界面替代策略,将CNT-Al界面替换为夹在cnt -陶瓷- al界面,从而增强界面连接。通过溶胶-凝胶法在碳纳米管表面沉积均匀、连续的SiO2层,然后采用粉末冶金方法制备SiO2@CNTs/Al复合材料,其中碳纳米管的结构损伤最小,并且在没有界面反应的情况下保持良好的分散。现场拉拔试验表明,由于残余压应力和界面润湿性的增强,SiO2@CNT-Al界面的界面强度高达32.5 MPa。因此,CNTs的加入显著提高了复合材料的强度,这与剪切滞后模型的预测结果一致。这种界面替代策略强调了调整碳纳米管-金属界面状态的可行性,并强调了设计先进纳米碳/铝复合材料的潜力。Composites Part B: EngineeringAn environmentally friendly superhydrophobic coating with high-temperature resistance, UV resistance, and abrasion resistance was fabricated on carbon fiber board via an aqueous phase polymer dispersion systemQian Su, Kangli Yang, Zhiqing Yuan, Cancheng Li, Shoutong Meng, Xuyu Long, Rui Hedoi:10.1016/j.compositesb.2025.112533 采用水相聚合物分散体系在碳纤维板上制备了一种具有耐高温、耐紫外线、耐磨损的环保型超疏水涂层Aiming at the problems of carbon fiber board (CFB), which is not waterproof and has poor UV resistance, a superhydrophobic coating with UV resistance and high-temperature resistance was innovatively prepared on CFB using an aqueous-phase polymer dispersion system by a highly efficient spraying method. The whole preparation system is highly environmentally friendly and safe. The results showed that the superhydrophobic carbon fiber board (SKCFB) could resist UV up to 85 h, could withstand high temperatures up to 300 °C, and had a water contact angle (WCA) of 159°. In addition, the abrasion resistance of SKCFB is 140 and 180 cycles under the action of 800 grit and 1200 grit sandpaper, respectively, for a load of 100 g, and 110 cycles under the action of 600 grit sandpaper. When carrying a load of 500 g, the 600 mesh, 800 mesh, and 1200 mesh sandpaper can be used for 40, 60, and 80 cycles of abrasion resistance, respectively. Compared with other samples of the same type, this SKCFB is simpler to prepare, has a greener and safer preparation route, and has better performance, plus the ability to control the appearance color as desired. This study provides a novel green, simple, and fast strategy for preparing superhydrophobic coatings on CFBs. At the same time, it opens a new path for preparing superhydrophobic coatings and enhances their application in industry.针对碳纤维板(CFB)不防水、抗紫外线能力差的问题,采用高效喷涂方法,采用水相聚合物分散体系在CFB上创新性地制备了一种耐紫外线、耐高温的超疏水涂层。整个制备系统非常环保和安全。结果表明,该超疏水碳纤维板(SKCFB)抗UV时间长达85 h,耐高温达300℃,水接触角(WCA)为159°。此外,在100 g载荷下,SKCFB在800砂纸和1200砂纸作用下的耐磨性分别为140次和180次,在600砂纸作用下的耐磨性为110次。承载500g载荷时,600目、800目、1200目砂纸可分别进行40、60、80次的耐磨性循环。与其他同类型样品相比,该SKCFB制备更简单,制备路线更环保,更安全,性能更好,并且可以根据需要控制外观颜色。本研究为在cfb上制备超疏水涂层提供了一种绿色、简单、快速的新方法。同时,为制备超疏水涂料开辟了新的途径,提高了超疏水涂料的工业应用。Advancing Aerospace Maintenance: Thermochromic Liquid Crystal Coating Method for Skin-to-Core Disbond Detection in CFRP Honeycomb StructuresM. Sun, D. Wowk, P.R. Underhill, T.W. Krausedoi:10.1016/j.compositesb.2025.112516推进航空航天维护:用于CFRP蜂窝结构表面到核心剥离检测的热致变色液晶涂层方法A novel Non-Destructive Evaluation (NDE) method for aerospace maintenance is introduced, utilizing advanced Thermochromic Liquid Crystal (TLC) ink to detect skin-to-core disbonds in carbon fiber-reinforced polymer (CFRP) honeycomb structures subjected to low-velocity impacts, representing a state-of-the-art integration of functional materials (TLC) with essential aerospace maintenance practices. Traditional NDE methods for detecting disbonds in aerospace structures often necessitate skilled technicians and sophisticated equipment. In contrast, the current study demonstrates that the proposed TLC coating method provides a straightforward, real-time detection technique that can serve as a preliminary or substitute inspection method. The detection and characterization results using the TLC coating method are rigorously evaluated through comparison with Forward-Looking Infrared (FLIR) by employing a high-performance thermal imaging camera. Results demonstrated that the TLC coating method achieved the same detection limits as FLIR thermography, with measurements of the disbond size differing by no more than 5% between the two methods. A new heating method, Communicative Heating Thermography (CHT), was introduced for use with the TLC coating method in field applications without the need for post-processing, or expensive equipment. CHT enabled operators to dynamically adjust heat application based on real-time feedback from the TLC coating, optimizing disbond detection. This method was successfully implemented by untrained operators with an accuracy of 100%.介绍了一种用于航空航天维修的新型无损评估(NDE)方法,该方法利用先进的热致色液晶(TLC)墨水来检测碳纤维增强聚合物(CFRP)蜂窝结构在低速撞击下的皮肤到核心的脱落,代表了功能材料(TLC)与航空航天维修实践的最先进集成。传统的无损检测方法通常需要熟练的技术人员和复杂的设备来检测航空航天结构的剥离。相比之下,目前的研究表明,所提出的TLC涂层方法提供了一种直接、实时的检测技术,可以作为初步或替代的检测方法。采用高性能热像仪与前视红外(FLIR)进行对比,对TLC涂层法的检测和表征结果进行了严格评价。结果表明,TLC涂层法与FLIR热成像法具有相同的检出限,两种方法测量的脱粘尺寸相差不超过5%。介绍了一种新的加热方法,通信加热热成像(CHT),可与TLC涂层方法一起用于现场应用,无需后处理或昂贵的设备。CHT使作业者能够根据TLC涂层的实时反馈动态调整热应用,优化剥离检测。该方法由未经训练的操作人员成功实现,准确率为100%。Hexagonal boron nitride (h-BN) “a miracle in white”: An emerging two-dimensional material for the advanced powered electronics and energy harvesting applicationChinmoy Kuila, Animesh Maji, Naresh Chandra Murmu, Tapas Kuiladoi:10.1016/j.compositesb.2025.112531 六方氮化硼(h-BN)“白色奇迹”:一种新兴的二维材料,用于先进的电力电子和能量收集应用The growing demand for batteries or other compact electronics received considerable attention because of its high energy density and excellent power-to-mass ratio. However, obstacles such as inconsistent temperature distribution, inefficient energy storage, and sluggish release rates have emerged. Effective heat dissipation is required for optimum efficiency and durability of electrical devices. Thus, it is critical to develop thermally conductive hybrid fillers for improved heat management in such systems. Two-dimensional (2D) hexagonal boron nitride (h-BN), also known as "white graphene," encounters conceivable uses in electronics and energy devices due to the broad bandgap (∼5.5 eV), superior thermal endurance, high thermal conductivity (TC), and exceptional dielectric properties. The anisotropic conductivity of BN causes a reduction in cross-plane TC, which is a fundamental concern for its practical deployments. Therefore, developing a unique technique and structural engineering remedy for enhancing BN's cross-plane TC could be achievable. The main focus of this article is to explore the phonon-phonon scattering phenomena, mechanisms, and insights to design h-BN-based composites with good cross-plane TC and electrical insulation. The article summarizes the significance of 2D h-BN in several sectors, including electronic packaging, energy (e.g., thermal energy management and conversion), and batteries/supercapacitors. These topics highlight cutting-edge filler properties and the innovative design of 2D h-BN. Finally, the challenges and perspectives of developing potential thermal interface materials (TIMs) are highlighted. Our insights offer an initial glimpse into future studies on fabricating advanced TIMs in an appropriate filler structure configuration for optimal cooling of electronic/optoelectronic devices.对电池或其他紧凑型电子产品日益增长的需求受到了相当大的关注,因为它具有高能量密度和优异的功率质量比。然而,诸如温度分布不一致、能量储存效率低下和释放速率缓慢等障碍已经出现。有效的散热是电气设备获得最佳效率和耐用性的必要条件。因此,开发导热混合填料以改善此类系统的热管理是至关重要的。二维(2D)六方氮化硼(h-BN),也被称为“白色石墨烯”,由于宽带隙(~ 5.5 eV),优异的热耐久性,高导热性(TC)和特殊的介电性能,在电子和能源设备中遇到了可以想象的用途。BN的各向异性电导率导致了跨平面TC的降低,这是其实际部署的一个基本问题。因此,开发一种独特的技术和结构工程补救措施来增强BN的跨平面TC是可以实现的。本文的重点是探讨声子-声子散射现象、机制以及设计具有良好跨平面TC和电绝缘的h- bn基复合材料的见解。本文总结了二维氢氮化硼在电子封装、能源(如热能管理和转换)和电池/超级电容器等几个领域的意义。这些主题突出了前沿填料的性能和2D h-BN的创新设计。最后,指出了开发潜在热界面材料的挑战和前景。我们的见解为未来在适当的填料结构配置中制造先进的TIMs以实现电子/光电器件的最佳冷却提供了初步的研究。Composites Science and TechnologyPhysical crosslinking optimized high-temperature capacitive energy storage of polyetherimide nanocomposites with ultralow C60 particlesWenjie Huang, Mengyu Xiao, Baoquan Wan, Zhonghua Xiang, Yuchao Li, Yong Chae Jung, Jun-Wei Zhadoi:10.1016/j.compscitech.2025.111194 物理交联优化的超低C60聚醚酰亚胺纳米复合材料高温电容储能The extreme operating environments of film capacitors have created an urgent need for a new generation of polymer dielectric materials. Polymer-based composites are a more efficient option in terms of outstanding performance and large-scale industrialized production. Herein, C60 is selected as a functional filler to be combined with commercial polyetherimide (PEI) through electrostatic interactions to construct polymer nanocomposites (C60/PEI). Ultralow-filled C60/PEI nanocomposites achieve the comprehensive improvement of electrical, thermal and mechanical performance due to the physical cross-linking points acted by C60 particles. C60 shows a strong ability to inhibit electron transfer due to the unique zero-dimensional cage structure and high electron affinity, which reduces the conduction loss at high temperatures. Theoretical and experimental results show that the introduction of trace amounts of C60 particles into PEIs constructs stable carrier traps and significantly improves the high-temperature energy storage characteristics. The dielectric permittivity and breakdown strength are increased from 3.24 and 447 MV/m for PEI to 3.45 and 520 MV/m for the optimal C60/PEI nanocomposite at 150 °C, respectively. Consequently, the optimal C60/PEI nanocomposite achieves a discharged energy density (Ud) of 3.69 J/cm3 at 150 °C, which is higher than 2.65 J/cm3 of PEI. This provides a convenient and effective strategy to synergistically improve the comprehensive performance of polymer nanocomposite films for high-temperature energy storage applications.薄膜电容器的极端工作环境对新一代聚合物介电材料产生了迫切的需求。聚合物基复合材料在突出的性能和大规模工业化生产方面是一个更有效的选择。本文选择C60作为功能性填料,通过静电相互作用与商用聚醚酰亚胺(PEI)结合,构建聚合物纳米复合材料(C60/PEI)。超低填充C60/PEI纳米复合材料由于C60粒子作用的物理交联点,实现了电学、热学和力学性能的全面提高。C60由于其独特的零维笼结构和高的电子亲和性,表现出很强的抑制电子转移的能力,从而降低了高温下的传导损失。理论和实验结果表明,引入微量C60粒子构建了稳定的载流子陷阱,显著改善了PEIs的高温储能特性。在150℃下,C60/PEI纳米复合材料的介电常数和击穿强度分别从PEI的3.24和447 MV/m提高到C60/PEI的3.45和520 MV/m。因此,最佳的C60/PEI纳米复合材料的放电能量密度Ud在150℃时为3.69 J/cm3,高于PEI的2.65 J/cm3。这为协同提高聚合物纳米复合薄膜的综合性能提供了一种方便有效的策略。 来源:复合材料力学仿真Composites FEM

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