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【新文速递】2024年2月21日固体力学SCI期刊最新文章

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今日更新:Journal of the Mechanics and Physics of Solids 1 篇,Thin-Walled Structures 8 篇

Journal of the Mechanics and Physics of Solids

Fluid-injection control on energy partitioning during the earthquake cycle

Maryam Alghannam, Hector Gomez, Ruben Juanes

doi:10.1016/j.jmps.2024.105580

注入流体对地震周期中能量分配的控制

During an earthquake, the elastic energy stored in the Earth is released as frictional energy and radiated energy in the form of seismic waves. The partitioning of energy released during an earthquake gives an indication of the overall size of the earthquake and its potential for damage to man-made structures. Here, we perform an energy analysis of fluid-injection-induced earthquakes using a single-degree-of-freedom spring poroslider and rate-and-state friction. We show that seismic radiation can be modeled within the single-degree-of-freedom spring-slider by adding a radiation damping term. We then use it to study fluid injection and assess its effects on the energy partitioning during induced and triggered earthquakes. We find that: (1) seismic efficiency, stress drop, and total slip are directly influenced by the rate of increase in pore pressure, (2) the ratio of elastic energy stored in the skeleton to injection energy is low and is influenced by the rate of fluid injection, (3) seismic injection efficiency is also low and is lower for induced earthquakes compared to triggered ones, and (4) fluid injection leads to bigger and potentially more damaging earthquakes overall.

地震时,地球中储存的弹性能量会以摩擦能和地震波的形式释放出来。地震过程中释放的能量分区可显示地震的总体规模及其对人造结构造成破坏的可能性。在此,我们使用单自由度弹簧孔滑块和速率与状态摩擦对注入流体引发的地震进行了能量分析。我们证明,地震辐射可以通过添加辐射阻尼项在单自由度弹簧滑块中建模。然后,我们用它来研究流体注入,并评估其对诱发地震和触发地震期间能量分配的影响。我们发现(1) 地震效率、应力下降和总滑移直接受孔隙压力增加速率的影响;(2) 骨架中存储的弹性能量与注入能量的比率较低,且受流体注入速率的影响;(3) 地震注入效率也较低,且诱发地震的注入效率低于触发地震;(4) 流体注入会导致更大、潜在破坏性更强的地震。


Thin-Walled Structures

Dynamic stiffness method and CUF-based component-wise theories applied to free vibration analysis of solid beams, thin-walled structures and reinforced panels

Xiao Liu, Alfonso Pagani, Erasmo Carrera, Xiang Liu

doi:10.1016/j.tws.2024.111707

应用于实心梁、薄壁结构和加固板自由振动分析的动态刚度法和基于 CUF 的分量-分项理论

In this paper, an exact dynamic stiffness formulation using higher-order theories with displacement variables only is presented and subsequently used to investigate the free vibration characteristics of solid beams, thin-walled structures and reinforced panel structures. In essence, higher-order displacement fields are developed by using the Carrera unified formulation (CUF), and by discretizing the cross-section kinematics with bilinear, cubic and fourth-order Lagrange polynomials. In particular, the component-wise (CW) approach based on Lagrange expansion is applied in which the solid part and thin-walled part are considered as two independent components that can be assembled. The principle of virtual displacements is used to derive the governing differential equations and the associated natural boundary conditions. An exact dynamic stiffness matrix is then developed by relating the amplitudes of harmonically varying loads to those of the responses. The explicit terms of the dynamic stiffness matrices are also presented. The Wittrick–Williams algorithm of the dynamic stiffness method (DSM) is applied with the explicit expressions of the J0 count for beam elements under all above support conditions. In return, there is no need to refine the element in the DSM, and thus, it becomes immensely efficient. The accuracy and efficiency of the proposed methodology are extensively assessed for different solid beams, thin-walled structures and reinforced panels and the results are compared with those appearing in published literature and also checked by 3D finite element (FE) solutions.

本文提出了一种仅使用位移变量的高阶理论的精确动态刚度公式,并随后用于研究实心梁、薄壁结构和加固板结构的自由振动特性。从本质上讲,高阶位移场是通过使用卡雷拉统一公式(CUF)以及使用双线性、三次方和四阶拉格朗日多项式对横截面运动学进行离散化而形成的。特别是采用了基于拉格朗日展开的分量法(CW),将实心部分和薄壁部分视为两个可组装的独立分量。虚拟位移原理用于推导控制微分方程和相关的自然边界条件。然后,通过将谐波变化载荷的振幅与响应的振幅联系起来,得出精确的动态刚度矩阵。动态刚度矩阵的显式项也一并列出。动态刚度法(DSM)的 Wittrick-Williams 算法与上述所有支撑条件下梁元素的 J0 数值的明确表达式一起应用。反过来,在 DSM 中不需要对元素进行细化,因此变得非常高效。针对不同的实心梁、薄壁结构和加固板,对所建议方法的准确性和效率进行了广泛评估,并将结果与已发表文献中的结果进行了比较,同时还通过三维有限元 (FE) 解决方案进行了检验。


Mechanical response of a novel square dome shell with bistable behavior: improved analytical method and empirical model

Zhuangzhuang Li, Xuelin Li, Zhuoyu Guo, Yue Zhou, Jiahui Lin, Zonglai Mo, Jun Li

doi:10.1016/j.tws.2024.111722

具有双稳态行为的新型方形穹顶壳的机械响应:改进的分析方法和经验模型

In this study, a novel square dome-shaped shell with a fascinating bistable behavior is proposed, which is able to quickly switch to a new stable configuration within its elastic range under a certain load, due to its elastic instability. Compared to most circular shells currently studied, it is easier to arrange multiple structures in three-dimensional space to obtain multistable responses. Numerical and experimental methods were adopted for the study of the mechanical response of the square shell, and main influence parameters were also investigated. In addition, an improved piecewise fitting method is introduced to establish an empirical formula for predicting the mechanical response of bistable shells, which can be used to guide the design of bistable shells. Finally, two types of metamaterials, uniaxial compressible metamaterials and triaxial compressible metamaterials, are successfully designed according to the above theory, the typical behaviors of which are studied via simulations. This novel structure presented in this paper has broad application prospects in the fields of energy absorption and programmable deformation structures.

本研究提出了一种具有迷人双稳态行为的新型方形穹顶壳,由于其弹性不稳定性,在一定载荷作用下,能够在弹性范围内快速切换到新的稳定构型。与目前研究的大多数圆壳相比,它更容易在三维空间中排列多个结构,从而获得多稳响应。采用数值和实验方法研究了方壳的力学响应,并对主要影响参数进行了研究。此外,还引入了一种改进的分片拟合方法,建立了预测双稳态壳力学响应的经验公式,可用于指导双稳态壳的设计。最后,根据上述理论成功设计了两种超材料,即单轴可压缩超材料和三轴可压缩超材料,并通过仿真研究了其典型行为。本文介绍的这种新型结构在能量吸收和可编程变形结构领域具有广阔的应用前景。


Design of Cold-Formed Z-shaped purlin-to-rafter connections subject to pull-through failure

Haripriya Karthikeyan, Bishal Naik, Mahendrakumar Madhavan

doi:10.1016/j.tws.2024.111725

受拉穿失效影响的冷成型 Z 形檩条与椽子连接设计

The current study is focused on understanding the pull-through behaviour of Z-Shaped Cold-Formed Steel (CFS) purlin-to-rafter connection. A total of forty tests were conducted using small-scale testing methods to investigate the influence of parameters such as thickness, depth, and flange width of the purlin section along with the size of the screw head diameter. The results indicated that the test specimens exhibited two modes of pull-through failure (i) rupture-type failure and (ii) bearing-type failure. A transition from rupture-type to bearing-type was observed with an increase in thickness from 1 mm to 3 mm. Both the failure modes were accompanied by tilting of the screw due to eccentricity in the applied load for Z-Shaped purlins. A full-field measurement approach called Three-Dimensional Digital Image Correlation (3D-DIC) technique was employed to better understand the failure mechanism. The DIC strain contours adequately captured the tilting of the screw that can be attributed to the increased strain and out-of-plane deformation at the vicinity of the screw head. A comparison of the test with existing design standards indicates that the design guidelines are unconservative for Z-shaped purlin sections. A modified design equation is proposed to determine the pull-through capacity of Z-shaped purlin-to-rafter connection. Further, reliability study was carried out to determine the resistance and safety factors for the preliminary design equations proposed.

当前研究的重点是了解 Z 形冷弯型钢(CFS)檩条与椽子连接的拉穿行为。研究人员使用小规模测试方法进行了总共 40 次测试,以研究檩条截面的厚度、深度和翼缘板宽度等参数以及螺钉头直径大小的影响。结果表明,试样表现出两种拉穿失效模式(i)断裂型失效和(ii)承载型失效。随着厚度从 1 毫米增加到 3 毫米,可观察到从断裂型向轴承型的过渡。对于 Z 形檩条来说,这两种失效模式都伴随着螺杆因外加载荷偏心而倾斜。为了更好地了解失效机理,我们采用了一种名为三维数字图像相关(3D-DIC)技术的全场测量方法。DIC 应变轮廓图充分捕捉到了螺杆的倾斜,这可归因于螺杆头部附近的应变增加和平面外变形。将测试结果与现有设计标准进行比较后发现,对于 Z 形檩条截面而言,设计准则并不严谨。我们提出了一个修改后的设计方程,以确定 Z 型檩条与椽子连接的抗拉能力。此外,还进行了可靠性研究,以确定初步设计方程的阻力和安全系数。


A two-direction cross-iteration solution for in-plane vibrations of thin-walled composite plates with a simplified explicit vibration mechanical model

Lin Zhao, Yuan Liu, Xibin Cao, Zhongxi Shao, Xuan Zhang, Qingyang Deng, Chenhao Sun

doi:10.1016/j.tws.2024.111728

用简化的显式振动力学模型解决薄壁复合板平面内振动的双向交叉迭代问题

For the fine and high reliability design of advanced precision engineering structures, this work presents an analytically cross-iteration method for in-plane vibrations analysis of thin-walled composite plates, the single-layer and laminated structures both involved. The governing equations and corresponding boundary conditions are derived adopting Rayleigh’s principle, in which the governing partial differential equations are transferred into ordinary differential equations. The most important advantage of this method lies in the fact that the explicit eigenvalue equations and mode functions are obtained with only a series of four-by-four matrices by simplifying boundary conditions in the two-direction cross-iteration procedures. Accuracy of the present method is verified by comparison with the previous studies and the finite element method in natural characteristics solutions, and convergence analysis on the single-layer orthotropic plates and composite laminates reveals the high efficiency and stability. Finally, the effects of boundary conditions, ply orientation angles, stacking sequences, aspect ratios and stiffness ratios on the in-plane natural characteristics are investigated. The extensive results presented in this work for the first time can be taken as the benchmarks data compared with other methods.

为实现先进精密工程结构的精细化和高可靠性设计,本研究提出了一种分析交叉迭代法,用于薄壁复合材料板的面内振动分析,包括单层结构和层状结构。利用雷利原理推导出控制方程和相应的边界条件,并将控制偏微分方程转换为常微分方程。该方法最重要的优点在于,通过简化双向交叉迭代程序中的边界条件,只需一系列四乘四矩阵即可获得显式特征值方程和模态函数。通过与前人的研究和自然特性求解中的有限元法进行比较,验证了本方法的准确性,对单层正交板和复合层压板的收敛分析表明了本方法的高效性和稳定性。最后,研究了边界条件、层间取向角、堆叠顺序、纵横比和刚度比对平面内自然特性的影响。本研究首次提出的大量结果可作为与其他方法比较的基准数据。


Experimental and numerical investigations of damage and ballistic limit velocity of CFRP laminates subject to harpoon impact

Wei Zhao, Zhaojun Pang, Mingxiao Wang, Peng Li, Zhonghua Du

doi:10.1016/j.tws.2024.111732

受鱼叉撞击的 CFRP 层压板损伤和弹道极限速度的实验和数值研究

The harpoon is a space debris capture mechanism with strong adaptability to targets. In this paper, experiments and finite element models are used to study the harpoon impact on carbon fiber laminate. Firstly, a harpoon penetration gas gun experiment was designed to obtain the damage and ballistic limit velocity of carbon fiber laminates. Then finite element modeling and numerical simulation of the impact on the laminate were carried out using the user-defined VUMAT subroutine in ABAQUS, focusing on the ballistic limit velocity change, damage evolution of the laminate and energy absorption of the laminate when the harpoon penetrates the laminate obliquely at a specific angle. The results showed that compared with vertical penetration, the ballistic limit velocity of harpoon increased by 3.2%, 9.6% and 24.3% respectively under 15°, 30° and 45° oblique penetration conditions; and with the increase of harpoon impact angle, the damage of laminates gradually tended to occur on one side of the projection of harpoon on laminates; while in terms of energy absorption, the energy absorption of laminates for the same angle tended to a constant value as the launch velocity increased.

鱼叉是一种空间碎片捕获装置,对目标具有很强的适应性。本文利用实验和有限元模型研究了鱼叉对碳纤维层压板的影响。首先,设计了鱼叉穿透气 枪实验,以获得碳纤维层压板的损伤和弹道极限速度。然后使用 ABAQUS 中用户自定义的 VUMAT 子程序对层压板的冲击进行有限元建模和数值模拟,重点研究了鱼叉以特定角度斜穿透层压板时,层压板的弹道极限速度变化、损伤演化和能量吸收。结果表明,与垂直穿透相比,在 15°、30° 和 45°斜穿透条件下,鱼叉的弹道极限速度分别增加了 3.2%、9.6% 和 24.3%;随着鱼叉撞击角度的增加,层压板的损伤逐渐趋向于鱼叉在层压板上投影的一侧;而在能量吸收方面,随着发射速度的增加,相同角度下层压板的能量吸收趋向于恒定值。


Multi-objective optimization design of a new non-uniform rectangular honeycomb sandwich panel

Xuanhe Luo, Gang Li, Zeng Meng

doi:10.1016/j.tws.2024.111729

新型非均匀矩形蜂窝夹芯板的多目标优化设计

Honeycomb sandwich panels have a wide range of applications in aerospace, marine and energy industry due to their high stiffness-to-weight ratio. In this study, a new non-uniform rectangular honeycomb core is presented to promote its material utilization ratio. The non-uniform wall of honeycomb core is described using Bezier curves, and the effective elastic constants are obtained by both the geometric equivalent method and the strain energy-based homogenization method. To analyze the bending and buckling behaviors of the sandwich panel, the parabolic shear deformation theory is adopted, and the governing equations are derived by employing Hamilton's principle. Then, the closed-form solutions of bending and buckling responses of the non-uniform rectangular honeycomb sandwich panel are derived. Furthermore, multi-objective design formulations are established, with the objectives of minimizing the weight and deflection, and maximizing the critical buckling load. Illustrative examples demonstrate that the non-uniform design of the honeycomb core can remarkably increase the material utilization rate and improve the mechanical performance of sandwich panels.

蜂窝夹芯板具有很高的刚重比,因此在航空航天、航海和能源行业有着广泛的应用。本研究提出了一种新型非均匀矩形蜂窝芯,以提高其材料利用率。利用贝塞尔曲线描述了蜂窝芯的非均匀壁,并通过几何等效法和基于应变能的均质化法获得了有效弹性常数。为了分析夹芯板的弯曲和屈曲行为,采用了抛物线剪切变形理论,并利用汉密尔顿原理推导了控制方程。然后,推导出了非均匀矩形蜂窝夹芯板弯曲和屈曲响应的闭式解。此外,还建立了以重量和挠度最小化以及临界屈曲载荷最大化为目标的多目标设计公式。示例表明,蜂窝芯的非均匀设计可显著提高材料利用率,改善夹芯板的机械性能。


A comparative study on failure mechanisms of open-hole and filled-hole composite laminates: Experiment and numerical simulation

Di Zhang, Jin Zhou, Jizhen Wang, Wenxin Zhang, Zhongwei Guan

doi:10.1016/j.tws.2024.111730

关于开孔和填充孔复合材料层压板失效机理的比较研究:实验与数值模拟

The strength of composites with open holes (OH) and filled holes (FH) is a critical factor in determining mechanical allowances for engineering design. This study employs both experimental and numerical analyses to investigate the mechanical behaviour of composite laminates subjected to open-hole tension (OHT) and open-hole compression (OHC), filled-hole tension (FHT) and filled-hole compression (FHC). A progressive damage model (PDM) has been developed to predict the load-carrying capacity of both OH and FH laminates, with deviations lower than 6 % in comparison to the corresponding experimental results. Results indicate that OHC/FHC laminates experience more pronounced damage compared to OHT/FHT laminates prior to the maximum load. Additionally, delamination in FHC laminates is significantly reduced compared to OHC laminates. In comparison to OHT/OHC laminates, the presence of a filled bolt increases the maximum load of FHT/FHC laminates by 10.8 % and 36.0 %, respectively, due to relieving the stress concentration near the hole. Moreover, a higher contact friction coefficient between the bolt and laminate leads to a higher maximum load, particularly for FHC laminates, as the increased friction effectively hinders the matrix crack propagation. These findings provide valuable insights for assisting the design of composite structures.

带有开孔(OH)和填充孔(FH)的复合材料的强度是确定工程设计机械余量的关键因素。本研究通过实验和数值分析来研究复合材料层压板在受到开孔拉伸(OHT)和开孔压缩(OHC)、填充孔拉伸(FHT)和填充孔压缩(FHC)作用时的机械性能。建立的渐进损伤模型(PDM)可预测 OHC 和 FHC 复合材料的承载能力,与相应的实验结果相比,偏差小于 6%。结果表明,与 OHT/FHT 层压板相比,OHC/FHC 层压板在最大载荷之前经历了更明显的损坏。此外,与 OHC 层压板相比,FHC 层压板的分层现象明显减少。与 OHT/OHC 层压板相比,填充螺栓的存在使 FHT/FHC 层压板的最大载荷分别增加了 10.8% 和 36.0%,这是由于孔附近的应力集中得到了缓解。此外,螺栓与层压板之间的接触摩擦系数越大,最大载荷就越大,尤其是对于 FHC 层压板,因为摩擦力的增加会有效阻碍基体裂纹的扩展。这些发现为复合材料结构的设计提供了宝贵的启示。


The competition between buckling and stress failure of degraded composite cylindrical shell under combined axial compression and external pressure loads

W.M. Mahdy, Linjuan Wang, Fengrui Liu, Libin Zhao

doi:10.1016/j.tws.2024.111731

轴向压缩和外部压力联合载荷下降解复合材料圆柱壳体屈曲与应力破坏之间的竞争

When thin-walled composite cylindrical shells are subjected to combined loads, not only will they buckle, but they could fail under overstressing. Buckling-failure and stress-failure are two types of failure that compete mutually, and if one of them occurs, the structure loses its ability to carry the load. However, there is a lack of study, and very little attention was paid to the competitive-failure of the composite cylindrical shells under combined loads. To bridge this research gap, a competitive failure analysis framework of degraded composite cylindrical shells exposed to combined axial compression and external pressure loads was developed, considering the nonlinear buckling-failure interacting curve approach for buckling-failure analysis and the Tsai-Wu failure criterion for stress-failure analysis. The material degradation model was adopted to modify the properties of the failed ply based on two degrading philosophies. The proposed framework agrees well with the published results. Extensive parametric studies are accomplished and presented to detect the failure mode of composites. For material parametric study, the variation of material properties does not significantly affect the shape of the normalized buckling-failure interacting curve, while it appreciably affects the behavior of the stress-failure interacting curve. Moreover, it is found that as the proportions of the longitudinal compressive strength to longitudinal modulus and transverse tensile strength to transverse modulus of composite materials increase, the tendency for buckling-failure increases; otherwise, stress-failure happens. For a geometric parametric study, decreasing the radius-to-thickness ratio leads to an increase in the shape of the buckling-failure interacting curve and the possibility of stress-failure.

当薄壁复合材料圆柱形壳体承受联合载荷时,不仅会发生屈曲,而且可能在过应力作用下失效。屈曲失效和应力失效是两种相互竞争的失效类型,如果其中一种失效发生,结构就会丧失承载能力。然而,目前对复合材料圆柱形壳体在组合载荷作用下的竞争失效还缺乏研究,关注度也很低。为了弥补这一研究空白,我们建立了承受轴向压缩和外部压力联合载荷的降解复合材料圆柱壳竞争失效分析框架,在屈曲失效分析中考虑了非线性屈曲失效交互曲线方法,在应力失效分析中考虑了蔡武失效准则。根据两种降解原理,采用材料降解模型来修改失效层的属性。所提出的框架与已公布的结果非常吻合。为检测复合材料的失效模式,完成并介绍了广泛的参数研究。在材料参数研究方面,材料特性的变化对归一化屈曲-失效交互曲线的形状没有显著影响,但对应力-失效交互曲线的行为有明显影响。此外,研究还发现,当复合材料的纵向抗压强度与纵向模量、横向抗拉强度与横向模量的比例增加时,屈曲失效的趋势也会增加;反之,则会发生应力失效。在几何参数研究中,减小半径与厚度之比会导致屈曲-失效交互曲线的形状和应力-失效的可能性增加。




来源:复合材料力学仿真Composites FEM
ACTMechanicalAbaqusDeform振动断裂复合材料非线性航空航天ADS裂纹理论材料控制螺栓
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首次发布时间:2024-11-06
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【新文速递】2024年2月24日复合材料SCI期刊最新文章

今日更新:Composite Structures 3 篇,Composites Part A: Applied Science and Manufacturing 2 篇,Composites Part B: Engineering 3 篇,Composites Science and Technology 1 篇Composite StructuresSmall-dependent nonlinear analysis of functionally graded triply periodic minimal surface nanoplatesP. Phung-Van, P.T. Hung, Chien H. Thaidoi:10.1016/j.compstruct.2024.117986功能分级三周期最小表面纳米板的小依赖非线性分析This paper introduces an effective and simple approach to analyze functionally graded triply periodic minimal surface (FG-TPMS) nanoplates, taking advantage of a novel nonlocal strain gradient nonlinear analysis. TPMS has recently gained attention as an extraordinary solution for constructing structures, drawing inspiration from natural architectures. It offers remarkable features, including high interconnectivity porous architectures, smooth surfaces, and the ability to achieve mathematically controllable geometry features. However, the extensive potential and benefits of TPMS structures have not been fully explored in current research. Hence, this study aims to address this limitation and unlock new possibilities for FG-TPMS nanoplates. Three patterns of FG-TPMS nanoplates, namely Primitive (P), Gyroid (G), and I-gragh and Wrapped Package-graph (IWP), are utilized in this investigation. The proposed model effectively incorporates the nonlocal,strain gradient and nonlinear effects into nanoplate structures. It enables a comprehensive understanding of the mechanisms responsible for both reducing and enhancing stiffness in the nanoplate by fine-tuning the nonlocal and strain gradient parameters. This research offers promising prospects for future design and optimization, providing a robust approach to address the intricate nonlinear behavior observed in FG-TPMS nanoplates.本文利用新颖的非局部应变梯度非线性分析方法,介绍了一种分析功能分级三周期最小表面(FG-TPMS)纳米板的有效而简单的方法。最近,TPMS 从自然建筑中汲取灵感,作为一种构造结构的非凡解决方案而备受关注。它具有显著的特点,包括高互联性多孔结构、光滑表面以及实现数学可控几何特征的能力。然而,目前的研究尚未充分挖掘 TPMS 结构的广泛潜力和优势。因此,本研究旨在解决这一局限性,为 FG-TPMS 纳米板开启新的可能性。本研究采用了三种 FG-TPMS 纳米板的模式,即原始(P)、陀螺(G)和 I-gragh and Wrapped Package-graph (IWP)。所提出的模型有效地将非局部、应变梯度和非线性效应纳入了纳米板结构。通过微调非局部和应变梯度参数,该模型能够全面了解降低和增强纳米板刚度的机制。这项研究为未来的设计和优化提供了广阔的前景,为解决在 FG-TPMS 纳米板中观察到的错综复杂的非线性行为提供了可靠的方法。Fiber-level modeling of 3D braided preforms using virtual braiding methodXi Liao, Yanan Jiao, Junbo Xie, Li Chendoi:10.1016/j.compstruct.2024.117988利用虚拟编织法进行三维编织预成型的纤维级建模High fidelity geometry models of the preforms are essential in mechanical property analysis for composite materials. The paper presents a virtual braiding method to generate digital material twins of 3D braided preforms. The four-step 3D braiding process is simulated based on the concept of virtual fiber and according to the rule of yarn movement. Fiber-level models of the preform are constructed which display the micro-scale architectures explicitly, including compressive deformations of yarn cross-sections and variations of yarn paths. The Micro-CT test is employed to investigate the internal fiber structures of 3D braided preform and quantitatively verify the accuracy of the proposed modeling method. Influence of the braiding parameters, such as yarn tension and arrangement angle in the initial state on geometric parameters of the preform is then investigated.预型件的高保真几何模型对于复合材料的机械性能分析至关重要。本文介绍了一种虚拟编织方法,用于生成三维编织预型件的数字材料双胞胎。根据虚拟纤维的概念和纱线运动规律,模拟了四步三维编织过程。构建的预型件纤维级模型可清晰显示微尺度结构,包括纱线横截面的压缩变形和纱线路径的变化。利用 Micro-CT 测试研究了三维编织预成型的内部纤维结构,并定量验证了所提出的建模方法的准确性。然后研究了初始状态下纱线张力和排列角度等编织参数对预型件几何参数的影响。Flexural performance of reinforced concrete beams strengthened using near-surface-mounted carbon-fiber-reinforced polymer bars: Effects of bonding patternsJ.B. Lv, D.J. Lin, Bing Fu, S.H. Liu, Z.J. Handoi:10.1016/j.compstruct.2024.117985使用近表面安装的碳纤维增强聚合物条加固的钢筋混凝土梁的挠曲性能:粘结模式的影响The near-surface-mounted (NSM) fiber-reinforced polymer (FRP) technique is effective for enhancing the load carrying capacity of strengthened reinforced concrete (RC) beams. However, this technique significantly reduces the deformability of strengthened RC beams. To overcome this, the present study combines the NSM strengthening method with the partial bonding technique: the strengthening FRP reinforcement is partially bonded onto the concrete substrate). Six full-scale 4.3 m long RC beams strengthened with NSM FRPs using various bonding patterns were tested. The results indicated that mechanical interlocking grooves slightly improve the load carrying capacity, but have a negligible effect on the deformability of the strengthened beams. A decrease in the bond length increased deformability by 27.2 %, with only a 7.6 % drop in load capacity compared to that of the beam with full bonding. An advanced finite element model was developed and validated to confirm an optimal bond length of 930 mm for maximum flexural performance.近表面安装(NSM)纤维增强聚合物(FRP)技术可有效提高加固钢筋混凝土(RC)梁的承载能力。然而,这种技术大大降低了加固后 RC 梁的变形能力。为了克服这一问题,本研究将 NSM 加固方法与部分粘结技术相结合:将加固 FRP 钢筋部分粘结在混凝土基材上)。采用不同粘结模式的 NSM FRP 加固了六根长 4.3 米的全尺寸 RC 梁,并对其进行了测试。结果表明,机械互锁槽可略微提高承载能力,但对加固梁变形能力的影响微乎其微。与完全粘结的梁相比,粘结长度的减少使变形能力提高了 27.2%,而承载能力仅下降了 7.6%。开发并验证了一种先进的有限元模型,以确认最佳粘接长度为 930 毫米,从而实现最大抗弯性能。Composites Part A: Applied Science and ManufacturingRecycling CF/PEEK offcut waste from laser assisted tape placement: Influence of overlaps and gapsAswani Kumar Bandaru, Thomas Anderson, Paul M. Weaverdoi:10.1016/j.compositesa.2024.108104回收激光辅助胶带贴装产生的 CF/PEEK 废料:重叠和间隙的影响A recycling method for waste CF/PEEK prepreg tapes is proposed that uses offcuts from laser assisted tape placement (LATP) processing, without shredding, grinding or further cutting. Laminates (using the prepreg waste) representing different configurations were manufactured considering overlaps and gaps reflecting observed defects in LATP. Interlaminar shear strengths (ILSS) with 0° fibre (Parallel) and bending strength for 90° fibre (Normal) directions were measured. The parallel samples with 3 mm overlap had the highest ILSS (100.3 MPa) while the 2 mm gapped samples had the lowest ILSS (58.7 MPa). The Normal samples failed at the surface due to matrix-dominated failure providing bending strengths between 44.0 MPa and 82.1 MPa. Failure mechanisms were identified similar to that of non-recycled composites reported in the literature (50–120 MPa), indicating that the recycled prepreg tapes retained approximately 84 % of the ILSS of the highest reported values.本文提出了一种废 CF/PEEK 预浸料带的回收方法,该方法使用激光辅助贴带 (LATP) 加工过程中产生的边角料,无需粉碎、研磨或进一步切割。考虑到反映 LATP 中观察到的缺陷的重叠和间隙,制造了代表不同结构的层压板(使用预浸料废料)。测量了 0° 纤维方向(平行)的层间剪切强度(ILSS)和 90° 纤维方向(正常)的弯曲强度。重叠 3 毫米的平行样品的层间剪切强度最高(100.3 兆帕),而间隙为 2 毫米的样品的层间剪切强度最低(58.7 兆帕)。正常样品由于基质主导的失效而在表面失效,弯曲强度介于 44.0 兆帕和 82.1 兆帕之间。失效机制与文献报道的非回收复合材料的失效机制(50-120 兆帕)相似,表明回收预浸带保留了最高报道值约 84% 的 ILSS。Mechanical and interfacial analysis of 3D-printed two-matrix continuous carbon fibre composites for enhanced structural performanceFei Liu, Shenru Wang, Wuxiang Zhang, Xilun Ding, Eleonora Ferraris, Jan Ivensdoi:10.1016/j.compositesa.2024.108105增强结构性能的 3D 打印双基质连续碳纤维复合材料的力学和界面分析Two-matrix continuous carbon fibre composites are recognized for enhancing structural and mechanical properties. However, a comprehensive investigation into their interfacial behaviour and potential has yet to be undertaken. Based on the 3D printing process, this study uses experimental and simulation techniques to analyse the mechanical and interfacial performance across multiple scales. The flexure properties under different processing parameters are studied at the macro level. Meso and micro-structural characterization are evaluated by scanning electron microscopy, optical microscopy and molecular dynamics simulation. The disparities in simulations and experimental results are attributed to macroscopic defects and reinforcement volume fraction. This yields insights into strategies for optimising performance, culminating in a comprehensive understanding of the fracture mechanism of two-matrix continuous carbon fibre composites. Our study provides an approach to creating and analysing other systems with multiple matrix composites and enabling new engineering applications for composites.双基体连续碳纤维复合材料被认为可以提高结构和机械性能。然而,对其界面行为和潜力的全面研究尚未开展。本研究以三维打印工艺为基础,采用实验和模拟技术分析了多种尺度的机械和界面性能。从宏观层面研究了不同加工参数下的挠曲性能。通过扫描电子显微镜、光学显微镜和分子动力学模拟评估了中观和微观结构特征。模拟和实验结果的差异归因于宏观缺陷和增强体体积分数。这使我们对优化性能的策略有了深入的了解,最终对双基体连续碳纤维复合材料的断裂机制有了全面的认识。我们的研究为创建和分析其他多基体复合材料系统提供了一种方法,并使复合材料的新工程应用成为可能。Composites Part B: EngineeringFibre orientation distribution function mapping for short fibre polymer composite components from low resolution/large volume X-ray computed tomographyRobert M. Auenhammer, Anuj Prajapati, Kaldon Kalasho, Lars P. Mikkelsen, Philip J. Withers, Leif E. Asp, Renaud Gutkindoi:10.1016/j.compositesb.2024.111313通过低分辨率/大容积 X 射线计算机断层扫描绘制短纤维聚合物复合材料的纤维取向分布函数图Short glass fibre injection moulded composites, used in interior and exterior automotive parts, are exposed to complex stress states, for example during a crash. As the fibre scale dominates the composite’s material properties, numerical models need to account for the local fibre orientation. In recent years, mould flow simulation results have been exploited to predict the fibre orientations for finite element models, albeit with limited accuracy. Alternatively, X-ray computed tomography can be used to directly image and analyse fibre orientations. Traditionally, achieving the necessary resolution to image individual fibres restricts the imaging to small regions of the component. However, this study takes advantage of recent advancements in imaging and image analysis to overcome this limitation. As a result, it introduces, for the first time, a reliable, fast, and automated fibre orientation mapping for a full component based on image analysis on a single fibre level; even for cases where the pixel size is significantly larger than the fibre diameter. By scanning at lower resolutions, a drastically larger volume of interest can be achieve. The resulting fibre orientation analysis and mapping algorithm, based on X-ray computed tomography, is well matched to the level of information required for automotive crash modelling with a standard element-size of a few millimetres. The entire process, encompassing image acquisition, image analysis and fibre orientation mapping, can be directly integrated in an industrial full component application in a matter of hours.用于汽车内外饰件的短玻璃纤维注塑复合材料会面临复杂的应力状态,例如在碰撞过程中。由于纤维尺度主导着复合材料的材料特性,因此数值模型需要考虑局部纤维取向。近年来,人们利用模流模拟结果来预测有限元模型的纤维取向,尽管精确度有限。另外,X 射线计算机断层扫描也可用于直接成像和分析纤维取向。传统上,要达到成像单个纤维所需的分辨率,成像范围只能局限于部件的小区域。然而,本研究利用成像和图像分析领域的最新进展来克服这一限制。因此,该研究首次在单根纤维层面的图像分析基础上,为整个组件引入了可靠、快速和自动化的纤维方向映射;即使在像素尺寸明显大于纤维直径的情况下也是如此。通过低分辨率扫描,可以获得更大的感兴趣体积。由此产生的基于 X 射线计算机断层扫描的纤维方向分析和绘图算法,完全符合汽车碰撞建模所需的信息水平,其标准元素尺寸仅为几毫米。整个过程包括图像采集、图像分析和纤维取向绘图,可在数小时内直接集成到工业全部件应用中。Architected flexible syntactic foams: Additive manufacturing and reinforcing particle driven matrix segregationHridyesh Tewani, Megan Hinaus, Mayukh Talukdar, Hiroki Sone, Pavana Prabhakardoi:10.1016/j.compositesb.2024.111315结构化柔性合成泡沫:增材制造和增强粒子驱动的基质分离Polymer syntactic foams are transforming materials that will shape the future of next-generation aerospace and marine structures. When manufactured using traditional processes, like compression molding, syntactic foams consist of a solid continuous polymer matrix reinforced with stiff hollow particles. However, polymer matrix segregation can be achieved during the selective laser sintering process with thermoplastic polyurethane (TPU). It is uncertain what role hollow particles play in forming this matrix segregation and its impact on the corresponding mechanical properties of syntactic foams. We show that the size of the hollow particles controls the internal microscale morphology of matrix segregation, leading to counter-intuitive macroscale mechanical responses. Particles with diameters greater than the gaps between the cell walls of the segregated matrix get lodged between and in the walls, bridging the gaps in the segregated matrix and increasing the stiffness of syntactic foams. In contrast, particles with smaller diameters with higher particle crushing strength get lodged only inside the cell walls of the segregated matrix, resulting in higher densification stresses (energy absorption). We show that stiffness and densification can be tuned while enabling lightweight syntactic foams. These novel discoveries will aid in facilitating functional and lightweight syntactic foams for cores in sandwich structures.聚合物合成泡沫是一种变革性材料,它将塑造下一代航空航天和海洋结构的未来。在使用压缩成型等传统工艺制造时,合成泡沫由固态连续聚合物基体和硬质空心颗粒组成。然而,在热塑性聚氨酯(TPU)的选择性激光烧结过程中,聚合物基质会发生偏析。目前还不确定空心颗粒在形成这种基质偏析中起到什么作用,以及它对合成泡沫相应机械性能的影响。我们的研究表明,中空颗粒的大小控制着基质离析的内部微观形态,从而导致与直觉相反的宏观机械响应。直径大于离析基质细胞壁间隙的颗粒会嵌入细胞壁之间和细胞壁内,从而弥合离析基质的间隙,增加合成泡沫的刚度。相反,直径较小、颗粒破碎强度较高的颗粒只能嵌入离析基质的细胞壁内,从而导致较高的致密化应力(能量吸收)。我们的研究表明,在实现轻质合成泡沫的同时,还可以调整刚度和致密性。这些新发现将有助于促进功能性轻质合成泡沫在夹层结构中的核心应用。A Novel machine learning model to design historical-independent health indicators for composite structuresMorteza Moradi, Ferda C. Gul, Dimitrios Zarouchasdoi:10.1016/j.compositesb.2024.111328 设计与历史无关的复合材料结构健康指标的新型机器学习模型Developing comprehensive health indicators (HIs) for composite structures encompassing various damage types is challenging due to the stochastic nature of damage accumulation and uncertain events (like impact) during operation. This complexity is amplified when striving for HIs independent of historical data. This paper introduces an AI-driven approach, the Hilbert transform-convolutional neural network under a semi-supervised learning paradigm, to designing reliable HIs (fulfilling requirements, referred to as 'fitness'). It exclusively utilizes current guided wave data, eliminating the need for historical information. Ensemble learning techniques were also used to enhance HI quality while reducing deep learning randomness. The fitness equation is refined for dependable comparisons and practicality. The methodology is validated through investigations on T-single stiffener CFRP panels under compression-fatigue and dogbone CFRP specimens under tension-fatigue loadings, showing high performance of up to 93% and 81%, respectively, in prognostic criteria.由于损伤累积的随机性和运行期间的不确定事件(如撞击),为包含各种损伤类型的复合材料结构制定全面的健康指标(HIs)具有挑战性。在寻求独立于历史数据的健康指标时,这种复杂性会进一步放大。本文介绍了一种人工智能驱动的方法,即半监督学习范式下的希尔伯特变换-卷积神经网络,用于设计可靠的 HI(满足要求,称为 "适配性")。它完全利用当前的导波数据,无需历史信息。此外,还使用了集 合学习技术来提高 HI 质量,同时减少深度学习的随机性。为了实现可靠的比较和实用性,对适度方程进行了改进。通过对压缩疲劳下的 T 型单加强筋 CFRP 面板和拉伸疲劳载荷下的狗骨 CFRP 试样进行研究,验证了该方法,结果表明其在预后标准方面的性能分别高达 93% 和 81%。Composites Science and TechnologyA novel one-step eco-friendly dipping system for PA66 fiber/rubber composites with excellent interfacial adhesion and its adhesion mechanismChaojun Wang, Xuewen Cheng, Wei Huang, Bing Yu, Nanying Ning, Ming Tiandoi:10.1016/j.compscitech.2024.110513 具有优异界面粘附力的 PA66 纤维/橡胶复合材料的新型一步法环保浸渍系统及其粘附机理Fiber-reinforced rubber composites (FRRC) are widely used in tires, hoses, conveyor belts and other fields. Currently, the industry heavily relies on the resorcinol-formaldehyde-latex (RFL) system to enhance interfacial adhesion performance of FRRC; however, both resorcinol (R) and formaldehyde (F) pose significant risks to human health and the environment. Thus, some two-step RF-free dipping systems have been developed to replace RFL system. Nevertheless, these complex two-step systems face challenges during industrialization. In this study, we proposed a novel one-step eco-friendly dipping system (PCGL) for PA66 fibers. By using the new system, a solid transition bridge between PA66 fiber and rubber matrix can be formed, due to the bonding between PA66 and isocyanate, the interaction among polyacrylic acid resin, isocyanate and epoxy, the catalytic effect of triethanolamine, as well as the co-crosslinking of styrene-butadiene-vinyl-pyridine latex and rubber. The interfacial adhesion performance of PA66 fiber/rubber composites treated by PCGL with optimized ratio of epoxy groups/isocyanate groups can reach more than 90% of RFL level, meeting industry requirements for high interfacial bonding performance, while maintaining strength and safety of composites. The mechanism of largely enhanced interfacial adhesion was revealed through the analysis of modulus transition and co-crosslinking at the composite interface.纤维增强橡胶复合材料(FRRC)广泛应用于轮胎、软管、传送带等领域。目前,该行业主要依赖间苯二酚-甲醛-乳胶(RFL)系统来提高 FRRC 的界面粘合性能;然而,间苯二酚(R)和甲醛(F)都会对人类健康和环境造成严重危害。因此,人们开发了一些两步无射频浸渍系统来取代 RFL 系统。然而,这些复杂的两步法系统在工业化过程中面临着挑战。在本研究中,我们针对 PA66 纤维提出了一种新型的一步法环保浸渍系统(PCGL)。通过使用这种新体系,PA66 纤维与橡胶基体之间可以形成固体过渡桥,这是由于 PA66 与异氰酸酯之间的粘合作用,聚丙烯酸树脂、异氰酸酯和环氧树脂之间的相互作用,三乙醇胺的催化作用,以及苯乙烯-丁二烯-乙烯基吡啶胶乳与橡胶的共交联作用。环氧基团/异氰酸酯基团比例优化的 PCGL 处理的 PA66 纤维/橡胶复合材料的界面粘合性能可达 RFL 水平的 90% 以上,满足了行业对高界面粘合性能的要求,同时保持了复合材料的强度和安全性。通过分析复合材料界面的模量转变和共交联,揭示了界面粘合力大幅增强的机理。来源:复合材料力学仿真Composites FEM

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