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【新文速递】2023年12月17日复合材料SCI期刊最新文章

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今日更新:Composite Structures 7 篇,Composites Part A: Applied Science and Manufacturing 1 篇,Composites Part B: Engineering 3 篇

Composite Structures

Study of the dynamic response and damage evolution of carbon fiber/ultra-thin stainless-steel strip fiber metal laminates under low-velocity impact

Shibo Wei, Xiaoqiong Zhang, Yan Li, Tao Wang, Qingxue Huang, Cuirong Liu, Hailu Guan

doi:10.1016/j.compstruct.2023.117772

低速冲击下碳纤维/超薄不锈钢带纤维金属层合板的动态响应及损伤演化研究

Two configurations of carbon fiber/ultra-thin stainless-steel strip fiber metal laminates (CUSFML) with differing metal volume contents (35.3% and 18.2%) and carbon fiber-reinforced polymer (CFRP) composite laminates were selected for tests. The impact response and the effect of metal volume content on the impact resistance of CUSFML were assessed via experiment and FEM. Inducing damage by drop-weight test within the impact energy range of 18.60 J ∼ 46.23 J, two types of CUSFML and CFRP composite laminates were compared. In particular, the bearing capacity, impact deflection, failure modes, and energy dissipation were considered. The impact modeling using the VUMAT subroutine refines the relationship between energy-dissipating mechanism and damage evolution. The results indicate that CUSFML are characterized by higher impact resistance than CFRP composite laminates under low-velocity impact. The effect of metal volume content on the impact resistance increases gradually with impact energy increasing. Under 46.23 J impact, the CUSFML with higher metal volume content exhibits more concentrated damaged area with severe penetration failure, which is more dominated by metal failure features with a higher proportion of plastic energy dissipation. For CUSFML with lower metal volume content, extensive delamination and damage expansion occurs under the dominance of fiber damage behaviors.

选择不同金属体积含量(35.3%和18.2%)的碳纤维/超薄不锈钢带纤维金属层合板(CUSFML)和碳纤维增强聚合物(CFRP)复合材料层合板两种结构进行试验。通过实验和有限元法分析了CUSFML的冲击响应特性以及金属体积含量对其抗冲击性能的影响。在18.60 J ~ 46.23 J的冲击能量范围内,对CUSFML和CFRP两种复合材料层合板进行了落重损伤试验。特别考虑了承载力、冲击挠度、破坏模式和能量耗散。使用VUMAT子程序的冲击建模细化了能量耗散机制与损伤演化之间的关系。结果表明,CUSFML在低速冲击下比CFRP复合材料层合板具有更高的抗冲击性。随着冲击能量的增加,金属体积含量对抗冲击性能的影响逐渐增大。在46.23 J冲击下,金属体积含量高的CUSFML损伤区域更集中,侵透破坏严重,以金属破坏为主,塑性耗能比例更高。对于金属体积含量较低的CUSFML,在纤维损伤行为主导下,发生了广泛的分层和损伤扩展。


Comprehensive parametric analyses on the mechanical performance of 3D printed continuous carbon fibre reinforced plastic

Georak Park, Nak-Kyun Cho, Yeajin Lee, Chung-Soo Kim

doi:10.1016/j.compstruct.2023.117804

3D打印连续碳纤维增强塑料力学性能综合参数分析

This study presents a novel in-house modelling method called “Fibre Path Generator” and comprehensive parametric analyses on the mechanical performance of carbon fibre reinforced plastic (CFRP) with the fibre path along the principal stress direction, using both finite element (FE) simulations and experiments. The reliability of the developed CFRP model is validated through the fabrication of open-hole tensile test specimens using a co-extrusion composite 3D-printer, which demonstrated a highly compatible maximum tensile load with an error less than 3%. A comparative analysis is conducted to assess the mechanical performance of the CFRP specimen with principal stress fibre placement, which result shows that the maximum tensile load achieved is 172.84% higher than a CFRP model with uniaxial fibre placement. Furthermore, comprehensive parametric studies are carried out, varying the carbon fibre location and width-to-depth (w/D) ratio of the open-hole specimen, in order to evaluate the mechanical performance under the tensile loading. This study results provide useful insights to engineers when enhancing the mechanical performance of CFRP composite structures with effective continuous fibre placement.

本研究提出了一种新颖的内部建模方法,称为“纤维路径生成器”,并利用有限元模拟和实验对碳纤维增强塑料(CFRP)沿主应力方向的纤维路径的力学性能进行了全面的参数分析。通过使用共挤复合材料3d打印机制作开孔拉伸试件,验证了CFRP模型的可靠性,该模型显示出高度兼容的最大拉伸载荷,误差小于3%。对比分析了主应力纤维放置CFRP试件的力学性能,结果表明,CFRP试件获得的最大拉伸载荷比单轴纤维放置CFRP模型高172.84%。此外,通过改变裸眼试件的碳纤维位置和宽深比(w/D),进行了综合参数研究,以评估拉伸载荷下的力学性能。该研究结果为工程师在有效的连续纤维布局下提高CFRP复合材料结构的力学性能提供了有益的见解。


Three-phase soft mechanical metamaterials for tunable negative expansion deformation and bandgaps

Ran Tao, Yu Chen, Geng Zhi, Junrong Luo, Tian Zhao, Wenwang Wu

doi:10.1016/j.compstruct.2023.117808

可调负膨胀变形和带隙的三相软机械超材料

As the new artificial composite structures combing the smart materials and extensible topologies, the mechanical negative-expansion metamaterials deformation are promising in the fields of aerospace, robotics, medical devices, and flexible electronics. Based on the swelling characteristics of hydrogels, this work develops 2D and 3D soft mechanical metamaterials suitable for super large negative expansion deformations. The 2D and 3D metamaterials are fabricated by the multi-material 4D printing, and characterized by the experiments of self-driven negative expansion deformation and recovery. To accurately and quickly predict the deformation behavior of negative expansion response, a large-deformation theoretical model is developed based on finite element method and verified by the experimental characterizations. The influence of lattice parameters on the negative expansion response deformation and the corresponding adjustability are characterized and demonstrated through the theory, simulations and experiments. The 2D and 3D soft mechanical metamaterials show that their elastic wave bandgaps can be regulated actively and flexibly using the evolution of the lattice during the negative expansion deformation process. The present metamaterials can be used to design and manufacture instruments with adjustable negative expansion deformation and acoustic functionalities, showing the potential applications in the fields of smart soft robots and active metamaterial devices.

机械负膨胀超材料作为一种将智能材料与可扩展拓扑结构相结合的新型人工复合材料结构,在航空航天、机器人、医疗器械、柔性电子等领域有着广阔的应用前景。基于水凝胶的膨胀特性,本工作开发了适用于超大负膨胀变形的二维和三维软力学超材料。采用多材料4D打印技术制备了二维和三维超材料,并进行了自驱动负膨胀变形和恢复实验。为了准确、快速地预测负膨胀响应的变形行为,建立了基于有限元法的大变形理论模型,并通过实验表征进行了验证。通过理论、仿真和实验,表征了晶格参数对负膨胀响应变形和相应的可调节性的影响。二维和三维软质力学超材料的弹性波带隙可以通过负膨胀变形过程中晶格的演化来主动灵活地调节。所述超材料可用于设计和制造具有可调负膨胀变形和声学功能的仪器,在智能软机器人和主动超材料装置领域具有潜在的应用前景。


Static and dynamic study of fiber-reinforced hemispherical stacked sandwich structure

Zhen-Yu Li, Jin-Shui Yang, Zhi-Yuan Wang, Hong Hu, Hao Han, Hong-Ze Li, Jian-Hao Wu

doi:10.1016/j.compstruct.2023.117809

纤维增强半球形叠层夹层结构的静动力研究

Sandwich structures have garnered considerable attention due to their ability to meet the requirements of the aerospace and defense industry for impact resistance and lightweight performance. Unlike the plate or block construction investigated in previous studies, this present study proposes a new type of configuration known as the fiber-reinforced hemispherical stacked sandwich (FRHSS) structure. The fabrication of this FRHSS is achieved through the utilization of the Vacuum Assisted Resin Transfer Molding (VARTM) process and its response under quasi-static compression load is analyzed through both simulation and experiment. It is found that the internal configuration design effectively determines the direction of contraction in the hemispherical construction when it is subjected to quasi-static compression load. Furthermore, the impact resistance of the FRHSS against projectile penetration is also assessed. Through a comparison of simulation and experimental results, it becomes evident that the Chang-Chang failure criterion can successfully model the penetration process. Finally, the influence of internal configuration on the penetration resistance of the structure is studied by finite element method. The results show that the internal configuration plays an important role in the ballistic limiting velocity and ballistic performance of the construction. This study provides a valuable reference for the design of hemispherical sandwich structures.

由于夹层结构能够满足航空航天和国防工业对抗冲击和轻量化性能的要求,因此引起了相当大的关注。与之前研究的板或块结构不同,本研究提出了一种新型的结构,称为纤维增强半球形堆叠三明治(FRHSS)结构。采用真空辅助树脂传递成型(VARTM)工艺制备了该FRHSS,并通过仿真和实验分析了其在准静态压缩载荷下的响应。研究发现,内部结构设计有效地决定了半球形结构在承受准静态压缩载荷时的收缩方向。此外,还评估了FRHSS对弹丸侵彻的抗冲击性。仿真结果与试验结果对比表明,Chang-Chang破坏准则可以很好地模拟侵彻过程。最后,采用有限元法研究了结构内部构型对侵彻阻力的影响。结果表明,内构型对结构的弹道极限速度和弹道性能有重要影响。该研究为半球形夹层结构的设计提供了有价值的参考。


Transition from folding to splaying failure of braided composite tubes subjected to axial compression hybridized by bi-axial and tri-axial laminate

Zhenyu Wu, Panyou Zhang, Shuang Qin, Xiaoying Cheng, Kehong Zheng

doi:10.1016/j.compstruct.2023.117810

双轴和三轴复合材料复合编织管轴向压缩从折叠到展开失效的转变

The failure mode is a dominant factor of mechanical performance of braided composite tube subjected to axial compression. The failure mode was modified by tailoring stack-up sequence of composite tubes hybridized by bi/tri-axial braided laminate. The thermal photographing and micro-CT scanning methods were employed to monitor the in-situ damage progression and post-mortem specimen, respectively. The results show that the delamination was easy to be induced at the interface nearby tri-axial braided laminate. It attributes to the combination between the crack caused by local buckling of the axial yarns and the crack caused by shear deformation of braiding yarns. By the illumination of this behavior, delamination is controlled to occur at the different position along thickness direction of braided tube by adjusting the stacking sequence of braided laminates. When delamination position transfer from the inner/outer sides to the middle of tube wall, the failure mode transfer from the progressive folding to splaying, which increase the specific energy absorption by 45.77%.

破坏模式是影响编织复合材料管轴压力学性能的主要因素。通过调整双/三轴编织层板杂交复合材料管的堆叠顺序,修正了复合材料管的失效模式。采用热成像和显微ct扫描方法分别监测了原位损伤进展和死后试样。结果表明:三轴编织层板附近的界面处容易发生分层;它是由轴向纱局部屈曲引起的裂纹和编织纱剪切变形引起的裂纹共同作用的结果。利用这一特性,通过调整编织层板的堆叠顺序,可以控制分层在编织管厚度方向上不同位置的发生。当脱层位置由内外侧转移到管壁中部时,失效模式由渐进式折叠转变为展开,比能吸收提高45.77%。


Experimental characterization of a Polymer Metal Hybrid (PMH) automotive structure under quasi-static, creep, and impact loading

A. Canegrati, A. Bernasconi, L.M. Martulli, P. Barriga, G. Previati, D. Fiumarella, A. Scattina, E. Spini, G. Belingardi, G. Mastinu

doi:10.1016/j.compstruct.2023.117813

准静态、蠕变和冲击载荷下聚合物金属混合材料汽车结构的实验表征

A feasibility study on a short fibre reinforced Polymer Metal Hybrid (PMH) solution of a car’s suspension control arm has been conducted through a simplified demonstrator, representative of the most critical portion of this component. It was injection moulded in two versions: an all composite one and a PMH version, in which the short fibre reinforced composite was over-moulded on to an aluminium insert. The demonstrator underwent quasi-static, creep and impact tests to simulate most of the loading conditions experienced by a suspension arm during its lifetime. The mechanical behaviours of the two demonstrator versions were compared to highlight the differences introduced by the proposed novel PMH solution. In particular, the ductile metal insert ensured the compliance of the PMH demonstrators with the automotive specific safety requirement of avoiding the complete separation at failure, which was successfully obtained in all testing conditions.

通过代表汽车悬架控制臂最关键部分的简化演示器,对短纤维增强聚合物金属混合材料(PMH)解决方案的可行性进行了研究。它被注塑成两种版本:一种是全复合材料版本,另一种是PMH版本,在PMH版本中,短纤维增强复合材料被过度模压到铝嵌件上。该演示器进行了准静态、蠕变和冲击测试,以模拟悬挂臂在其使用寿命期间所经历的大多数负载条件。比较了两个演示版本的力学行为,以突出所提出的新型PMH解决方案所带来的差异。特别是,延展性金属插入确保了PMH演示器符合汽车特定的安全要求,即在失效时避免完全分离,这在所有测试条件下都成功实现了。


Mode I fracture behavior of glass fiber composite-steel bonded interface – experiments and CZM

Pei He, Marcio Moreira Arouche, Mathieu Koetsier, Marko Pavlovic

doi:10.1016/j.compstruct.2023.117814

玻璃纤维-钢复合界面I型断裂行为-实验与CZM

Debonding is characterized as the governing failure mode in the innovative wrapped composite joints made with glass fiber composite material wrapped around steel hollow sections without welding. The prerequisite for predicting debonding failure of wrapped composite joints is to obtain fracture behavior of the composite-steel bonded interface. The mode I fracture behavior of the bonded interface was experimentally investigated using glass fiber composite-steel double cantilever beam (DCB) specimens. The crack length a and the crack tip opening displacement (CTOD) during the test were accurately measured by analyzing the digital image correlation (DIC) data while the strain energy release rate (SERR) was calculated through the extended global method (EGM). The cohesive zone modeling (CZM) was utilized in the finite element model with the proposal of a four-linear traction-separation law to simulate the mode I fracture process. An approach is introduced to determine the critical stages of the proposed four-linear cohesive law by combining accurate measurements of crack length a and CTOD, along with SERR values. The validity of the four-linear cohesive law and the introduced approach to determine the critical stages were confirmed by good agreement in both global and local behavior between the testing and the FEA results.

玻纤复合材料无焊缠绕钢空心截面的新型包覆复合材料接头的主要失效模式是脱粘。预测包裹复合材料接头脱粘破坏的前提是获得复合材料-钢结合界面的断裂行为。采用玻璃纤维复合材料-钢双悬臂梁(DCB)试样,对粘结界面的I型断裂行为进行了实验研究。通过分析数字图像相关(DIC)数据,精确测量了试验过程中的裂纹长度a和裂纹尖端张开位移(CTOD),并通过扩展全局法(EGM)计算了应变能释放率(SERR)。在有限元模型中采用内聚区建模(CZM),提出了四线牵引-分离规律来模拟I型断裂过程。通过结合裂纹长度a和CTOD的精确测量以及SERR值,介绍了一种方法来确定所提出的四线性内聚规律的关键阶段。四线性内聚律和引入的关键阶段确定方法的有效性得到了验证,测试结果与有限元结果在整体和局部行为上都很吻合。


Composites Part A: Applied Science and Manufacturing

Modeling anisotropic friction in triaxial overbraiding simulations

A.N. Vu, W.J.B. Grouve, L.L. Warnet, R. Akkerman

doi:10.1016/j.compositesa.2023.107958

三轴编织模拟中各向异性摩擦的建模

Triaxial overbraiding is a highly intricate textile manufacturing process that involves interlacing yarns in three directions, enhancing reinforcement of the final composite compared to biaxial braids. Predictive process simulation is a cost-effective approach to optimizing the manufacturing process. Previous research on biaxial overbraiding simulations indicates that yarn-yarn friction has a significant effect on the braid angle and convergence zone length. This study presents an extended yarn interaction model; it utilizes a fast frontal approach and a Eulerian on Lagrangian method to simulate the complex interlacing of multiple yarns in triaxial overbraiding, including yarn-yarn and yarn-ring friction. Experiments were conducted to evaluate the effect of UD yarn tension on the convergence zone length and braid angle, and to validate the simulations. The model validation shows that a recently proposed anisotropic yarn-yarn friction model predicts braid angle more accurately than an isotropic friction model.

三轴编织是一种高度复杂的纺织制造工艺,涉及在三个方向上交织纱线,与双轴编织相比,增强了最终复合材料的增强性。预测过程仿真是优化制造过程的一种经济有效的方法。已有的双轴编织模拟研究表明,纱线间摩擦对编织角和收敛区长度有显著影响。本文提出了一种扩展的纱线相互作用模型;采用快速正面法和欧拉-拉格朗日法模拟了三轴编织中多根纱线的复杂交织,包括纱线与纱线之间的摩擦和纱线与纱环之间的摩擦。通过实验考察了UD纱线张力对汇聚区长度和编织角的影响,验证了仿真结果。模型验证表明,新提出的各向异性纱线摩擦模型比各向同性摩擦模型更能准确地预测编织角。


Composites Part B: Engineering

3D-printed stepped structure based on graphene-FeSiAl composites for broadband and wide-angle electromagnetic wave absorption

Chao Yang, Enyi He, Peng Yang, Qi Gao, Tangming Yan, Xicong Ye, Yongsheng Ye, Haihua Wu

doi:10.1016/j.compositesb.2023.111135

 

基于石墨烯- fesal复合材料的宽带广角电磁波吸收3d打印阶梯结构

The design and preparation of absorbers with ultra-wide bandwidth and wide-angle absorption characteristics are crucial technologies for addressing electromagnetic (EM) pollution. In this paper, a stepped structure absorber was fabricated of graphene (GR)-FeSiAl/polylactic acid (PLA) composite by 3D printing technology. The absorber contains four layers, the bottom layer being a slab with periodic square holes, and the upper layer is a periodic distribution of three cubes with equal thickness and gradient changes in side length. It is shown that the stepped structure achieves a minimum reflection loss (RLmin) of −36.01 dB, with an effective absorption bandwidth (EAB, corresponding to the bandwidth of RL < −10 dB) of 12.75 GHz. These results were obtained when the unit cell had a side length of 22.5 mm, the slab thickness was 1.5 mm, and the cube had a thickness and edge length difference of 2.5 mm and 4.0 mm, respectively. Furthermore, the value of EAB is greater than 10 GHz for both transverse electric (TE) polarization and transverse magnetic (TM) polarization when the incident angle changes from 0° to 50°. The broadband and efficient EM wave (EMW) absorption characteristics of this absorber can be attributed to integration of excellent impedance matching and the multi-scale loss mechanisms.

设计和制备具有超宽带宽和广角吸收特性的吸收剂是解决电磁污染的关键技术。采用3D打印技术制备了石墨烯(GR)- fesal /聚乳酸(PLA)复合材料的阶梯结构吸波材料。吸收器由四层组成,底层为具有周期性方孔的板状结构,上层为具有等厚度和边长梯度变化的三个立方体的周期性分布。结果表明,阶梯形结构的最小反射损耗(RLmin)为−36.01 dB,有效吸收带宽(EAB,对应于RL带宽 < −10 dB)为12.75 GHz。这些结果是在单元格边长为22.5 mm,板坯厚度为1.5 mm,立方体的厚度和边长分别为2.5 mm和4.0 mm时得到的。当入射角在0°~ 50°范围内变化时,横向电极化和横向磁极化的EAB值均大于10 GHz。该吸波器具有宽带、高效的电磁波吸收特性,主要归功于其良好的阻抗匹配和多尺度损耗机制的结合。


Effect of hygrothermal aging on compression behavior of CFRP material with different layups

Yuchi Liu, Han Wang, Huiming Ding, Haijin Wang, Yunbo Bi

doi:10.1016/j.compositesb.2023.111134

 

湿热老化对不同铺层CFRP材料压缩性能的影响

This study investigates the mechanical degradation mechanism and statistical analysis of residual compressive strength of three lay-up laminates under more than one-year seawater environment. Fick and Langmuir model were used to describe the moisture absorption process with a maximum moisture equilibrium content of 3.78% and various characterization methods were used to reveal the microstructural evolution of CFRP during aging. Experimental results demonstrate that the multiple fiber directions in the MD specimens provide additional moisture absorption channels, leading to a stronger wicking effect and a higher equilibrium moisture content. The layups can significantly affect the compression failure mode after long-term aging. The compressive strength of the cross-ply and multidirectional laminates decreased by 50% while that of unidirectional laminates decreased by 28%, and surface cracking is easily observed in the aged specimens. An empirical prediction model based on the Langmuir model and experimental data is proposed and verified by the data from the literature, with at least a 10% improvement in prediction accuracy. Meanwhile the three-parameter Weibull distribution was used to describe the residual compressive strength after hygrothermal aging and tested by Kolmogorov-Smirnov test. It is expected to provide insight for the application of CFRP in seawater environment.

研究了三种层压板在一年多海水环境下的力学退化机理和残余抗压强度的统计分析。采用Fick和Langmuir模型描述CFRP在最大水分平衡含量为3.78%时的吸湿过程,并采用多种表征方法揭示CFRP在老化过程中的微观结构演变。实验结果表明,MD样品中的多个纤维方向提供了额外的吸湿通道,从而导致更强的排湿效果和更高的平衡含水率。铺层对长期老化后的压缩破坏模式有显著影响。交叉层合板和多向层合板的抗压强度下降了50%,单向层合板的抗压强度下降了28%,并且在时效过程中容易观察到表面开裂。提出了基于Langmuir模型和实验数据的经验预测模型,并通过文献数据进行了验证,预测精度至少提高了10%。采用三参数威布尔分布描述湿热老化后的残余抗压强度,并进行了Kolmogorov-Smirnov试验。为碳纤维增强塑料在海水环境中的应用提供参考。


Temperature-dependent mechanical properties of graphene nanoplatelet reinforced polymer nanocomposites: Micromechanical modeling and interfacial analysis

Mengqing Yang, Lei Cao, Pingping Yang, Jun Jiang, Weifu Sun, Ying Li, Weiguo Li

doi:10.1016/j.compositesb.2023.111143

石墨烯纳米板增强聚合物纳米复合材料的温度依赖力学性能:微观力学建模和界面分析

One of the challenges to be addressed in the reasonable prediction of the mechanical properties of nanocomposites at elevated temperatures is the quantitative characterization of the temperature-dependent interfacial behavior. In this study, the temperature-dependent mechanical properties for graphene nanoplatelets (GNPs) reinforced polymer-matrix nanocomposites are modeling based on the nonlinear interfacial shear stress transfer mechanism. Besides, the influence of interfacial debonding, polymer matrix plasticity, thermomechanical parameters of components, and their evolution with temperature, as well as the orientation, dimensions and volume fractions of GNPs is considered. The Young's modulus, yield/ultimate strength, and stress-strain relationships at elevated temperatures are predicted and are verified by the available experimental data. Compared to the extended room-temperature models previously established, the proposed model considering the microscopic structures achieves higher prediction accuracy with only basic material parameters input. Furthermore, the temperature-dependent interfacial mechanical behavior is analyzed. The initial strain of debonding and the maximum debonding ratio of the interface at elevated temperatures are calculated. The micromechanical modeling establishes the quantitative relationships between the temperature-dependent interfacial behavior and the mechanical properties of nanocomposites. This study deepens the understanding of the mechanical behavior of the interface and their evolution with temperature, which contributes to the prediction of the high-temperature mechanical performance and reliability analysis of nanocomposites.

在合理预测纳米复合材料在高温下的力学性能时,需要解决的挑战之一是对温度相关界面行为的定量表征。在本研究中,基于非线性界面剪切应力传递机制,对石墨烯纳米片增强聚合物基纳米复合材料的温度依赖力学性能进行了建模。此外,还考虑了界面脱粘、聚合物基体塑性、组分热力学参数及其随温度的变化,以及GNPs的取向、尺寸和体积分数等因素的影响。预测了高温下的杨氏模量、屈服/极限强度和应力-应变关系,并通过现有的实验数据进行了验证。与已有的扩展室温模型相比,考虑微观结构的模型在仅输入基本材料参数的情况下具有更高的预测精度。此外,还分析了随温度变化的界面力学行为。计算了高温条件下界面的初始脱粘应变和最大脱粘比。微观力学模型建立了纳米复合材料界面行为与力学性能之间的定量关系。该研究加深了对界面力学行为及其随温度变化的理解,有助于纳米复合材料高温力学性能的预测和可靠性分析。



来源:复合材料力学仿真Composites FEM
ACTMechanicalMarcMAGNETDeform断裂复合材料非线性航空航天汽车电子声学裂纹理论化机材料多尺度控制
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【新文速递】2023年12月22日复合材料SCI期刊最新文章

今日更新:Composite Structures 7 篇,Composites Part A: Applied Science and Manufacturing 1 篇,Composites Part B: Engineering 1 篇,Composites Science and Technology 1 篇Composite StructuresRapid evaluation and prediction of cure-induced residual stress of composites based on cGAN deep learning modelXinyu Hui, Yingjie Xu, Jianwen Niu, Weihong Zhangdoi:10.1016/j.compstruct.2023.117827基于 cGAN 深度学习模型的复合材料固化诱导残余应力的快速评估和预测In this piece of present work, we propose a deep learning model driven by conditional generative adversarial network (cGAN) for rapid evaluation and prediction of cure-induced residual stress (CRS) of composites. The CRS is evaluated by solving for the material behaviors of the cure kinetics, viscoelasticity, thermal expansion, and cure shrinkage under heat transfer condition using finite element (FE) method. The geometry and CRS fields are extracted from numerous simulations and subsequently utilized in the proposed cGAN training process. With this end-to-end unsupervised learning, the cGAN model can predict the CRS with high fidelity based on the fiber random distributed microstructure and capture the variation of fiber volume fraction. In qualitative measures, peak signal to noise ratio (PSNR) and structure similarity index (SSIM) are employed for accuracy verification. Moreover, the cGAN model can also significantly reduce the computational cost and provide some insights for optimizing the manufacturing process of composites.在本作品中,我们提出了一种由条件生成对抗网络(cGAN)驱动的深度学习模型,用于快速评估和预测复合材料的固化诱导残余应力(CRS)。通过使用有限元(FE)方法求解热传导条件下的固化动力学、粘弹性、热膨胀和固化收缩等材料行为,对 CRS 进行评估。从大量模拟中提取几何形状和 CRS 场,然后将其用于拟议的 cGAN 训练过程。通过这种端到端的无监督学习,cGAN 模型可以根据纤维随机分布的微观结构高保真地预测 CRS,并捕捉纤维体积分数的变化。在定性测量中,采用峰值信噪比(PSNR)和结构相似性指数(SSIM)来验证准确性。此外,cGAN 模型还能显著降低计算成本,并为优化复合材料制造工艺提供一些启示。Experimental study on the bonding performance of engineered cementitious composites to normal concrete interface subjected to salt freeze-thaw cyclesJincheng Cao, Fangwen Wu, Lei song, Xiangyan Fan, Laijun Liu, Zirun Li, Ao Chendoi:10.1016/j.compstruct.2023.117828盐冻融循环条件下工程水泥基复合材料与普通混凝土界面粘结性能的实验研究This research aims to clarify the damage mechanism of engineered cementitious composites (ECC) to normal concrete (NC) interface under salt freeze–thaw cycles. A comprehensive analysis was conducted to investigate the effects of the interfacial type, ECC strength grade, and the number of salt freeze–thaw cycles on the interfacial bonding performance. The results showed that interfacial failure modes were significantly affected by the interfacial types. Two failure modes (direct shear and fatigue) were observed in the salt freeze-thaw test, and the other two failure modes (bonding material and matrix material) were observed in the direct shear test. Meanwhile, the interfacial shear strength was negatively correlated with the cycle number. Increasing the ECC strength could effectively improve the interfacial bonding performance, especially for specimens with ultra-high-performance concrete (UHPC) bonding. Finally, an interfacial bond–slip degradation model was proposed, which could be used to predict the interfacial salt freeze-thaw damage accurately.本研究旨在阐明盐冻融循环条件下工程水泥基复合材料(ECC)与普通混凝土(NC)界面的破坏机理。综合分析了界面类型、ECC强度等级和盐冻融循环次数对界面粘结性能的影响。结果表明,界面破坏模式受界面类型的影响很大。在盐冻融试验中观察到两种失效模式(直接剪切和疲劳),在直接剪切试验中观察到另外两种失效模式(粘接材料和基体材料)。同时,界面剪切强度与循环次数呈负相关。提高 ECC 强度可有效改善界面粘结性能,尤其是对于采用超高性能混凝土(UHPC)粘结的试样。最后,提出了界面粘结滑动退化模型,该模型可用于准确预测界面盐冻融破坏。Gradient Shear Thickening Gel/ Stacked Kevlar Multi-layer Armor with Enhanced Impact Attenuation PropertyFeng Chen, Zhen-Hua Tang, Yu Zhu, Jian-Qiang Deng, Yuan-Qing Li, Ya-Qin Fu, Shao-Yun Fudoi:10.1016/j.compstruct.2023.117829梯度剪切增厚凝胶/叠层凯夫拉纤维多层装甲,具有更强的冲击衰减性能Realizing highly-efficient energy absorbing performance in soft body armor, yet with lightweight feature, has always been an eternal subject for personal protective equipment. This work reports a gradient shear thickening gel (STG)/stacked Kevlar (GS-STG/Kevlar) multi-layer fabric armor with both lightweight feature and excellent impact attenuation performance. Firstly, STG is prepared by mechanical blending and chemical crosslinking and then coated on Kevlar fabrics, and afterwards STG-coated Kevlar multi-layer fabrics with gradient STG distribution in the thickness direction are fabricated. Single yarn pull-out test demonstrates that the friction between Kevlar yarns is greatly increased after STG treatment. Moreover, tribological testing also indicates that the friction coefficient of Kevlar fabrics is improved by coating STG. Furthermore, low- and high-speed impact experiments are conducted, and the results demonstrate that the GS-STG/Kevlar composite exhibits the best impact attenuation property when compared with multilayered Kevlar fabrics and uniformly stacked STG/Kevlar fabrics under the same impact conditions. The increased friction and stiffening effect by STG, and the gradient stacking strategy are responsible for the great improvement in the impact attenuation performance of GS-STG/Kevlar multi-layer armors. This study provides an effective methodology for achieving soft body armors with lightweight and high impact attenuation properties for personal impact protection.在软质防弹衣中实现高效的能量吸收性能,同时兼顾轻质特性,一直是个人防护装备的永恒课题。本研究报道了一种梯度剪切增稠凝胶(STG)/叠层凯夫拉纤维(GS-STG/Kevlar)多层织物装甲,兼具轻质特性和优异的冲击衰减性能。首先,通过机械混合和化学交联制备 STG,然后将其涂覆在凯夫拉纤维上,最后制成 STG 在厚度方向上梯度分布的 STG 涂覆凯夫拉多层纤维装甲。单根纱线拉出试验表明,经过 STG 处理后,凯夫拉纱线之间的摩擦力大大增加。此外,摩擦学测试也表明,涂覆 STG 后,凯夫拉纤维的摩擦系数得到了改善。此外,还进行了低速和高速冲击实验,结果表明,在相同的冲击条件下,GS-STG/Kevlar 复合材料与多层 Kevlar 织物和均匀堆叠的 STG/Kevlar 织物相比,具有最佳的冲击衰减性能。STG 增加的摩擦和刚度效应以及梯度堆叠策略是 GS-STG/Kevlar 多层装甲冲击衰减性能大幅提高的原因。这项研究为实现轻质、高冲击衰减性能的软体护甲提供了一种有效的方法,可用于人身冲击防护。Hygrothermal effects on fatigue delamination behavior in composite laminatesLiaojun Yao, Jiexiong Wang, Yonglyu He, Xiuhui Zhao, Xiangming Chen, Jurui Liu, Licheng Guo, R.C. Alderliestendoi:10.1016/j.compstruct.2023.117830湿热效应对复合材料层压板疲劳分层行为的影响Fatigue delamination growth (FDG) is an important failure in composite structures during their long-term operations. Hygrothermal aging can have significant effects on interlaminar resistance. It is therefore really necessary to explore FDG behavior in composite laminates with hygrothermal aging. Dynamic mechanical thermal analysis (DMTA), mode I FDG experiments and fractographic examinations were conducted to fully investigate hygrothermal aging effects and the corresponding mechanisms on FDG behavior. The DMTA results indicated that environmental aging can induce obvious Tg decrease. Mode I experimental fatigue data interpreted via different Paris-type correlations demonstrated that: Bridging has obvious retardation effects on FDG behavior via the Paris interpretations; The modified Paris relation can well characterize the intrinsic FDG behavior around the crack front; The use of the two-parameter Paris-type relation can appropriately account for R-ratio effects, contributing to a master resistance curve in determining mode I FDG behavior. According to these interpretations, it can be concluded that hygrothermal aging can have adverse effects on mode I FDG behavior. SEM examinations demonstrated that moisture absorption can cause fibre/matrix debonding and resin matrix pores/voids in the composite. However, no obvious difference in damage mechanisms was identified in mode I fatigue delamination for composite with/without environmental conditioning. Both fibre/matrix debonding and matrix brittle fracture were identified on fatigue fracture surfaces. Accordingly, it was concluded that fibre/matrix interface and matrix degradation induced by water absorption were the main reasons for a faster mode I fatigue crack growth in environmental aged composite.疲劳分层生长(FDG)是复合材料结构长期运行过程中的一个重要故障。湿热老化会对层间阻力产生重大影响。因此,有必要对湿热老化复合材料层压板的 FDG 行为进行研究。为了全面研究湿热老化对 FDG 行为的影响和相应机制,我们进行了动态力学热分析(DMTA)、模式 I FDG 实验和断裂学检查。DMTA 结果表明,环境老化会导致 Tg 下降。通过不同的巴黎型相关性解释的模式 I 实验疲劳数据表明通过巴黎关系式解释,桥接对 FDG 行为具有明显的延缓效应;修正的巴黎关系式可以很好地描述裂纹前沿周围的固有 FDG 行为;使用双参数巴黎关系式可以适当地考虑 R 比率效应,有助于在确定模式 I FDG 行为时形成主电阻曲线。根据这些解释,可以得出结论:湿热老化会对模式 I FDG 行为产生不利影响。扫描电子显微镜检查表明,吸湿会导致复合材料中的纤维/基质脱粘和树脂基质孔隙/空洞。然而,在有/无环境调节的复合材料中,模式 I 疲劳分层的损坏机制并无明显差异。在疲劳断裂面上发现了纤维/基质脱粘和基质脆性断裂。由此得出结论,吸水引起的纤维/基质界面和基质降解是环境老化复合材料中模式 I 疲劳裂纹增长较快的主要原因。Investigating the Influence of High-Void Content on the Impact and Post-Impact Properties of Flax/Epoxy Composite Laminates with Different Stacking ConfigurationsAbdelhadi Hadj-Djilani, Lotfi Toubal, Habiba Bouguerara, Redouane Zitounedoi:10.1016/j.compstruct.2023.117832研究高类固醇含量对不同堆叠配置的亚麻/环氧复合材料层压板的冲击和冲击后性能的影响Defects in composite materials, such as voids, significantly impact their long-term performance and should be carefully considered in the design process of engineering structures. This study investigates the effects of high void content on the impact and post-impact properties of pure Flax/Epoxy (FE) composite laminates. Three main configurations, namely cross-ply (CFE), angle-ply FE (AFE), and quasi-isotropic FE (QFE), are examined using drop-weight impact and three-point bending tests. The results reveal distinct behavior among the configurations. The drop-weight impact test results show that the AFE configuration exhibits 3.5% and 6.45% higher impact resistance compared to CFE and QFE, respectively. to the increase of the impact energy to 15J amplifies the differences to 9.31% and 19.11 %. Also, post-impact flexion tests demonstrate a significant decline in flax composite resistance by 14% for CFE, 26% for QFE, and AFE. Furthermore, the overall impact and flexural properties of the FE composites are not significantly affected by the void content. However, it has a major impact on the damage mechanism that is ispected visually and through X-ray tomography, emphasizing the importance of considering the void content in the design and analysis of such flax composites. The proposed numerical model to predict the onset of damage and damage evolution in these composite materials under low velocity impact show a good greement with the experimental results.复合材料中的缺陷(如空隙)会严重影响其长期性能,因此在工程结构设计过程中应慎重考虑。本研究探讨了高空隙含量对纯亚麻/环氧(FE)复合材料层压板的冲击性能和冲击后性能的影响。通过落重冲击和三点弯曲试验,研究了三种主要结构,即交叉层(CFE)、角层 FE(AFE)和准各向同性 FE(QFE)。试验结果表明,这些结构之间存在明显差异。落重冲击试验结果表明,与 CFE 和 QFE 相比,AFE 配置的抗冲击性分别高出 3.5% 和 6.45%。此外,冲击后的弯曲测试表明,CFE、QFE 和 AFE 的亚麻复合材料抗冲击性显著下降了 14%、26%。此外,空隙含量对 FE 复合材料的整体冲击和弯曲性能影响不大。然而,它对通过视觉和 X 射线断层扫描观察到的损伤机制有重大影响,这强调了在设计和分析此类亚麻复合材料时考虑空隙含量的重要性。为预测这些复合材料在低速冲击下的损伤开始和损伤演变而提出的数值模型与实验结果显示出良好的一致性。Investigation into quasi-static compressive behaviors of several kinds of honeycomb like structures in three axial directionsGuijia Gao, Haibiao Lu, Chunhui Sha, Weili Ren, Yunbo Zhong, Zuosheng Leidoi:10.1016/j.compstruct.2023.117833几种蜂窝状结构在三个轴向的准静态抗压行为研究The natural beesʼ honeycombs maintain long-term structural stability in harsh environments, employing a highly material-efficient approach. However, the reasons remain somewhat ambiguous. To clarify the stabilization mechanism and investigate quasi-static compression responses of double-layer ordered cellular structures, honeycomb, Tóth and single-layer cellular structures with a relative density (ρr) of 25.84% were fabricated using 3D printing technology. Then, quasi-static compression experiments in three directions were conducted. Further, a numerical study was conducted to uncover the stabilization mechanism and effect of ρr on compressive behaviors. Results revealed that the stabilization mechanism was mainly attributed to bearing load priority of intermediate layer and its inhibition on formation of plastic hinges. A relative density of 5.17% served as a transition point for deformation mode, beyond which honeycomb and Tóth structures exhibited stronger in-plane compressive strength at expense of less sacrificed out-of-plane compressive strength, below which they both exhibited more stable compressive curves compared to single-layer cellular structures, which were favorable for energy absorption. This study clarifies the stability mechanism of beesʼ honeycombs and addresses the lack on compression behaviors of double-layer ordered cellular structures. Moreover, it introduces two available bionic structures with controllable deformation modes to expand the application of single-layer cellular structures.天然蜜蜂的蜂巢在恶劣的环境中保持着长期的结构稳定性,采用了一种非常节省材料的方法。然而,其中的原因仍然有些模糊。为了阐明稳定机制并研究双层有序蜂窝结构的准静态压缩响应,利用三维打印技术制作了相对密度(ρr)为25.84%的蜂窝、托斯和单层蜂窝结构。然后,进行了三个方向的准静态压缩实验。此外,还进行了数值研究,以揭示稳定机制和ρr对压缩行为的影响。结果表明,稳定机制主要归因于中间层的承载力优先及其对塑性铰形成的抑制作用。5.17%的相对密度是变形模式的一个过渡点,超过该点,蜂窝结构和托特结构表现出更强的平面内抗压强度,但牺牲的平面外抗压强度较小,低于该点,与单层蜂窝结构相比,它们都表现出更稳定的抗压曲线,有利于能量吸收。这项研究阐明了蜜蜂蜂窝的稳定机制,并解决了双层有序蜂窝结构抗压行为方面的不足。此外,它还介绍了两种具有可控变形模式的仿生结构,以扩大单层蜂窝结构的应用范围。The alignment of CNTs perpendicular to electric filed resulted in effective electrothermal de/anti-icing performance at high voltage for CNT/XLPE compositesXiaoli Wu, Yunyi Li, Ting Yin, Yijun Liao, Site Mo, Wanxia Huangdoi:10.1016/j.compstruct.2023.117835垂直于电场的 CNT 排列使 CNT/XLPE 复合材料在高压下具有有效的电热除冰/防结冰性能The composite in transverse direction to the alignment is considered as completely insulating and unsuitable for utilization in de-icing system. Here, we found that the composite in transverse direction to the alignment exhibits excellent electrothermal performance at high voltage, for the first time. Furthermore, we compared and investigated the electrical and electrothermal performance of the aligned and random non-percolative CNT/crosslinked polyethylene (XLPE) composites at high voltage. A temperature increase of 7.5–72.7 ℃ at a record high voltage of 900–3100 V is reached for the aligned CNT/XLPE composites. The filed emission at high voltage enables the electron to transfer along the CNTs radial direction, resulting in joule heating for the aligned CNT/XLPE composites in transverse direction to the alignment. Besides, the non-percolative structure contributes a temperature increase of 8.2–40.1 ℃ at applied voltages of 900–2800 V to random CNT/XLPE composites. The high applied voltages is significantly higher than rGO-based composites. More importantly, effective de-icing and anti-icing performance at high voltage of 900–2800 V are achieved for the random non-percolative and aligned CNT-based composites at −20 ℃. These results demonstrate the potential of applying the CNT/XLPE composites in de/anti-icing system of transmission-lines and other fields requiring joule heating at high voltage.横向排列的复合材料被认为是完全绝缘的,不适合用于除冰系统。在这里,我们首次发现,在高电压下,横向排列的复合材料表现出优异的电热性能。此外,我们还比较并研究了有序排列的 CNT/交联聚乙烯(XLPE)复合材料与无序排列的 CNT/交联聚乙烯(XLPE)复合材料在高压下的电气和电热性能。在 900-3100 V 的创纪录高压下,排列的 CNT/XLPE 复合材料的温度升高了 7.5-72.7 ℃。高电压下的锉射使电子沿 CNT 的径向转移,从而导致对齐 CNT/XLPE 复合材料在对齐的横向上产生焦耳热。此外,在施加 900-2800 V 的电压时,非气蚀结构会使无规 CNT/XLPE 复合材料的温度升高 8.2-40.1 ℃。高应用电压明显高于基于 rGO 的复合材料。更重要的是,在 900-2800 V 的高电压下,无规非腐蚀性和排列有序的 CNT 复合材料在 -20 ℃ 下实现了有效的除冰和防冰性能。这些结果证明了将 CNT/XLPE 复合材料应用于输电线路除冰/防冰系统以及其他需要在高压下进行焦耳加热的领域的潜力。Composites Part A: Applied Science and ManufacturingProcess-Induced Residual Stress in a Single Carbon Fiber Semicrystalline Polypropylene Thin FilmNithin K. Parambil, Branndon R. Chen, John W. Gillespiedoi:10.1016/j.compositesa.2023.107969单碳纤维半结晶聚丙烯薄膜中的工艺诱导残余应力During the processing of semicrystalline thermoplastic composites, various models for the prediction of residual stress have been proposed but experimental validation is limited. In this study, a modeling framework is developed to predict the evolution of residual stress in a single carbon fiber embedded in a semicrystalline polypropylene thin film subjected to non-isothermal cooling. Validation is based on in-situ measurement of axial fiber strain after processing using micro-Raman Spectroscopy. A material model for polypropylene (50% equilibrium crystallinity) is presented that incorporates the effects of non-isothermal cooling on crystallinity-dependent resin shrinkage and crystallinity-dependent resin modulus from the amorphous polymer melt to room temperature. The evolution of residual stress is calculated using a finite element (FE) model with a user-developed subroutine incorporating the resin material models. Single-fiber polypropylene films are fabricated using a range of fiber pretension levels to prevent fiber waviness during cooling and to induce a wide range of axial strain levels in the fiber for model validation. The fiber axial strain was measured over the length of the fiber, from the free edge into the bulk, capturing the ineffective length region where strain builds up and plateaus. A good correlation has been obtained between the model results and the in-situ measurements of axial compression strain in the fiber. A key finding was the importance of including temperature-dependent resin modulus and that the contribution of crystallinity shrinkage to residual strain in the carbon fiber is relatively low. The model developed in this study is also compared to residual stress models in the literature which shows the importance of including the effects of crystallization and cooling rate on temperature and crystallinity-dependent modulus and resin shrinkage for accurate predictions.在半结晶热塑性复合材料的加工过程中,人们提出了各种预测残余应力的模型,但实验验证却很有限。本研究建立了一个建模框架,用于预测嵌入半结晶聚丙烯薄膜中的单根碳纤维在非等温冷却条件下的残余应力演变。验证基于使用显微拉曼光谱法对加工后纤维轴向应变的现场测量。介绍了聚丙烯(50% 平衡结晶度)的材料模型,该模型包含了非等温冷却对从无定形聚合物熔体到室温的结晶度相关树脂收缩和结晶度相关树脂模量的影响。残余应力的演变是通过有限元(FE)模型和用户开发的包含树脂材料模型的子程序计算得出的。在制作单纤维聚丙烯薄膜时,使用了一系列纤维预拉伸水平,以防止纤维在冷却过程中产生波纹,并在纤维中产生各种轴向应变水平,以验证模型。纤维的轴向应变是在纤维长度上测量的,从自由边缘到纤维体,捕捉到了应变累积和稳定的无效长度区域。模型结果与纤维轴向压缩应变的现场测量结果之间具有良好的相关性。一个重要的发现是,包含随温度变化的树脂模量非常重要,而且结晶收缩对碳纤维残余应变的影响相对较小。本研究中开发的模型还与文献中的残余应力模型进行了比较,结果表明,要进行准确预测,必须将结晶和冷却速度对温度的影响以及与结晶度相关的模量和树脂收缩包括在内。Composites Part B: EngineeringTensile mechanical properties and damage analysis of layered woven GFRP composite boltsJintong Zhang, Tao Yang, Yu Du, Renyu He, Chang Liudoi:10.1016/j.compositesb.2023.111155分层编织 GFRP 复合材料螺栓的拉伸力学性能和损伤分析Composite bolts have become one of the research focuses in screw threads joints due to their lightweight, high-strength, and wave transmission properties. We elucidate the differences in tensile properties, damage processes, and tensile failure forms between two types of layered woven GFRP composite bolts through tests and numerical simulations. It was found that the tensile strength of layered plain woven bolts is 40% higher than layered twill woven bolts. The failure forms of both types of bolts are related to their layered woven structure. The fracture surface of plain bolts is planar, while the fracture surface of twill bolts is apex shaped. Subsequently, a refined thread stretching model was established to study the effect of loading speed on the tensile property of screw threads. It was found that the tensile strength of plain woven screw threads and twill woven screw threads at a loading speed of 1 mm/min was 11% and 6% higher than that at 3 mm/min, respectively. The results show that the bolts and screw threads with layered plain woven have stronger tensile strength than those with layered twill woven, and a decrease in loading speed within a certain range can improve the tensile strength of the screw threads.复合材料螺栓因其轻质、高强、透波等特性已成为螺纹接头的研究重点之一。我们通过试验和数值模拟,阐明了两种分层编织 GFRP 复合材料螺栓在拉伸性能、损伤过程和拉伸失效形式上的差异。试验发现,分层平纹编织螺栓的拉伸强度比分层斜纹编织螺栓高 40%。两种螺栓的破坏形式都与其分层编织结构有关。平纹螺栓的断裂面为平面,而斜纹螺栓的断裂面为顶点形。随后,建立了精炼的螺纹拉伸模型,以研究加载速度对螺纹拉伸性能的影响。结果发现,在加载速度为 1 毫米/分钟时,平织螺纹和斜织螺纹的拉伸强度分别比加载速度为 3 毫米/分钟时高 11% 和 6%。结果表明,分层平纹编织的螺栓和螺纹比分层斜纹编织的螺栓和螺纹具有更强的抗拉强度,在一定范围内降低加载速度可以提高螺纹的抗拉强度。Composites Science and TechnologyPreparation of superhydrophobic shape memory composites with uniform wettability and morphing performanceXinlin Li, Bin Zhan, Xueting Wang, Yan Liu, Yanju Liu, Jinsong Lengdoi:10.1016/j.compscitech.2023.110398 制备具有均匀润湿性和变形性能的超疏水形状记忆复合材料Superhydrophobic shape memory surfaces have attracted much attention in recent years, as they can intelligently control surface wettability. However, less research has focused on the development of superhydrophobic shape memory materials that can maintain uniform wettability in any morphing shape. It is common in nature that species such as lotus leaves and kingfisher show good superhydrophobicity in any movement under/on water. Based on this inspiration, this work presents a novel superhydrophobic shape memory composite (SSMC) by coupling superhydrophobic coatings and shape memory epoxy composites. The SSMC exhibits excellent water repellency and self-cleaning performance regardless of how it is bent. In addition, its good shape memory effect and variable stiffness characteristics enable it to be potentially used as deployable marine structures and morphing skin of aquatic unmanned aerial vehicles. On the other hand, the SSMC also offers good anti-icing properties and mechanical/chemical robustness that enhance long-term service performance all year round. This research provides a fresh idea for the design of new smart superhydrophobic materials and expands applications in the field of marine and aviation facilities.超疏水形状记忆表面能够智能控制表面润湿性,因此近年来备受关注。然而,关于开发可在任何变形形状下保持均匀润湿性的超疏水形状记忆材料的研究却较少。在自然界中,荷叶和翠鸟等物种在水下/水上的任何运动都表现出良好的超疏水性。受此启发,本研究通过将超疏水涂层与形状记忆环氧树脂复合材料相结合,提出了一种新型超疏水形状记忆复合材料(SSMC)。无论如何弯曲,SSMC 都能表现出优异的憎水性和自清洁性能。此外,其良好的形状记忆效果和可变刚度特性使其有可能用作可部署的海洋结构和水上无人飞行器的变形表皮。另一方面,SSMC 还具有良好的防冰性能和机械/化学坚固性,可提高全年的长期使用性能。这项研究为新型智能超疏水材料的设计提供了新思路,拓展了其在海洋和航空设施领域的应用。来源:复合材料力学仿真Composites FEM

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