首页/文章/ 详情

【新文速递】2023年11月22日复合材料SCI期刊最新文章

23天前浏览251

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

Composite Structures

Hierarchical lattice stiffened cylindrical shell: Design, high-order vibration theory and composite parameter identification

Zhang Lu, He Weiping, Zhu Shiyang, Lai Changliang, Tao Yanming, Zhu Hengyi, Li Ming, Fan Hualin

doi:10.1016/j.compstruct.2023.117725

分层晶格加劲圆柱壳:设计、高阶振动理论和复合参数识别

A carbon fiber reinforced hierarchical lattice stiffened cylindrical shell (HLSCS) was designed and manufactured. Introducing effects of bending and coupling stiffness caused by neutral plane offsetting, an improved smeared stiffener method was proposed to homogenize the HLSCS to an anisotropic continuous cylindrical shell with varying-stiffness. The transverse shear stiffness was predicted by the higher-order shear deformation theory to build a high order vibration theory. Composite parameter identification method of the HLSCS was proposed based on the experimental and theoretical results to identify the composite parameters nondestructively. The method suggests discounted fiber volume fraction and stiffness for the completed HLSCS.

设计并制造了碳纤维增强分层晶格加劲圆柱壳(HLSCS)。在引入中性面偏移引起的弯曲和耦合刚度的影响后,提出了一种改进的涂抹加劲体方法,将 HLSCS 均质化为具有变化刚度的各向异性连续圆柱壳。横向剪切刚度由高阶剪切变形理论预测,从而建立了高阶振动理论。根据实验和理论结果,提出了 HLSCS 的复合材料参数识别方法,以非破坏方式识别复合材料参数。该方法为完成的 HLSCS 提出了纤维体积分数和刚度折扣。


Composites Part A: Applied Science and Manufacturing

Investigating the tensile properties of 3D printed semi-woven intraply hybrid composites reinforced with carbon/glass continuous fibres

Huang Cheng, Norton Michael, Joosten Mathew W

doi:10.1016/j.compositesa.2023.107924

研究用碳/玻璃连续纤维增强的 3D 打印半编织内包混合复合材料的拉伸性能

In this study the mechanical performance of 3D printed intraply hybrid semi-woven composites was investigated. The hybrid composites were fabricated from two types of tow-preg filaments that consist of either carbon or glass fibres impregnated with polyamide, referred to as low elongation (LE) and high elongation (HE) materials respectively. The effect of two printing parameters, weave type and the LE material ratio, were investigated using fifteen unique laminates. The ultimate strain of the hybrid laminates was dependent on the LE material ratio with a transition point at ∼50%. Analytical and FE models were used to predict laminate strength and modulus. In general, the FE model underpredicted the experimental data and the analytical models showed good correlation with experimental observations. The validated analytical model can be used to design hybrid semi-woven laminates to produce a targeted modulus and strength through appropriate selection of weave type and LE material ratio.

本研究调查了三维打印内包混合半编织复合材料的机械性能。混合复合材料由两种类型的丝束-浸渍聚酰胺的碳纤维或玻璃纤维组成,分别称为低伸长率(LE)和高伸长率(HE)材料。我们使用 15 种独特的层压材料研究了两种印刷参数(编织类型和 LE 材料比率)的影响。混合层压板的极限应变取决于 LE 材料比,过渡点为 ∼50%。分析和 FE 模型用于预测层压板的强度和模量。一般来说,FE 模型对实验数据的预测较低,而分析模型与实验观测结果显示出良好的相关性。经过验证的分析模型可用于设计混合半编织层压板,通过适当选择编织类型和 LE 材料比来产生目标模量和强度。


An Effective Micro-arc Oxidation (MAO) Treatment on Aluminum Alloy for Stronger Bonding Joint with Carbon Fiber Composites

Zuo Shihao, Cheng Fei, Yang Guangming, Li Jiangzhou, Deng Yongjun, Gou Guangjun, Cui Xuejun, Hu Yunsen, Hu Xiaozhi

doi:10.1016/j.compositesa.2023.107919

对铝合金进行有效的微弧氧化(MAO)处理,使其与碳纤维复合材料的连接更牢固

The micro-arc oxidation (MAO) treatment was used in this study to modify aluminum (Al) alloys to improve bond strength with carbon fiber reinforced polymer (CFRP). Various porous surfaces of Al alloy with better hardness, roughness and wetting were created. Void defects were reduced via using resin pre-coating (RPC) technique to guide high-viscosity epoxy into the holes, CNTs fiber bridging was constructed to improve bonding interface and epoxy adhesive layer. Combined treatments of “Na2SiO3 + KOH solution” MAO, RPC and introducing CNTs on Al alloy surface yielded 21.34 MPa, up to 156.1% increment over base strength. Original de-bonding failure on Al alloy surface was altered into dominant fiber tearing failure of CFRP composites, indicating the reinforced bond strength and stronger adhesive joint. MAO was the first try and proved as a feasible treatment for bond strength improvement, which could provide an alternative to manufacture high-performance Al-CFRP composites in industrial production.

本研究采用微弧氧化(MAO)处理方法对铝(Al)合金进行改性,以提高其与碳纤维增强聚合物(CFRP)的结合强度。铝合金的各种多孔表面具有更好的硬度、粗糙度和润湿性。通过使用树脂预涂层(RPC)技术将高粘度环氧树脂导入孔中,减少了空隙缺陷,并构建了碳纳米管纤维桥接以改善粘接界面和环氧树脂粘合层。在铝合金表面采用 "Na2SiO3 + KOH 溶液 "MAO、RPC 和引入 CNT 的组合处理方法,可获得 21.34 MPa 的强度,比基础强度提高了 156.1%。铝合金表面原有的脱粘失效转变为 CFRP 复合材料的主要纤维撕裂失效,表明粘接强度得到了增强,粘接强度更高。MAO 是首次尝试并被证明是提高粘接强度的可行处理方法,可为在工业生产中制造高性能 Al-CFRP 复合材料提供替代方案。


Effects of accelerated curing in thermoplastic particle interleaf epoxy laminates

Kratz James, Paris Christophe, Gaska Karolina, Maes Vincent, Partridge Ivana, Olivier Philippe

doi:10.1016/j.compositesa.2023.107922

加速固化对热塑性颗粒夹层环氧树脂层压板的影响

Faster heating rates of 10°C/min and higher process temperatures of 210°C were applied to the commercial M21 resin system. The total process time was reduced by two-thirds while achieving the same degree-of-cure in the epoxy. Thermal analysis and hot-stage microscopy showed that the thermoplastic interleaf particles melt at around 15°C above the manufacturer's recommended 180°C curing temperature. A short dwell at 180°C was found to prevent the thermoplastic particle from mixing with the thermoset pre-polymer before ramping to the accelerated curing temperature of 210°C. Such interaction was found to decrease the glass transition temperature by 13–45%, but increase the mode I delamination resistance by 70–105%, respectively. The results demonstrate that accelerated curing of interleaf systems can shorten cycle time and produce a range of physical and mechanical properties from a single base material, opening the design space to new and optimised composite structures.

对商用 M21 树脂系统采用了 10°C/min 的更快加热速率和 210°C 的更高加工温度。在环氧树脂达到相同固化度的同时,总加工时间缩短了三分之二。热分析和热阶段显微镜显示,热塑性夹层颗粒在高于制造商建议的 180°C 固化温度约 15°C 时熔化。在升至 210°C 加速固化温度之前,180°C 的短暂停留可防止热塑性颗粒与热固性预聚物混合。结果发现,这种相互作用会使玻璃化转变温度降低 13-45%,但会使模式 I 分层阻力增加 70-105%。研究结果表明,夹层系统的加速固化可以缩短周期时间,并从单一基材中产生一系列物理和机械特性,为优化新型复合材料结构打开了设计空间。


Composites Part B: Engineering

Non-additive polymer matrix coated rGO/MXene inks for embedding sensors in prepreg enhancing smart FRP composites

Duongthipthewa Anchalee, Hanmo Zhou , Wang Qingqing, Zhou Limin

doi:10.1016/j.compositesb.2023.111108

非添加型聚合物基体涂覆 rGO/MXene 油墨,用于在预浸料中嵌入传感器,增强智能 FRP 复合材料的性能

Two-dimensional (2D) nanosheets are promising nanomaterials that can be used as sensing elements in numerous applications such as wearable devices, machine tools, and aircraft; however, challenges remain in achieving high sensitivity, wide frequency sensing range, and reliability after long cyclic loading. Suitable ink formulations and preparation parameters for embedded sensors while retaining the structural integrity of the host structure should be determined. In this work, we demonstrated a synergistic combination of l-cysteine-reduced graphene oxide and MXene (LGM) inks in the absence of an additional polymer matrix to establish noninvasive conditions for embedding sensors in prepreg fiberglass/epoxy for smart composites with sensing capabilities. This sensor offers a high gauge factor of 47–1400 in different tensile strain ranges, with unnoticeable changes in the outstanding mechanical properties of the host glass fiber-reinforced polymer (GFRP) laminate. Long-term fatigue three-point bending tests were performed at different frequencies and bending angles, demonstrating excellent durability and stability. The corresponding sensors can also capture vibration signals in the low-high-frequency ranges. The nonintrusive embedment of sensors in GFRP laminates using the new coated non-additive polymer matrix LGM ink successfully preserves the mechanical properties of the host, including its structural integrity, with outstanding sensing performance for low-to-high-frequency signals.

二维(2D)纳米片是一种前景广阔的纳米材料,可在可穿戴设备、机床和飞机等众多应用中用作传感元件;然而,在实现高灵敏度、宽频率传感范围以及长时间循环加载后的可靠性方面仍存在挑战。应确定适合嵌入式传感器的油墨配方和制备参数,同时保持主结构的结构完整性。在这项工作中,我们展示了在没有额外聚合物基体的情况下,l-半胱氨酸还原氧化石墨烯和 MXene(LGM)油墨的协同组合,为在预浸玻璃纤维/环氧树脂中嵌入传感器创造了无创条件,从而实现了智能复合材料的传感功能。这种传感器在不同的拉伸应变范围内具有 47-1400 的高测量系数,同时不会明显改变主玻璃纤维增强聚合物(GFRP)层压板的出色机械性能。在不同频率和弯曲角度下进行了长期疲劳三点弯曲测试,结果表明其具有出色的耐用性和稳定性。相应的传感器还能捕捉低频-高频范围内的振动信号。使用新型涂层非添加剂聚合物基质 LGM 油墨在 GFRP 板材中非侵入式嵌入传感器,成功地保持了主机的机械性能,包括其结构完整性,并对低频至高频信号具有出色的传感性能。


Composites Science and Technology

CNTs-induced superhydrophobic and photothermal coating with long-term durability and self-replenishing property for anti-icing/de-icing

Deng Lechun, Wang Zongwen, Niu Yuxiang, Luo Fa, Chen Qiang

doi:10.1016/j.compscitech.2023.110347

 

由 CNT 引发的超疏水和光热涂层具有长期耐久性和自我补给特性,可用于防冰/除冰

Ice formation and accumulation of various equipment often leads to economic loss and severe traffic accidents. Although numerous anti-icing coating strategies have been exploited in recent years, robust and durable surfaces for effective anti-icing and de-icing remains a big challenge. In this work, mesoporous silica nanoparticles (mSiO2) were loaded with high-dosage polydimethylsiloxane (PDMS) to prepare hydrophobic PDMS@mSiO2 aggregates, which was then incorporated into silicon resin matrix together with carbon nanotubes (CNTs), to construct a near infrared-responsive anti-icing/de-icing coating by a one-step spraying method. The PDMS@mSiO2 particles imparted to the coating micro-scaled roughness and low surface energy, and the CNTs supplemented the formation of micro-nano hierarchical structure to enhance the water repellency and offered the photothermal property. Consequently, the prepared coating possessed superhydrophobic character with the contact angle up to 154.3 ° as well as the delayed freezing time of 440 s at −20 °C, nearly 73 times of that on aluminum plates. Furthermore, the as-obtained coating exhibited robust adhesion and stable anti-icing properties under various harsh environmental conditions, which is promising for anti-icing and de-icing modification of rotor wings with robustness and long-term durability.

各种设备结冰和积冰往往会导致经济损失和严重的交通事故。尽管近年来已开发出多种防冰涂层策略,但用于有效防冰和除冰的坚固耐用的表面仍然是一个巨大的挑战。本研究采用高剂量聚二甲基硅氧烷(PDMS)负载介孔二氧化硅纳米颗粒(mSiO2),制备疏水性PDMS@mSiO2聚集体,然后将其与碳纳米管(CNTs)一起加入硅树脂基体中,通过一步喷涂法构建近红外响应的防冰/除冰涂层。PDMS@mSiO2 颗粒赋予涂层微尺度的粗糙度和低表面能,CNTs 补充形成了微纳层次结构,增强了憎水性并提供了光热特性。因此,制备的涂层具有超疏水特性,接触角高达 154.3 °,在 -20 °C 下的延迟冻结时间为 440 秒,几乎是铝板的 73 倍。此外,所制备的涂层在各种恶劣环境条件下均表现出强大的附着力和稳定的防冰性能,有望用于具有坚固性和长期耐久性的旋翼防冰和除冰改装。



 


来源:复合材料力学仿真Composites FEM
ACTMechanicalAdditiveSystemDeform振动疲劳复合材料理论材料
著作权归作者所有,欢迎分享,未经许可,不得转载
首次发布时间:2024-11-03
最近编辑:23天前
Tansu
签名征集中
获赞 5粉丝 0文章 776课程 0
点赞
收藏
作者推荐

【新文速递】2023年11月26日固体力学SCI期刊最新文章

今日更新:International Journal of Solids and Structures 2 篇,Journal of the Mechanics and Physics of Solids 2 篇,Mechanics of Materials 1 篇,Thin-Walled Structures 3 篇International Journal of Solids and StructuresComputational Cosserat periporomechanics for strain localization and cracking in deformable porous mediaXiaoyu Song, Hossein Pashazaddoi:10.1016/j.ijsolstr.2023.112593可变形多孔介质中应变定位和开裂的 Cosserat 周缘力学计算Strain localization and cracking in porous media are significant issues in engineering and science. Periporomechanmics is a strong nonlocal framework for modeling the mechanics and physics of porous media with evolving discontinuities. In periporomechanics, the horizon that usually lacks a physical meaning serves as a nonlocal parameter. In this article, as a new contribution, we formulate a Cosserat periporomechanics paradigm incorporating a micro-structure related length scale for modeling shear banding and cracking in dry porous media. In this new Cosserat-periporomechanics framework, each material point is endowed with both translational and rotational degrees of freedom following the Cosserat continuum theory. We formulate a stabilized Cosserat constitutive correspondence principle through which classical micro-polar constitutive models for porous media can be used in Cosserat periporomechanics. We have numerically implemented the Cosserat periporomechanics paradigm through an explicit Lagrangian meshfree algorithm. We first present numerical examples to validate the implemented computational Cosserat periporomechanics paradigm for modeling shear bands and cracks. We then present numerical examples to demonstrate the efficacy and robustness of the Cosserat periporomechanics for modeling the shear banding bifurcation and crack branching in dry porous media.多孔介质中的应变局部化和开裂是工程和科学领域的重大问题。周界力学是一个强大的非局部框架,用于模拟具有不断变化的非连续性的多孔介质的力学和物理学。在周界力学中,通常缺乏物理意义的地平线可作为非局部参数。在本文中,作为一项新贡献,我们提出了一种 Cosserat 周缘力学范式,该范式结合了与微结构相关的长度尺度,用于模拟干燥多孔介质中的剪切带和裂缝。在这一新的 Cosserat 周缘力学框架中,每个材料点都被赋予了 Cosserat 连续理论的平移和旋转自由度。我们提出了一个稳定的 Cosserat 构成对应原理,通过该原理,多孔介质的经典微极性构成模型可用于 Cosserat 周界力学。我们通过显式拉格朗日无网格算法,在数值上实现了 Cosserat 周缘力学范式。我们首先通过数值示例验证了用于剪切带和裂缝建模的 Cosserat 周缘力学计算范式。然后,我们以数值实例证明了 Cosserat 周缘力学在干多孔介质剪切带分叉和裂缝分支建模中的有效性和稳健性。Determination of flexoelectric coefficients of higher-order continuum theories from CsCl lattice modelMoonhong Kim, Seunghun Lee, Dongwoo Sohn, Hyun-Gyu Kimdoi:10.1016/j.ijsolstr.2023.112596从氯化铯晶格模型确定高阶连续理论的柔电系数Flexoelectricity is an electromechanical coupling phenomenon between inhomogeneous deformation and electric polarization. The classical theory, which relies on the strain, is insufficient for representing flexoelectricity. Instead, a higher-order continuum theory that employs a measure capable of expressing local inhomogeneous deformation is necessary. In the present work, we concatenate higher-order continuum theories with a CsCl lattice structure consisting of charged particles and determine the resulting constitutive coefficients for higher-order continuum theories. First, we derived continuum internal energy density functions for dielectrics from the conservation laws. We consider two different higher-order continuum theories: coupled stress and strain gradient theories. Second, we present a procedure for determining the coefficients of higher-order continuum theories by using a discrete lattice model under the assumption that the internal energies of the lattice and continuum models are the same for identical deformations. To validate the coefficients, three sample problems are examined by presenting their analytical solutions. The results of sample problems demonstrate that the two higher-order theories can provide quantitative information about the size and flexoelectric effects. In particular, the strain gradient theory predicts the deformation of the lattice structure more accurately.挠电是不均匀变形与电极化之间的一种机电耦合现象。依靠应变的经典理论不足以表现挠电现象。取而代之的是一种高阶连续理论,它采用了一种能够表达局部不均匀变形的量度。在本研究中,我们将高阶连续理论与由带电粒子组成的氯化铯晶格结构结合起来,并确定了由此产生的高阶连续理论的构成系数。首先,我们根据守恒定律推导出了电介质的连续内能密度函数。我们考虑了两种不同的高阶连续理论:耦合应力和应变梯度理论。其次,我们提出了一种通过使用离散晶格模型来确定高阶连续理论系数的程序,该程序的假设是,在相同变形情况下,晶格模型和连续模型的内能是相同的。为了验证这些系数,我们对三个示例问题进行了研究,并给出了它们的分析解。样本问题的结果表明,两种高阶理论可以提供有关尺寸和挠电效应的定量信息。尤其是应变梯度理论能更准确地预测晶格结构的变形。Journal of the Mechanics and Physics of SolidsInfluence of nearby fiber on fiber–matrix debonding: Coupled Criterion prediction and debonding shape determinationH. Girard, A. Doitrand, B. Koohbor, R.G. Rinaldi, N. Godin, D. Long, J. Bikarddoi:10.1016/j.jmps.2023.105498附近纤维对纤维-基体脱粘的影响:耦合标准预测和脱胶形状确定Fiber-matrix interface debonding in two-fiber specimens under remote tensile loading is studied both experimentally and numerically by means of a coupled stress and energy criterion. Depending on its relative position, the neighboring fiber induces a perturbation of both stress and energy fields at the reference fiber interface which results in asymmetrical debonding initiation and propagation. The determination of the debonding initiation and propagation shape is addressed based on either (i) stress isocontours, (ii) energy isocontours or (iii) the Coupled Criterion (CC). It was found that the debonding initiation configuration can be determined based on stress (respectively energy) isocontours for small (respectively large) enough interface brittleness number. For intermediate brittleness number, the debonding initiation configuration cannot be obtained using neither the stress nor the energy isocontours, but requires a coupling of both aspects. Despite different initiation debonding configurations, the corresponding initiation remote stresses do not differ much, which results in similar debonding configurations after unstable crack propagation following initiation.通过应力和能量耦合准则,对远程拉伸加载下双纤维试样中的纤维-基体界面剥离进行了实验和数值研究。根据其相对位置,邻近纤维会在参考纤维界面上引起应力场和能量场的扰动,从而导致非对称的脱粘开始和传播。脱粘开始和传播形状的确定基于 (i) 应力等值线、(ii) 能量等值线或 (iii) 耦合准则 (CC)。研究发现,在界面脆性数足够小(分别为足够大)的情况下,可以根据应力(分别为能量)等值线确定脱粘起始构型。对于中等脆性数,既不能使用应力等值线,也不能使用能量等值线,而是需要将这两方面耦合起来,才能获得脱粘起始构型。尽管起始脱粘构型不同,但相应的起始远应力差别不大,这就导致起始后裂纹不稳定扩展后的脱粘构型相似。A theoretical model to determine solid surface tension through droplet on film configuration and experimental verificationFeng Du, Pengyu Lv, Hongyuan Li, Jianxiang Wang, Li-Hua Shaodoi:10.1016/j.jmps.2023.105504通过膜上液滴构型确定固体表面张力的理论模型及实验验证Determination of the surface tension of solids has been a challenging issue. This work presents an approach to the issue based on the configuration of a droplet spreading on a free standing film. Firstly, a theoretical model for the equilibrium configuration of a droplet spreading on a film is developed, which reveals that the surface elasticity has little contribution to the equilibrium configuration, and the effective strain of the film is determined by the bulge angle analytically. Based on these observations, a new procedure is presented to measure the surface tension of the film through droplet loading, which is realized by extrapolating the film tension as a function of the product of the film thickness and the effective strain. Finally, as a validation, we use this approach to extract the surface tension of soft elastomers. This work provides a viable and robust approach to determination of the surface tension of solids.固体表面张力的测定一直是一个具有挑战性的问题。这项研究提出了一种基于液滴在独立薄膜上扩散的构型来解决这一问题的方法。首先,建立了液滴在薄膜上扩散的平衡构型理论模型,发现表面弹性对平衡构型的贡献很小,薄膜的有效应变由凸起角分析确定。基于这些观察结果,我们提出了一种通过液滴加载测量薄膜表面张力的新程序,该程序通过将薄膜张力推断为薄膜厚度和有效应变乘积的函数来实现。最后,作为验证,我们使用这种方法提取软弹性体的表面张力。这项工作为测定固体表面张力提供了一种可行且稳健的方法。Mechanics of MaterialsNanoscale dynamic mechanical analysis of a viscoelastic matrix inclusion within an elastic substrateOfer Braunshtein, Yaniv Shelef, Benny Bar-Ondoi:10.1016/j.mechmat.2023.104873对弹性基底中的粘弹性基质包含物进行纳米级动态力学分析Advanced composite materials incorporate viscoelastic matrix inclusions in designated locations within elastic substrates, which grant them specialized energy dissipation capabilities of dynamic loadings. Identifying the local nanomechanical properties of the matrix-substrate complex within the composite is critical to its design and adaptation toward a specific target function. Here, we conduct FE simulations of nanoscale dynamic mechanical analysis (DMA) testing on hemispherical matrix inclusions within elastic substrates and analyze the variations in its indentation storage loss moduli measures for different matrix-substrate configurations. Then, we describe the mechanical system by simple spring models, identify the dominating parameters at different contact states of the nanoscale DMA testing, and obtain highly accurate analytical formulae that link the indentation measures of the matrix-substrate complex to the individual mechanical properties of the matrix and substrate parts. Our analysis can be directly integrated into benchmark nanomechanical testing methodologies of composite materials and promotes the local dynamic-mechanical characterization of complex materials systems, including nanomaterials, micro-architected structures, and bio-inspired designs.先进的复合材料在弹性基体的指定位置加入粘弹性基体夹杂物,使其在动态载荷下具有特殊的能量消耗能力。确定复合材料中基质-基底复合体的局部纳米力学性能,对其设计和适应特定目标功能至关重要。在此,我们对弹性基底中的半球形基质夹杂物进行了纳米级动态力学分析(DMA)测试的有限元模拟,并分析了不同基质-基底配置下压痕存储损耗模量的变化。然后,我们用简单的弹簧模型描述了机械系统,确定了纳米级 DMA 测试中不同接触状态下的主导参数,并获得了高精度的分析公式,将基体-基底复合体的压痕测量值与基体和基底部分的单个机械特性联系起来。我们的分析可直接集成到复合材料的基准纳米力学测试方法中,并促进复杂材料系统(包括纳米材料、微架构结构和生物启发设计)的局部动态力学表征。Thin-Walled StructuresAnalysis on aeroelastic stability of rectangular-planed air-supported membrane structuresKeye Yan, Yue Wu, Zhaoqing Chen, Junbin Zhaodoi:10.1016/j.tws.2023.111416矩形平面气撑膜结构的气弹稳定性分析This research investigates aeroelastic stability of rectangular air-supported membrane structures subjected to wind actions. By employing potential theory to tackle air flows, the relations between extra aerodynamic forces and structural motions are resolved through the utilization of the boundary element method and the finite element method, capturing the complexities associated with structural geometries and wind pressure distributions. By combining these extra aerodynamic forces with structural dynamic equilibrium equations, critical instability wind velocities for various structural vibration modes are derived. The simulation results are validated through aeroelastic wind tunnel tests, demonstrating a close alignment between the numerical findings and experimental observations in terms of the critical wind velocity and the corresponding instability mode. Additionally, the study analyzes influences of structural geometric configurations, internal pressures, and membrane tensile stiffness on the critical instability wind velocities and corresponding instability modes. It is observed that lower aspect ratios, smaller structural spans, higher internal pressures, and greater membrane tensile stiffness can increase the critical instability wind velocity, corresponding to variations in critical instability mode shapes. Results obtained from this research are expected to provide guidance for the development of wind-resistant designs for air-supported membrane structures.本研究探讨了矩形气撑膜结构在风力作用下的气动弹性稳定性。通过采用势理论处理气流,利用边界元法和有限元法解决了额外气动力和结构运动之间的关系,捕捉到了与结构几何形状和风压分布相关的复杂性。通过将这些额外的空气动力与结构动态平衡方程相结合,得出了各种结构振动模式的临界失稳风速。通过气动弹性风洞试验对模拟结果进行了验证,结果表明在临界风速和相应的失稳模式方面,数值结果与实验观测结果非常吻合。此外,研究还分析了结构几何配置、内部压力和膜拉伸刚度对临界失稳风速和相应失稳模式的影响。研究发现,较低的长宽比、较小的结构跨度、较高的内部压力和较大的膜拉伸刚度都会提高临界失稳风速,从而导致临界失稳模式形状的变化。这项研究的结果有望为开发空气支撑膜结构的抗风设计提供指导。Dynamic modeling and simulation for pneumatic landing airbag system with frictional contactBo Lei, Tingting Yuan, Jinyang Liu, Caishan Liudoi:10.1016/j.tws.2023.111417带摩擦接触的气动着陆安全气囊系统的动态建模与仿真The landing airbag system is a mechanism composed of thin-walled structures designed to ensure the safe landing of a lander. To investigate the dynamic behavior of the landing airbag with large deformations, a novel modeling approach incorporating gas exchange and frictional contact is proposed. The Absolute Nodal Coordinate Formulation (ANCF) is introduced to model the flexible airbag. Subsequently, the gas parameters inside the airbag are calculated by integrating the Control Volume (CV) Method and the energy conservation equation. Additionally, based on master–slave techniques, a frictional contact formulation for the thin-walled structure and the rigid plane is presented, in which the normal contact force is estimated using the penalty method, and the velocity-based friction model accounting for the stick–slip transition characterizes the tangential friction. Furthermore, the bounding box technology is adopted to improve contact detection efficiency. A series of numerical examples are performed, which demonstrates the proposed model’s advantages in terms of precision and versatility. Finally, the landing dynamic characteristics of the airbag landing system for the small lunar lander are successfully revealed, and the parameter analysis for the airbag system is expected to aid the design optimization of the airbag cushioning system.着陆气囊系统是一种由薄壁结构组成的装置,旨在确保着陆器安全着陆。为了研究着陆气囊在大变形情况下的动态行为,提出了一种包含气体交换和摩擦接触的新型建模方法。该方法引入了绝对节点坐标公式(ANCF)来模拟柔性气囊。随后,通过整合控制体积(CV)法和能量守恒方程,计算出安全气囊内部的气体参数。此外,基于主从技术,提出了薄壁结构与刚性平面的摩擦接触公式,其中法向接触力使用惩罚法估算,而基于速度的摩擦模型考虑了粘滑过渡,表征了切向摩擦。此外,还采用了边界框技术来提高接触检测效率。通过一系列数值示例,证明了所提模型在精度和通用性方面的优势。最后,成功揭示了小型月球着陆器气囊着陆系统的着陆动态特性,气囊系统的参数分析有望帮助气囊缓冲系统的优化设计。Analysis of Negative Stiffness Structures with B-spline Curved BeamsSize Ai, Jianzheng Wei, Zhimin Xie, Huifeng Tandoi:10.1016/j.tws.2023.111418利用 B-样条曲线梁分析负刚度结构With unique mechanical properties, negative stiffness (NS) structures have presented significant advantages in energy absorption. In recent years, NS structures consisting of periodically arranged curved beams have attracted comprehensive attention. However, the curved beams of the current report mainly focus on geometrical parameters in specific configurations, and the variety of the reported geometrical configurations of the flexible beams is relatively limited. In this paper, a B-spline curved beam design method is proposed. A static analysis model of a B-spline curved beam is developed to investigate the force-displacement relations of curved beams in different configurations. The configuration for the B-spline curved beam is obtained, and the relation between the geometric parameters and the mechanical properties of the B-spline curved beam is discussed. Then the mechanical properties of NS structures with periodically arranged B-spline curved beams are analyzed by the finite element method (FEM), and the experiments verified the correctness of the simulation method. Finally, the force-displacement relation and energy-absorption properties of gradient NS structures with B-spline curved beams are discussed. The results indicate that the NS structure with B-spline curved beams has repeatability and effective energy absorption properties. The deformation form of the NS structure can be modulated by gradient NS design, and the energy absorption properties of the NS structure can be improved effectively. The research can provide a reference for the design of NS structures.负刚度(NS)结构具有独特的机械特性,在能量吸收方面具有显著优势。近年来,由周期性排列的曲线梁组成的负刚度结构引起了广泛关注。然而,目前所报道的曲线梁主要集中在特定配置的几何参数上,所报道的柔性梁的几何配置种类相对有限。本文提出了一种 B-样条曲线梁设计方法。建立了 B-样条曲线梁的静态分析模型,以研究不同配置下曲线梁的力-位移关系。得到了 B-样条曲线梁的构型,并讨论了 B-样条曲线梁的几何参数与力学性能之间的关系。然后用有限元法(FEM)分析了周期性布置 B-样条曲线梁的 NS 结构的力学性能,并通过实验验证了模拟方法的正确性。最后,讨论了带有 B-样条曲线梁的梯度 NS 结构的力-位移关系和能量吸收特性。结果表明,带 B-样条曲线梁的 NS 结构具有可重复性和有效的能量吸收特性。通过梯度 NS 设计可以调节 NS 结构的变形形式,有效改善 NS 结构的能量吸收性能。该研究可为 NS 结构的设计提供参考。来源:复合材料力学仿真Composites FEM

未登录
还没有评论
课程
培训
服务
行家
VIP会员 学习 福利任务 兑换礼品
下载APP
联系我们
帮助与反馈