微液滴在PDMS软基体表面的动态摩擦行为研究

通过固液界面摩擦力测试装置研究了微液滴在PDMS软基体表面运动时的动态摩擦学行为,并对微液滴体积、滑动速度及软基体力学性能对固液界面动态摩擦行为的影响进行了分析. 结果表明:微液滴在软基体表面运动时表现出最大静摩擦力和动态摩擦力. 最大静摩擦力与微液滴黏度和速度梯度呈正比,动态摩擦力与微液滴体积、滑动速度和基体力学性能有关. 随着微液滴体积的增加,三相接触线长度增加,动态摩擦力增加;随着相对滑动速度增加,三相接触线长度及接触角滞后增加,动态摩擦力增加;随着软基体弹性模量降低,固液界面黏附力增加,固液界面运动能量耗散增加,动态摩擦力增加. 研究结果可为PDMS软基体表面微液滴的精确驱动和运动参数优化提供理论指导,也可进一步丰富固液界面摩擦理论.      

基于分子动力学的结合材料界面破坏准则

结合材料的破坏通常都是从界面或其附近发生的,但界面破坏的机理及其评价准则尚未十分清楚.采用分子动力学模拟方法,可以对结合材料的界面破坏过程进行模拟,从而获得结合材料的界面应力和界面破坏之间的关系.界面破坏可以分为奇异应力场作用下的破坏,和界面应力集中引起的破坏两种.虽然在分子动力学模拟中采用了高度简化的界面模型,但对界面破坏过程的模拟,仍可以帮助人们获得结合材料界面破坏过程的规律性认识.分别模拟远场作用下界面上存在初始裂纹和界面附近存在初始裂纹两种情况下的界面破坏,根据分子动力学模拟结果,提出了一个结合材料界面破坏的准则.     

复合材料非破坏性测试

非破坏性测试用于检验材料和结构的内在特征,了解构件原有缺陷对性能的影响,并在进行各种载荷条件下力学性能试验时观察或试验后检查构件的破坏过程,以分析和确定构件的强度、刚度、断裂、疲劳、振动等力学性能以及破坏机理,复合材料由两种以上的增强元件及基体构成,材料本身就是一种力学结构,如纤维增强复合材料,纤维是主要承力件,基      

基于实验的反演识别方法及其在材料力学性能研究中的应用

本文介绍了基于实验的反演识别方法,综述了该方法在材料力学以及界面力学性能研究中的应用.内容包括:讨论了基于实验反演识别整体化策略与若干关键技术,比较了几种识别算法的优缺点,给出了在金属基复合材料界面力学损伤与破坏及考虑时间效应的粘接界面力学模型与实验表征方面的应用,简介了在其它材料力学性能研究等方面取得的进展.最后,对该实验分析方法发展趋势进行简要评述.     

异质双材料粘接梁的界面端部应力及端部龟裂破坏的实验应力分析

本文采用了高灵敏度的云纹干涉法对异质双材料粘接梁在弯曲载荷作用下的位移进行了测量，用局部杂交法对界面端部区域的应变和应力进行了计算。通过对该区域内的实验应力分析发现：拉应力σｘ是影响结构强度的关键因素。本文还对在基体材料表面近角点区域可能出现的龟裂破坏的原因进行了分析。     

沟槽表面填充材料对界面摩擦振动噪声的影响

采用机械加工方式,在基体(蠕墨铸铁)表面加工出平行且等间距的沟槽,并在沟槽中分别填满铝材料和锻钢材料,对该填充材料试样和基体试样进行界面摩擦噪声试验,并采用数值模拟方法加以分析,得出界面摩擦振动噪声行为在不同沟槽填充材料下的变化特性,并将不同界面摩擦磨损行为与振动噪声动态关联起来.试验及数值模拟结果表明,在沟槽中填充铝材料加剧界面磨损,增大摩擦系数,并加速系统不稳定振动的产生,增大噪声强度,而在沟槽中填充钢材料能有效延缓界面不稳定振动和摩擦尖叫噪声信号的产生.此外,计算结果表明,界面磨擦磨损行为导致的界面接触非线性特性是产生多频率不稳定振动和噪声的重要因素.     

涂层式裂纹监测系统中基体裂纹穿越行为研究

建立了智能涂层的两相模型与三相模型,基于能量准则分别用这两种模型研究了基体裂纹达到涂层界面后的穿越/偏转行为. 用有限元法分析了相对裂纹扩展长度、弹性错配参数及界面层厚度对偏转裂纹与穿越裂纹能量释放率之比的影响,结果表明当基体裂纹到达驱动层与基体界面时,能量释放率之比不仅与基体和驱动层之间的弹性错配相关,而且当驱动层较薄时对驱动层与传感层之间的弹性错配亦有较强的依赖性. 此外,随着驱动层厚度的增加,能量释放率之比对驱动层与传感层之间的弹性错配的依赖性逐渐降低. 通过与实验结果相比,建立的模型能够较好的解释基体裂纹在界面的扩展行为,可用于智能涂层裂纹传感器的优化设计.      

双层薄膜与弹性梯度基底三层结构表面失稳分析

硬薄膜/软基底结构的表面失稳问题一直是柔性电子器件的难题,基于此,本文考虑了双层结构与弹性梯度基底间的界面剪切力,建立了双层薄膜/弹性梯度基底模型;利用位移协调条件,理论推导得到了双层薄膜/弹性梯度基底结构的临界应变和失稳波长的表达式并通过有限元仿真,验证了本研究解析解的有效性。在此基础上,应用此解析解进一步研究了弹性梯度基底的材料、双层薄膜结构厚度比等参数对临界应变和波长的影响。结果表明：减小器件层的厚度或者增加封装层的厚度,可以提高双层膜/弹性梯度基底结构的稳定性;当弹性梯度材料基底表面“较软”或器件层“较硬”时,器件层与基底界面的剪切力的影响较大,可以提升三层膜/基结构抵抗界面破坏的能力。本研究成果将为硬薄膜/弹性梯度基底结构的柔性电子器件的制备提供理论支撑。     

钢筋混凝土界面的近场动力学方法

近场动力学方法已被广泛用于钢筋混凝土的开裂破坏研究,传统近场动力学方法的控制方程与参数是基于同种均质材料的能量方程确定,在处理不同种材料之间的相互作用时,无法合理反映其界面的力学行为.针对这一问题,通过分析钢筋混凝土界面的黏结-滑移机理,提出了近场动力学界面区材料点的相互作用模型,发展了考虑钢筋混凝土界面黏结的键基近场动力学方法.基于键基近场动力学与连续介质力学的能量密度等效方法,提出了界面微弹性参数的确定方法;根据钢筋肋间混凝土的应力分布规律,获得界面材料点域半径与受限楔体半径的等效关系;利用界面黏结-滑移曲线峰值应力对应的滑移变形,给出了界面临界拉伸常数确定方法.通过与2组钢筋混凝土构件的拉拔试验对比,验证了发展的界面近场动力学方法,并开展了不同条件下钢筋混凝土构件的数值试验.结果表明,发展的近场动力方法能够合理反映钢筋直径、锚固长度、混凝土强度以及肋间距对钢筋混凝土界面黏结行为的影响,体现了所提方法的合理性与优越性.     

基于离散模型的混凝土构件破坏过程研究

刚体-弹簧元模型是一种离散化分析模型,可以反映连续体从开裂到破坏不连续过程的真实裂缝形态.论文在总结既有相关研究的基础上,引入并程序化刚体-弹簧元模型用于混凝土构件开裂破坏行为研究,特别是有关混凝土构件开裂后直至破坏的裂缝真实形态研究.首先确定了三维刚体-弹簧元模型中刚体单元的划分、弹簧元的特性(混凝土材料本构关系施加于弹簧元)、刚体单元与弹簧元装配方式、钢筋本构关系及其与混凝土相互作用,然后实现了刚体-弹簧元模型用于混凝土构件开裂破坏行为研究的程序化,并以剪切破坏的钢筋混凝土构件进行实例验证.结果表明,基于刚体-弹簧元模型的程序可以较为准确地反映该钢筋混凝土构件从开裂到破坏真实裂缝形态.     

Improved theoretical solution for interfacial stresses in concrete beams strengthened with FRP plate

In this paper, an improved theoretical interfacial stress analysis is presented for simply supported concrete beam bonded with a FRP plate. The adherend shear deformations have been included in the present theoretical analyses by assuming a linear shear stress through the thickness of the adherends, while all existing solutions neglect this effect. Remarkable effect of shear deformations of adherends has been noted in the results. Indeed, the resulting interfacial stresses concentrations are considerably smaller than those obtained by other models which neglect adherent shear deformations. It is shown that both the normal and shear stresses at the interface are influenced by the material and geometry parameters of the composite beam. This research is helpful for the understanding on mechanical behavior of the interface and design of the FRP–RC hybrid structures.     

Stress-function variational method for interfacial stress analysis of adhesively bonded joints

High interfacial stresses at the free edges of adherends are responsible for the debonding failure of adhesively bonded joints (ABJs). In this paper, a general stress-function variational method is formulated to determinate the interfacial shear and normal (peeling) stresses in ABJs in high accuracy. By extending authors’ prior work in stress analysis of bonded joints (Wu and Jenson, 2011), all the planar stress components in the adherends and adhesive layer of an ABJ are expressed in terms of four unknown interfacial stress functions, which are introduced at the upper and lower surfaces of the adhesive layer. A set of governing ordinary differential equations (ODEs) of the four interfacial stress functions is obtained via minimizing the complimentary strain energy of the ABJ, which is further solved by using eigenfunctions. The obtained semi-analytic stress field can satisfy all the traction boundary conditions (BCs) of the ABJ, especially the stress continuity across the bonding lines and the shear-free condition at the ends of adherends and adhesive layer. As an example, the stress field in an adhesively single-sided strap joint is determined by the present method, whose numerical accuracy and reliability are validated by finite element method (FEM) and compared to existing models in the literature. Parameter studies are performed to examine the dependencies of the interfacial stresses of the exemplified ABJ upon the geometries, moduli and temperature change of the adherends and adhesive layer, respectively. The present method is applicable for scaling analysis of joint strength, optimal design of ABJs, etc.     

基于弹性-塑性内聚力模型的纤维拔出界面宏观行为分析

用解析法分析了单纤维从聚合物基体中的拔出过程,采用弹性—塑性内聚力模型模拟裂纹的扩展和界面失效,确定了临界纤维埋入长度,该值区分两种不同长度的纤维拔出过程. 在纤维拔出过程,界面经历不同的阶段. 纤维埋长小于临界长度时,界面的脱粘载荷与纤维的埋长成正比;超过临界长度后,界面的脱粘载荷近似为常数. 分析了界面参数对脱粘载荷的影响:增加界面的剪切强度和界面的断裂韧性,或减小界面裂纹萌生位移,均能提高界面的脱粘载荷;界面脱粘后无界面摩擦应力时,拔出载荷—位移曲线的峰值载荷等于界面的脱粘载荷;界面摩擦应力存在时,使峰值载荷大于脱粘载荷,需要较长的纤维埋入长度和较大的界面摩擦应力.      

Dynamic interfacial debonding initiation induced by an incident crack

When a crack propagates towards a weak interface, interface debonding may occur before the incident crack reaches the interface. This phenomenon refers to the “Cook–Gordon mechanism”. In this investigation, an equivalent dynamic Cook–Gordon mechanism is studied both experimentally and analytically. Two strength-based criteria incorporating dynamic fracture mechanics analysis are proposed to predict the initiation location of interface debonding ahead of a dynamic incident crack. As validation, a comparison is made between the analytical predictions and experimental measurements. Results show that the strength-based criteria can effectively predict the initiation of interface debonding. Meanwhile, effects of the stress intensity factor and the T stress of the incident crack, on the interfacial debonding initiation are investigated. It is concluded that high-stress intensity factors of the incident cracks will easily induce interfacial debonding initiation, and changing the T stress is an effective way to control interfacial debonding initiation. Furthermore, high-interfacial tensile strengths rather than shear strengths, tend to suppress interfacial debonding initiation induced by a mode-I incident crack.     

A model of debonding instability for solid propellant rocket motor: Part I - Uniform longitudinal and transverse stress rate

The interface between a soft and a hard material is vulnerable to debonding because of the prevailing high stress gradient that could be further aggravated under dynamic transient conditions. Such a situation is common in a solid-fuel rocket motor where unstable debonding could be triggered from the initiation of a macrocrack near the interface. The transition from a survival state to a failure state requires knowledge of how the nonlinear, dissipative and nonhomogeneous effects of the dissimilar material interface would interact with load.The solid-fuel rocket motor problem is modeled by a three-layered composite system made of steel, adhesive and rubber under plane extension. Assessed are the time dependent nonhomogeneous deformation and possible failure modes. Only initial properties of the materials were used to determine the evolution of nonequilibrium response. This is made possible by application of the isoenergy density theory that accounts for internal heat generation and energy dissipation effects. Results are presented in two parts. In Part 1, the applied stress rates are assumed to be 0.75 ksi/s in both the longitudinal and transverse direction while Part II assumes different stress rates in these two directions. At approximately one second after loading, a slanted but straight macrocrack of about 5 × 10⁻³ in. is predicted to occur in the rubber next to the interface. This initial crack was found to become unstable at eight seconds and was estimated to be close to the adhesive/rubber interface over a length of 1.88 in. The onset of fracture depended directly on the load transient behavior.     

A three-parameter elastic foundation model for interface stresses in curved beams externally strengthened by a thin FRP plate

Externally bonding of fiber reinforced polymer (FRP) plates or sheets has become a popular method for strengthening reinforced concrete structures. Stresses along the FRP–concrete interface are of great importance to the effectiveness of this type of strengthening because high stress concentration along the FRP–concrete interface can lead to the FRP debonding from the concrete beam. In this study, we develop an analytical solution of interface stresses in a curved structural beam bonded with a thin plate. A novel three-parameter elastic foundation model is used to describe the behavior of the adhesive layer. This adhesive layer model is an extension of the two-parameter elastic foundation commonly used in existing studies. It assumes that the shear stress in the adhesive layer is constant through the thickness, and the interface normal stresses along two concrete/adhesive and adhesive/FRP interfaces are different. Closed-form solutions are obtained for these two interfacial normal stresses, shear stress within the adhesive layer, and beam forces. The validation of these solutions is confirmed by finite element analysis.     

FRP加固梁的FRP-混凝土界面脱胶分析

为了研究纤维增强聚合物(fiber reinforced polymer, FRP) 加固梁的FRP-混凝土界面脱胶破坏过程,本文将混凝土梁和FRP 板均视为线弹性的欧拉-伯努利梁(Euler-Bernoulli beams), 且两者通过粘结层胶结在一起. 对于FRP-混凝土结构,有两种形式的脱胶破坏：板端脱胶破坏和跨中裂缝导致的脱胶破坏.对于FRP-混凝土梁,利用合理的粘结模型按第2 种脱胶失效形式,详细讨论了FRP-混凝土界面的脱胶过程,得到了不同阶段的胶结滑移、界面剪应力和FRP 轴向力的解析解. 实验研究验证了理论分析的结果,参数研究进一步探讨了胶结长度和粘结层厚度对于FRP-混凝土界面脱胶行为的影响.     

含胶接缺陷的椭球泡沫夹层结构破坏机理与承载能力研究

采用试验和有限元方法,对含胶接缺陷的椭球泡沫夹层结构在外压作用下的破坏模式和承载能力进行了研究。针对国内在研的大尺寸椭球泡沫夹层结构,实施了全尺寸静力外压试验,发现初始胶接缺陷破坏了夹层结构界面应力传递的连续性;随着载荷增加,面板发生皱褶且脱胶界面继续扩展,从而降低结构整体承载能力。通过红外无损检测确定了缺陷的类型和形貌;采用预留相应初始脱粘面积、脱粘间隙以及内聚力单元模拟界面脱粘的有限元分析方法,对含胶接缺陷的椭球泡沫夹层结构承载能力进行预测。数值结果表明:含胶接缺陷结构易发生面板皱褶,且结构顶部和根部区域较易发生界面脱粘扩展。数值和试验结果取得了较好的一致性,本文结果可为同类结构设计提供参考。     

Higher order model for soft and hard elastic interfaces

The present paper deals with the derivation of a higher order theory of interface models. In particular, it is studied the problem of two bodies joined by an adhesive interphase for which “soft” and “hard” linear elastic constitutive laws are considered. For the adhesive, interface models are determined by using two different methods. The first method is based on the matched asymptotic expansion technique, which adopts the strong formulation of classical continuum mechanics equations (compatibility, constitutive and equilibrium equations). The second method adopts a suitable variational (weak) formulation, based on the minimization of the potential energy. First and higher order interface models are derived for soft and hard adhesives. In particular, it is shown that the two approaches, strong and weak formulations, lead to the same asymptotic equations governing the limit behavior of the adhesive as its thickness vanishes. The governing equations derived at zero order are then put in comparison with the ones accounting for the first order of the asymptotic expansion, thus remarking the influence of the higher order terms and of the higher order derivatives on the interface response. Moreover, it is shown how the elastic properties of the adhesive enter the higher order terms. The effects taken into account by the latter ones could play an important role in the nonlinear response of the interface, herein not investigated. Finally, two simple applications are developed in order to illustrate the differences among the interface theories at the different orders.     

EXPERIMENTAL INVESTIGATIONS OF STRENGTH,TOUGHNESS AND FAILURE MECHANISM OF THE METAL/EPOXY/METAL ADHESIVE SYSTEM

本文系统地开展了金属/环氧/金属胶结体系的强韧机理及失效行为实验研究,针对铝合金圆棒与铝合金圆棒通过环氧树脂胶层的各种斜截面方向粘结,实验观测了该体系的拉伸变形和失效行为,测量了界面失效载荷对胶层厚度和粘结界面倾斜角的依赖关系;通过引入胶结界面平均正应力、平均剪应力、平均正应变、平均剪应变等概念,可对界面失效强度进行测量,获得界面强度与界面粘结角度以及胶层厚度的关系,进而获得了铝合金/环氧胶层/铝合金体系的强度失效面以及胶结界面的断裂能和胶结体系的能量释放率.上述研究结果为深入认识金属胶结体系的强韧性能和失效机制提供了科学依据,对金属胶结体系的优化设计和性能评判具有重要指导意义.研究结果表明,铝合金/环氧胶层/铝合金体系的拉伸失效总体呈弹脆性破坏特征,失效表现为胶层粘结界面的断裂,失效强度和界面断裂能在胶层厚度为百微米量级时表现出强烈的尺度效应：界面粘结强度随着胶层厚度的减小而显著增大,临界状态的平均正应力和平均剪应力在强度破坏面上近似位于同一圆上,界面断裂能随着胶层厚度的减小而显著减小;与此同时,界面失效强度和界面断裂能也密切依赖于界面粘结角度.