复合材料层合结构冲击损伤研究进展

分析总结了复合材料层合结构冲击损伤破坏形式及特征,以及冲击损伤产生和扩展机理;综述了国内外冲击损伤理论和冲击损伤检测的研究进展。探讨了复合材料层合结构冲击损伤研究的发展趋势。     

不同铺层厚度复合材料的低速冲击特性与损伤模式研究

复合材料凭借其轻质、高强的特性逐渐在工程材料界占据重要地位,对于复合材料的冲击损伤的研究也一直吸引着诸多研究学者的关注．为表征不同铺层厚度复合材料层合板的抗冲击性能,利用自由落体冲击设备,进行了复合材料层合板的冲击实验研究．给出了不同冲击能量下的损伤模式,并利用位移、速度、接触力以及能量的时间变化曲线,深入分析了侵入和穿透两种损伤模式的特点．研究发现,随着铺层厚度的增加,复合材料在冲击过程中吸收的能量也随之增加．引入能量平衡法,基于体系的能量守恒定律,利用Newton-Raphson数值方法求解了侵入损伤模式下的接触力大小,通过实验结果给定挠度求解了对应的速率变化情况,并将理论结果与实验结果进行比较．     

复合材料层合板三维线性理论的完整性

本文针对文献[1]所述复合材料层合板三维模型,在三维线性弹性理论基本方程和经典变分原理的基础上,通过分块矩阵运算和线性Lagrange乘子法,推导出比文献[1]更全面更系统的基本方程和变分原理,使复合材料层合板三维线性理论臻于完整。     

复合材料对称层合板单向拉伸与面内剪切下的三维应力分析

本文给出了单向拉伸与面向剪切载荷下复合材料对称层合板中心区域的应力和应变沿板厚的数值计算分布规律。计算结果表明，在斜交对称辅层的层合板中心区域层间界面附近存在着层间边界层效应。层间界面处纤维走向的突变导致局部的三维应力状态和很强的应力集中。     

层合板壳脱层曲面的有限元分析

通过建立一类新的参考面有限单元,得到适应于分析层合板壳脱层屈曲问题的有限元方法,指出了利用Ｍｉｎｄｌｉｎ假设意义下的变形协调条件,可以将大多数胜任层合板壳分析的一般板壳单元改造为相应的参考面单元,这一方法确保了位移场的合理性和协调条件满足,为验证参考而单元的有效性和协调还对壳体脱层屈曲的几个算例作了数值分析。     

受弯层合板边缘效应数值-摄动分析*

本文将分析一个受弯复合材料层合板的计算模型.首先利用无量纲变量将层合板任一层的平衡方程变成以位移表示的摄动型微分方程式;然后利用合成展开法,将求解区域分成内部区域和边界层区域,并推导出求解外部解和内部解的数学模型.为突出边缘效应,最后用边界积分方程表示内部解.     

层合板一个新的高队理论解析解

本以复合材料的Ｒｅｄｄｙ高阶理论为基础，引进一个位移函数Φ，将原来求解的微分方程组转化为一个高阶微分方程，得到了四边简支情况下的Ｎａｖｉｅｒ型解，和一对边简支另一对边任意情况下的Ｌｅｖｙ型解，中列举了算例进行比较，其数值结果和献上已有结果相吻合，表明本采用的解法是可靠的，Ｒｅｄｄｙ高阶理论未知数不多，但精度比一阶剪切变形理论要好，计算时地需剪切修正系数，计算较为简单。     

不同铺层厚度复合材料的低速冲击特性与损伤模式研究

复合材料凭借其轻质、高强的特性逐渐在工程材料界占据重要地位,对于复合材料的冲击损伤的研究也一直吸引着诸多研究学者的关注.为表征不同铺层厚度复合材料层合板的抗冲击性能,利用自由落体冲击设备,进行了复合材料层合板的冲击实验研究.给出了不同冲击能量下的损伤模式,并利用位移、速度、接触力以及能量的时间变化曲线,深入分析了侵入和穿透两种损伤模式的特点.研究发现,随着铺层厚度的增加,复合材料在冲击过程中吸收的能量也随之增加.引入能量平衡法,基于体系的能量守恒定律,利用Newton-Raphson数值方法求解了侵入损伤模式下的接触力大小,通过实验结果给定挠度求解了对应的速率变化情况,并将理论结果与实验结果进行比较.     

对称复合材料层合板弯曲的三维数值分析

本文采用三维各向异性有限单元模拟纯弯曲载荷下的复合材料层合板，给出了应力、应变沿厚度方向的变化规律。分析结果表明，在斜交对称铺层层合板的中心区域（远离加载端和自由边的区域），板的层间粘接界面附近，有根强的应力集中现象，可称之为层间效应。层间界面处力学性质的突变导致了层间应力的产生，并使层合板处于三向应力状态。三维数值模型给出的应变分布不同于基于Ｋｉｒｃｈｈｏｆｆ－Ｌｏｖｅ直法线假设的经典层合板理论给出的应变分布。     

具界面损伤压电智能层合板的非线性自由振动分析

基于广义6自由度板理论、应变等效原理和Hamilton变分原理,通过引入三维弹性平衡方程和静电平衡方程的通解来构造满足界面间力电耦合关系和各类连续条件的位移、电势分布形函数,建立了具铺设层内和层间界面处损伤效应的压电智能层合板的非线性运动控制方程组,并运用Galerkin 方法进行求解.数值算例中,分别讨论了,不同损伤程度、压电层厚度、厚跨比及长宽比对四边简支非理想界面压电智能层合板线性自由振动频率和非线性幅频响应曲线的影响.     

一般各向异性复合材料层板基体损伤性能衰减研究(Ⅱ)——分解刚度值确定与层板性能衰减研究

本文尝试将损伤复合材料层板性能衰减研究扩展到含一般各向异性铺层的基体开裂层板对第(Ⅰ)部分提出的分解刚度法给出分解刚度值确定方程,完整了开裂层板本构关系解;对(θm/90n)s开裂层板刚度衰减进行了数值计算并对计算结果进行了讨论.     

一般各向异性复合材料层板基体损伤性能衰减研究(Ⅰ)——分解刚度法建立(θ_m/90_n)_s开裂层板本构关系

本文尝试将损伤复合材料层板性能衰减研究扩展到含一般各向异性铺层的基体开裂层板·在第一部分中，采用分解刚度法处理法向与剪切响应的耦合问题，对承受面内载荷的对称约束开裂（θｍ／９０ｎ）ｓ层板，导出本构关系的近似解析解，将层板有效刚度表为裂纹密度的函数     

Design of Microstrip Antennas with Composite Laminates Considering Their Structural Rigidity

Two types of conformal load-bearing antenna structures (CLAS) were designed with microwave composite laminates and Nomex honeycomb cores to secure both the structural rigidity and a good electrical performance. One was a 4 × 8 array for the synthetic-aperture radar (SAR) system and the other was a 5 × 2 array for the wireless local-area network (LAN) system. The design was based on a wide bandwidth, high polarization purity, low losses, and high structural rigidity. The design, fabrication, and structural/electrical performances of the antenna structures were studied. Their flexural behavior was examined by three-point bending, impact, and buckling tests. The electrical measurements were in a good agreement with simulation results. The complex antenna structures obtained have good flexural characteristics. The design of this antenna structure is extended to give a useful guide for sandwich panel manufacturers as well as antenna designers.     

Estimation of laminate stiffness reduction due to cracking of a transverse ply by employing crack initiation-and propagation-based master curves

The applicability range of toughness-and strength-based criteria for progressive cracking of a transverse layer in a cross-ply composite laminate subjected to tensile loading is considered. Using a deterministic cracking model, approximate relations for the crack density as a function of stress are derived for initiation-and propagation-controlled types of cracking. The master-curve approach is applied to progressive cracking in glass/epoxy laminates. The accuracy of estimation of laminate stiffness reduction by using crack density master curves is evaluated. Russian translation published in Mekhanika Kompozitnykh Materialov, Vol. 44, No. 5, pp. 633–646, September–October, 2008.     

Damage behavior of laminated E-glass/epoxy beams with an initial delamination subjected to an axial impact

The damage behavior of laminated E-glass/epoxy beams, with and without an initial delamination, subjected to an axial impact by a moving bullet has been investigated experimentally and numerically. The specimens were made from a unidirectional fiber fabric stacked in the sequences [0₆] _s , [±45₃] _s , and [90₆] _s , and a delamination was created in them by locating a copper foil at a specified position. The data on the bullet speed and strain history were recorded by a laser setup, a high-speed dynamic strain indicator, and a TDS420A oscilloscope. It is shown that the delamination and the ply stacking sequence play a significant role in the dynamic response and damage behavior of laminated beams. A numerical simulation is performed by using the commercial finite-element software ABAQUS/Explicit, and the results obtained are in a good agreement with experimental observations. Russian translation published in Mekhanika Kompozitnykh Materialov, Vol. 45, No. 1, pp. 49–64, January–February, 2009.     

Modeling the nonlinear deformation of composite laminates based on plasticity theory

The plasticity theory has been successfully used for describing the nonlinear deformation of laminated composite materials under a monotonically increasing loading. Generally, several tests are needed to determine the parameters of the plastic potential for a laminate. We explore an alternative approach and obtain the plastic potential by using theoretical considerations based on a laminate analysis. The model is shown to provide an accurate prediction for the response of a cross-ply glass/epoxy laminate under uniaxial tensile loading at different angles to the material orthotropy axes. Russian translation published in Mekhanika Kompozitnykh Materialov, Vol. 43, No. 3, pp. 309–318, May–June, 2007.     

Analysis of Thick Laminated Composite Plates on an Elastic Foundation with the Use of Various Plate Theories

In this study, various theories of composite laminated plates are extended to rectangular composite laminates resting on an elastic foundation. First, an analysis based on the classical theory of laminated plates is employed. Then the first-order Reissner-Mindlin theory is used for analyzing the laminates. At last, the Reddy shear deformation theory, which allows for the transverse shear strains, is applied to the bending analysis of the laminates. In the analysis, the two-parameter Pasternak and Winkler foundations are considered. The accuracy of the present analysis is demonstrated by solving problems numerical results for which are available in the literature. Some numerical examples are presented to compare the three methods and to illustrate the effects of parameters of the elastic foundations on the bending of shear-deformable laminated plates. __________ Russian translation published in Mekhanika Kompozitnykh Materialov, Vol. 41, No. 5, pp. 663–682, September–October, 2005.     

碳纤维-不锈钢层板热载条件下冲击动态响应及层间损伤仿真研究

为了研究碳纤维不锈钢层板的冲击动态响应以及热载荷条件下的冲击性能,采用ABAQUS/Explicit,编写基于复合材料渐进损伤用户子程序VUMAT;引入Johnson-Cook模型,仿真计算了碳纤维增强环氧树脂基复合材料-SS304不锈钢层板热载条件下冲击动态响应过程;分析了其冲击动态响应及渐进损伤,着重讨论了热载荷条件对碳纤维金属层板的冲击能量吸收、接触力等抗冲击性能及失效模式的影响.结果显示,高速冲击载荷作用下,纤维层的脆性断裂、金属层的塑性变形以及纤维层与金属层之间的脱层是碳纤维不锈钢层板的主要失效形式.热载荷的存在直接影响了冲头的接触力,随环境温度升高,接触力总体上降低,子弹的速度衰减越慢,剩余速度增大.结果表明,热载荷降低了纤维金属板的冲击动能吸收特性,弱化了碳纤维金属板的抗冲击性能.无论是纤维金属层板的整体破坏,还是纤维失效、基体失效和脱层失效,热载荷都产生了重要影响.