三明治复合材料加筋L型接头的弯曲承载能力和损伤机理

针对一种三明治复合材料加筋L型接头,介绍了其结构形式和成型工艺,通过试验测试了接头的弯曲承载能力,分析了接头的破坏模式,并对其损伤机理进行了研究,以探求接头的技术改进路径。研究结果表明:L型接头具有良好的吸能效果,在结构发生大变形破坏时,仍具有较高的弯曲承载能力;L型接头的破坏主要发生在垂横加强筋的相交处,初始损伤是相交处侧面的玻璃钢和芯材发生界面分离;工程上应将改进L型接头垂横加强筋相交处的蒙皮和芯材之间的连接工艺作为提高接头承载能力的技术路径。     

弹性薄板的条形传递函数单元模型

应用改进的条形传递函数方法 ,建立了弹性薄板的二结线四自由度条形单元模型 ,用于分析系统的静力响应。用结线将矩形区域划分为条形单元 ,将边界结线离散 ,以内部结线和边界结点的位移和转角为未知量 ,采用三次插值 ,得到能够与有限元单元耦合求解的超级单元。利用广义函数给出了一种精确积分方法 ,可以得到有关矩阵的显式表达 ,得到提高了求解精度和效率。     

平头弹丸侵彻金属靶板的数值仿真

基于ABAQUS/Explicit非线性有限元分析程序,通过二次开发利用含损伤的Johnson-Cook本构模拟靶板材料,对刚性平头弹丸垂直侵彻不同厚度的金属靶板进行了数值仿真,实现了侵彻过程的可视化。结果表明：网格密度对计算结果有影响,但随着网格密度增加,结果趋于收敛;侵彻过程中,弹丸与靶板发生了多次碰撞,靶板的塑性变形局限在很窄的剪切带内;对数值计算结果与试验结果进行了比较,发现二者吻合得较好。相关结论对防护结构的设计具有指导意义。     

基于静力与稳定性分析的小卫星主接头选型优化

基于对预埋主接头蜂窝板的静力与稳定性分析,对小卫星主接头进行选型优化。采用三明治夹心板理论建立预埋分叉式和面板式小卫星主结构连接接头的蜂窝板试件有限元模型,分析得到了蜂窝板最大应力值与失稳载荷,通过与试验结果的对比分析确定了蜂窝板试件破坏原因。在此基础上讨论结构参数对蜂窝板承载性能的影响,确定出最优的接头设计形式。     

Static and free vibration analyses of functionally graded porous variable-thickness plates using an edge-based smoothed finite element method

The main purpose of this paper is to present numerical results of static bending and free vibration of functionally graded porous (FGP) variable-thickness plates by using an edge-based smoothed finite element method (ES-FEM) associate with the mixed interpolation of tensorial components technique for the three-node triangular element (MITC3), so-called ES-MITC3. This ES-MITC3 element is performed to eliminate the shear locking problem and to enhance the accuracy of the existing MITC3 element. In the ES-MITC3 element, the stiffness matrices are obtained by using the strain smoothing technique over the smoothing domains formed by two adjacent MITC3 triangular elements sharing an edge. Materials of the plate are FGP with a power-law index (k) and maximum porosity distributions (Ω) in the forms of cosine functions. The influences of some geometric parameters, material properties on static bending, and natural frequency of the FGP variable-thickness plates are examined in detail.     

Influence of porosity distribution on nonlinear free vibration and transient responses of porous functionally graded skew plates

This article deals with the investigation of the effects of porosity distributions on nonlinear free vibration and transient analysis of porous functionally graded skew (PFGS) plates. The effective material properties of the PFGS plates are obtained from the modified power-law equations in which gradation varies through the thickness of the PFGS plate. A nonlinear finite element (FE) formulation for the overall PFGS plate is derived by adopting first-order shear deformation theory (FSDT) in conjunction with von Karman’s nonlinear strain displacement relations. The governing equations of the PFGS plate are derived using the principle of virtual work. The direct iterative method and Newmark’s integration technique are espoused to solve nonlinear mathematical relations. The influences of the porosity distributions and porosity parameter indices on the nonlinear frequency responses of the PFGS plate for different skew angles are studied in various parameters. The effects of volume fraction grading index and skew angle on the plate’s nonlinear dynamic responses for various porosity distributions are illustrated in detail.     

Critical interfaces in body armour systems

The ballistic performance, and behaviour, of an armour system is governed by two major sets of variables, geometrical and material. Of these, the consistency of performance, especially against small arms ammunition, will depend upon the consistency of the properties of the constituent materials. In a body armour system for example, fibre diameter, areal density of woven fabric, and bulk density of ceramic are examples of critical parameters and monitoring such parameters will form the backbone of associated quality control procedures. What is often overlooked, because it can fall into the User’s domain, are the interfaces that exist between the various products; the carrier, the Soft Armour Insert (SAI), and the one or two hard armour plates (HAP1 and HAP2). This is especially true if the various products are sourced from different suppliers.There are between 30 and 150 individual layers within a typical body armour system, and each of the interfaces between each of those layers will, in some way or another, contribute to the ballistic performance of the system. For example, consider the following interfaces/interlayers: (i) the frictional, sliding, inter-ply surfaces within a soft armour pack, and also between the pack and the carrier, (ii) the air-gaps that may develop within the soft armour pack, (iii) the interconnecting space between the soft armour pack and the hard armour plate, (iv) the nature of the interfaces between adjacent plies of a multiplied backing laminate, even in a highly compressed Ultra High Molecular Weight Polyethylene (UHMWPE) variant, (v) the interlayer between the ceramic and its substrate, within a HAP, and (vi) the geometrical fit between two hard armour plates within a stacked body armour system. This paper will provide a User-friendly overview of all such interfaces and provide unique guidance as to their criticality and influence.     

卫星中心承力筒结构优化设计研究

利用有限元软件ANSYS建立复合材料中心承力筒式卫星平台结构的参数化有限元分析模型,计算了整星结构振动模态,在此基础上对复合材料蜂窝夹层中心承力筒结构分析模型进行简化,在满足结构的强度、变形、振动和屈曲约束条件下,对承力筒结构进行优化设计,并对多种方案进行比较,提出的方法和思路为今后同类结构设计提供了参考。     

复合材料层合结构层向理论及应用进展

层向理论是由Reddy提出来的一种用于精确分析复合材料层合结构的三维板壳分析理论。由于不引入任何的变形和应力假设条件,因此相较于传统的等效单层板理论,层向理论在分析大厚度复合材料层合板壳结构的静动态响应及其局部层间效应时具有较大的优势。系统地综述了层向理论近年来的研究进展、数值解法及其应用情况。具体包括:层向理论的基本原理及发展现状、基于层向理论的有限元方法及改进模型、层向理论在复合材料层合结构静动态响应及含损伤问题领域的应用等。并对该理论可进一步拓展的研究方向进行了展望。     

Optimization of buckling load for laminated composite plates using adaptive Kriging-improved PSO: A novel hybrid intelligent method

An effective hybrid optimization method is proposed by integrating an adaptive Kriging (A-Kriging) into an improved partial swarm optimization algorithm (IPSO) to give a so-called A-Kriging-IPSO for maxi-mizing the buckling load of laminated composite plates (LCPs) under uniaxial and biaxial compressions. In this method, a novel iterative adaptive Kriging model, which is structured using two training sample sets as active and adaptive points, is utilized to directly predict the buckling load of the LCPs and to improve the efficiency of the optimization process. The active points are selected from the initial data set while the adaptive points are generated using the radial random-based convex samples. The cell-based smoothed discrete shear gap method (CS-DSG3) is employed to analyze the buckling behavior of the LCPs to provide the response of adaptive and input data sets. The buckling load of the LCPs is maximized by utilizing the IPSO algorithm. To demonstrate the efficiency and accuracy of the proposed methodology, the LCPs with different layers (2, 3, 4, and 10 layers), boundary conditions, aspect ratios and load patterns (biaxial and uniaxial loads) are investigated. The results obtained by proposed method are in good agreement with the literature results, but with less computational burden. By applying adaptive radial Kriging model, the accurate optimal results-based predictions of the buckling load are obtained for the studied LCPs.