功能梯度材料圆（环）板的屈曲分析

基于经典板理论，推导了功能梯度材料圆形板在边界面内均布压力作用下的轴对称屈曲方程．假设功能梯度材料性质沿板厚度方向按成分含量百分比的幂指数形式连续变化，用打靶法求解所得方程，得到了功能梯度材料圆(环)板的临界屈曲载荷，并分析了材料的梯度性质、内外半径比以及边界条件对板临界载荷的影响．     

带压电层功能梯度悬臂板非线性动力学分析

分析了在热环境条件下受横向栽荷作用的、带压电功能梯度材料悬臂板的非线性动力学问题。基于vonKarman理论和Reddy一阶剪切变形理论,推导出了带压电功能梯度悬臂板的动力学方程。利用Galerkin法对偏微分方程进行离散,对离散后的方程进行数值模拟,分析中考虑了组分材料热物参数对温度变化的依赖性,讨论了材料组分指数、控制电压对系统非线性动力学行为的影响,结果表明正电压减小了板的振幅,负电压增大了板的振幅,而随着材料体积分数指数的增大,板的振幅也在变大。     

粘弹性板热机耦合非线性振动（Ⅰ）——动力学模型

建立了横向周期荷载、面内均布荷载和温度场作用下,考虑热传导效应的粘弹性矩形板的热机耦合非线性动力学模型.基于薄板大挠度Karman理论和用Boltzmann叠加原理描述的粘弹性材料本构方程、动力学平衡方程和热粘弹能量原理建立了考虑热传导效应的粘弹性矩形板的热机耦合非线性动力学模型,并用Galerkin方法将该热机耦合非线性动力学模型转化为非线性微分-积分动力系统.研究表明:1)在热传导系数和热膨胀都为0时,该热机耦合非线性动力学模型退化为粘弹性板动力学模型;2)在热传导系数为0而热膨胀不为0时,该热机耦合动力学模型简化为仅考虑热膨胀时的粘弹性板动力学模型;3) 当材料的粘性项为0时,即动力学模型中积分项为0时,该热机耦合动力学模型退化为热机耦合弹性板动力学模型.     

DQM求解功能梯度圆板轴对称线性弯曲问题研究

基于一阶剪切变形板理论,研究了功能梯度圆板在均布机械载荷作用下的轴对称线性弯曲问题.假设功能梯度材料性质只沿板厚方向变化,且服从幂函数规律,推导了该问题的控制方程,考虑固支边界条件,用微分求积法对其进行数值求解.利用求解结果讨论了功能梯度材料的梯度参数、板厚半径比对圆板线性弯曲的影响.     

扁球面网壳的非线性动力学特征

由壳体结构的几何方程、物理方程和平衡方程,根据薄壳的非线性动力学理论,用拟壳法推导出扁球面网壳的非线性动力学变分方程和变形协调方程,在周边固定夹紧和底面内可移夹紧的边界条件下,用Galerkin方法得到一个含二次、三次项的非线性微分方程。     

DQ法求解功能梯度矩形板的弯曲问题

基于经典理论和一阶剪切变形理论,研究了功能梯度材料矩形板的线性弯曲问题.在假设功能梯度材料性质只沿板厚度方向变化,且其变化规律满足体积分数的幂指数函数的基础上,推导了线性弯曲问题的控制方程,并运用二维问题的微分求积法对其进行数值求解,利用数值结果考察了简支边界条件下梯度参数、长宽比等因素对板的无量纲挠度的影响,并验证了...     

热载荷作用下含裂纹功能梯度板的有限元分析

为深入理解功能梯度材料的热断裂行为,研究了热载荷作用下任意热机械属性功能梯度材料板的裂纹尖端特性.利用解析方法推导了不含裂纹功能梯度板的温度场和热应力场,根据叠加法,把热应力场转化为裂纹表面载荷,采用基于非均匀单元的有限元方法计算分析了稳态热载荷下功能梯度板的裂纹尖端特性,并针对不同材料热机械属性分布形式,考察了热应力...     

有初始缺陷的FGM圆柱壳的非线性动力学分析

研究了有初始几何缺陷的FGM圆柱壳在面内载荷与横向载荷共同作用下的非线性动力学行为。材料组分的体积分数沿厚度方向呈幂律分布。基于Reddy的三阶剪切变形理论,运用Hamilton原理,推导出了FGM圆柱壳振动的非线性偏微分方程;利用Galerkin法离散控制方程,将偏微分方程离转化为常微分方程。为了准确地描述圆柱壳的非线性动力学行为,考虑到了对称模态。通过Runge-Kutta法进行数值仿真,研究了系统的非线性动态响应,并得到了分岔图、最大Lyapunov指数、相图和时间历程图。通过对比有2种不同类型缺陷的数值结果分析了缺陷类型和面内载荷对系统非线性动态响应的影响。     

含压电结构的FGM悬臂板非线性动力学分析

针对含压电层功能梯度材料（FGM）悬臂板的非线性动力学问题,提出了基于von-Karman理论和Reddy三阶剪切变形理论的FGM板动力学方程,建立了以表面覆盖（P/FGM/P）和埋置压电层（FGM/P/FGM）的FGM板模型,利用Galerkin法对偏微分方程组进行离散,通过Runge-kutta算法求解方程组并对系统进行数值分析,得出控制电压和压电层铺设方式对系统非线性动力学行为有很大的影响,板的横向振幅随着正电压的升高而减小,随着负电压的增大则增大,另外控制电压对P/FGM/P混合板振动的影响更为显著。     

各向异性功能梯度材料弯曲断裂模型探讨

探讨各向异性功能梯度材料裂纹板受纯弯、纯扭、弯扭载荷作用下的弯曲断裂问题．根据弹性力学的基本方程以及断裂力学的有关理论及微积分方法,将材料常数（刚度系数）设为空间变量的任意函数,建立了各向异性功能梯度材料板弯曲断裂模型,即三类偏微分方程边值问题．再将材料常数依次设为空间变量的指数函数和幂函数,建立了相应的弯曲断裂模型,即一系列相关的偏微分方程的边值问题．这些模型是研究有关各向异性功能梯度材料板弯曲断裂问题的一个出发点和理论基础．     

Nonlinear transient responses of rotating twisted FGM cylindrical panels

This paper develops a new structure dynamic model to investigate nonlinear transient responses of the rotating blade made of functionally graded material(FGM). The rotating blade is simplified as a rotating FGM cylindrical panel with a presetting angle and a twist angle. The geometric nonlinearity effects are taken into account in the strain-displacement relationships, which are derived by Green strain tensor. Based on the first-order piston theory and the first-order shear deformation theory, the equations of motion for the rotating twisted FGM cylindrical panel are acquired by means of Hamilton principle and Galerkin method.Backward Differentiation Formula(BDF) and Runge-Kutta Algorithm are used to solve the nonlinear equations of motion for the system. The effects of four pulse load conditions on the system subjected to the internal pulse load or the external pulse load are fully discussed. A detailed parametric analysis is performed by considering the effects of the rotating speed, volume fraction index and temperature.     

负载与支承刚度对面齿轮传动系统动态特性的影响分析

为研究负载及支承刚度变化时对面齿轮传动系统动态特性的影响,建立了包含支承、齿侧间隙、时变啮合刚度、综合传动误差、阻尼和负载激励等参数的系统弯-扭耦合动力学模型,并使用PNF（Poincaré-Newton-Floquet）方法进行求解。计算结果表明,在不同的负载及支承刚度条件下,系统会出现简谐响应、次谐响应、拟周期响应及混沌响应4类稳态响应。增加负载及支承刚度能有效降低系统的动载荷,而增大支承刚度还可以减小面齿轮支承在方向与方向上的振动位移幅值差距。     

Method of lines for temperature field of functionally graded materials

The finite element method (FEM) and the boundary element method (BEM) are often adopted. Howev er, they are not convenient to spatially vary thermal properties of functionally graded material (FGM). Therefore, the method of lines (MOL) is introduced to solve the temperature field of FGM. The basic idea of the method is to semi-discretize the governing equation into a system of ordinary differential equations (ODEs) defined on discrete lines by means of the finite difference method. The temperature field of FGM can be obtained by solving the ODEs. The functions of thermal properties are directly embodied in these equations and these properties are not discretized in the domain. Thus, difficulty of FEM and BEM is overcome by the method. As a numerical example, the temperature field of a plane problem is analyzed for FGMs through varying thermal conductivity coefficient by the MOL.     

Periodic and chaotic dynamics of composite laminated piezoelectric rectangular plate with one-to-two internal resonance

The bifurcations and chaotic dynamics of a simply supported symmetric cross-ply composite lami- nated piezoelectric rectangular plate are studied for the first time, which are simultaneously forced by the transverse, in-plane excitations and the excitation loaded by piezoelectric layers. Based on the Reddy’s third-order shear deformation plate theory, the nonlinear governing equations of motion for the composite laminated piezoelectric rectangular plate are derived by using the Hamilton’s principle. The Gal...     

Method of lines for temperature field of functionally graded materials

The finite element method (FEM) and the boundary element method (BEM) are often adopted. However, they are not convenient to spatially vary thermal properties of functionally graded material (FGM). Therefore, the method of lines (MOL) is introduced to solve the temperature field of FGM. The basic idea of the method is to semi-discretize the governing equation into a system of ordinary differential equations (ODEs) defined on discrete lines by means of the finite difference method. The temperature field of FGM can be obtained by solving the ODEs. The functions of thermal properties are directly embodied in these equations and these properties are not discretized in the domain. Thus, difficulty of FEM and BEM is overcome by the method. As a numerical example, the temperature field of a plane problem is analyzed for FGMs through varying thermal conductivity coefficient by the MOL. Foundation item: Project (90305023 and 59731020) supported by the National Natural Science Foundation of China     

Vibration of functionally graded sandwich doubly curved shells using improved shear deformation theory

Nonlinear forced vibrations and natural frequency of sandwich functionally graded material doubly curved shallow shell with a rectangular base are investigated. The sandwich functionally graded material (FGM) doubly curved shell is subjected to a harmonic point load at centre. The sandwich doubly curved shell with homogeneous face sheets and FGM face sheets is considered respectively when the natural frequencies are studied. Reddy’s third order shear deformation theory is expanded in which stretching effects in thickness are considered by introducing the secant function. Hamilton’s principle and von-Karman type nonlinear geometric equation are applied to obtain partial differential equation of the FGM sandwich doubly curved shell. Comparative studies with other shear deformation theories are carried out to validate the present formulation. Navier method is used to discuss the natural vibration frequencies of the FGM sandwich doubly curved shell. Numerical simulation is applied to demonstrate the nonlinear dynamic responses of the FGM sandwich doubly curved shell. Multiple periods, quasi-period and chaos are detected for the dynamic system for different core thickness.     

预应力钢箱梁的非线性分析

为提高预应力钢筋梁的计算精度，对预应力钢箱梁的两个受力阶段作了全过程非线性分析，建立了预应力钢箱梁的非线性分析模型，采用平衡原理和能量原理分别推导出预应力钢箱梁在预加力阶段和荷载阶段的控制微分方程，用上述方程进行理论计算所获得的数据，如钢梁的跨国挠度、底板应变均与预应力钢箱梁模型的实验结果符合良好，表明了建立的模型和所推导的控制微分方程的有效性和正确性，对影响钢箱梁刚度的因素诸如预加力的大小，预应力钢索的跨中垂度等进行了详细讨论，讨论结果表明，当外荷载较小时，预加力对钢箱梁刚度影响较小，当外荷载较大时，预加力对钢箱梁刚度影响较大，钢索在跨中的垂度越大对钢箱梁刚度的提高越大。     

伞形膜结构在冰雹荷载作用下的非线性动力响应

对伞形张拉膜结构在自然灾害等外荷载冲击下的振动反应进行研究,为实际工程膜结构建筑受灾破坏分析提供依据。基于冯·卡门大挠度理论和薄板振动理论,建立伞形张拉膜结构在冰雹荷载作用下的非线性动力响应控制方程。采用贝塞尔函数及欧拉方程求得其振型函数,再运用KBM摄动法和迦辽金法对控制方程求解,得到其动力响应的近似解析解。利用Mathmatics软件对方程进行求解并对求解后的数据进行整理,通过Origin绘图软件画出膜面受迫振动后的时程位移图。采用ANSYS软件建立伞形张拉膜结构的有限元模型;再通过LS-DYNA显示动力学模块对冰雹冲击膜面的动力过程进行模拟,得到膜面动力响应的结果。同理,画出数值模拟结果的位移图,将整理后的理论与数值分析数据结果进行对比分析,结果表明,理论解析和数值分析结果吻合。