环板结构面内自由振动特性分析

采用谱几何法(Spectro-Geometric Method,SGM)对弹性边界条件下环板结构的面内自由振动特性进行计算分析,弹性边界条件采用沿各边界均匀分布的法向和切向线性弹簧来模拟。板结构的位移容许函数被不变地描述为一种谱形式的改进三角级数,正弦三角级数项的引入能够有效地克服弹性边界处潜在的不连续或跳跃现象。将位移容许函数的级数展开系数看作广义坐标,并采用瑞利-里兹法对其进行求解,得到一个关于级数展开系数的标准特征值问题。通过求解标准特征值问题而简便地求解环板结构面内自由振动固有频率及其振型。通过不同数值算例,并与现有文献解及有限元法计算结果进行对比,验证了文中方法的正确性。     

基于谱几何法的耦合板结构固有振动特性分析

以耦合板结构为研究对象,建立结构振动特性分析模型,利用人工虚拟弹簧技术模拟结构边界条件及耦合效应,并通过调整弹簧刚度系数模拟任意边界条件及耦合条件。考虑板结构弯曲、面内振动及耦合边界处的耦合效应,采用谱几何法(Spectro-Geometric Method,SGM)对弯曲振动位移和面内振动位移函数进行描述,可以克服传统傅里叶级数在整个求解区域内周期展开时在边界上存在的不连续或者跳跃现象。应用Hamliton原理从能量的角度推导获得表征耦合板振动特性的离散动力学方程,求解得到耦合板结构的自由振动特性。通过不同数值算例,并与有限元法计算结果进行对比,验证了文中方法的正确性。     

耦合板在任意弹性边界条件下的自由振动分析

采用改进傅立叶级数的方法对任意弹性边界条件下的耦合板进行自由振动分析,将板的振动位移函数表示为标准的二维傅立叶余弦级数和辅助级数的线性组合。通过辅助级数的引入,解决了位移导数在边界不连续的问题。边界条件和耦合条件通过均匀布置的线性位移弹簧和旋转弹簧来模拟,通过改变弹簧刚度值可以实现任意边界条件和耦合条件的模拟。利用Hamilton原理建立求解方程,建立一个线性方程组,最终得到耦合板的控制方程的矩阵表达式,通过特征值分解可以求得固有频率。通过数值仿真分析计算并与有限元结果进行比较,验证了本方法的准确性。     

热环境下弹性边界约束FGM圆环板面内振动特性分析

采用一种改进傅立叶级数方法建立了热环境下弹性边界约束FGM圆环薄板面内振动特性分析模型。基于平面弹性理论应力-应变关系推导了热环境下FGM圆环板面内振动能量原理方程,其中,弹性边界条件通过边界弹簧沿边界分布进行模拟,任意边界条件可以相应设置刚度系数获得。为了改善面内耦合位移场函数在径向边界处连续微分特性,圆环板面内位移径向分量构造为标准傅里叶级数与边界光滑多项式的叠加形式。结合RayleighRitz步骤,热环境下弹性边界约束FGM圆环板结构模态信息可以通过求解一个标准特征值问题而全部得到。随后,通过给出相关数值算例对所建立模型进行了验证,并分析了复杂边界约束情况下圆环板结构面内振动特性的影响。在此基础上,继续探讨并研究了热环境条件、功能梯度材料指数、弹性边界约束刚度等重要参数对FGM圆环薄板面内振动特性的影响规律,为人们全面理解此类复杂结构动力学特性提供了有效的模型基础和分析手段。     

变厚度薄板在任意弹性边界条件下的自由振动分析

采用改进傅立叶级数的方法对任意弹性边界条件下的单向变厚度薄板进行自由振动分析,将板的振动位移函数表示为标准的二维傅立叶余弦级数和辅助级数的线性组合。通过辅助级数的引入,解决了位移导数在边界不连续的问题,改进后的位移函数能够同时满足位移边界条件和力的边界条件。边界条件通过均匀布置的线性位移弹簧和旋转弹簧来模拟,改变弹簧刚度值可以实现不同边界条件的模拟。利用Hamilton原理和Rayleigh-Ritz法建立求解方程,得到变厚度板的控制方程的矩阵表达式,通过特征值分解可以求得固有频率和振型。通过数值仿真分析计算并与有限元及文献的结果进行比较,验证了本方法的准确性。     

任意边界条件下环扇形板面内振动特性分析

基于改进傅里叶级数方法(Improved Fourier Series Method,IFSM)对任意边界条件下环扇形板的面内自由振动特性进行计算分析,任意边界条件可采用沿各边界均匀分布的法向和切向线性弹簧来模拟。环扇形板的径向和切向位移函数被不变地表示为改进傅里叶级数形式,并通过引入正弦函数项来克服弹性边界的不连续或跳跃现象。将位移函数的傅里叶展开系数看作广义坐标,并采用瑞利-里兹方法对其进行求解,得到一个关于未知傅里叶系数的标准特征值问题。通过求解标准特征值问题而简单地求解环扇形板面内振动的固有频率及其振型。通过不同边界条件下环扇形板模型结果与文献解及有限元法结果相对比来验证了本文方法的正确性及可靠性。     

弹性边界约束田字型耦合板的振动特性研究

以平面内田字型耦合薄板结构为研究对象,提出了一种计算弹性约束边界条件耦合板振动响应的解析方法。利用耦合部位的平衡条件和连续性条件,建立了耦合板结构的边界耦合方程。使用改进的傅里叶级数作为每个子板的弯曲位移函数,从而使得微分形式的边界耦合方程和各子板的运动方程离散为简单的线性方程组。ANSYS有限元软件仿真验证了建立的理论模型的正确性。利用该理论模型,分析了边界约束刚度的附带阻尼对耦合板结构振动响应的影响,结果表明:在横向约束刚度较软的情况下,横向约束刚度附带的边界阻尼可以明显削弱低阶共振响应。在求得结构位移的基础上,进一步给出了耦合板结构功率流的表达式,并对耦合板结构内的振动功率流传递特性进行了仿真研究,结果表明:增大边界约束刚度能有效阻碍功率流在边界处的流动;当外激励频率为低阶共振频率时,功率流更容易从受激板流向与受激板相同材质的接受板。     

含焊接残余应力薄圆板结构自由振动近似解

研究焊接残余应力对薄圆板结构振动特性的影响,解决薄圆板结构振动中存在非均匀分布预应力问题。根据含预应力结构的应变-应力方程,建立含预应力薄圆板结构的运动控制方程。基于Rayleigh-Ritz法构造Lagrange能量泛函方程。将预应力和位移试函数展开成三角级数形式,对含预应力薄圆板结构的自由振动问题进行求解。以周边简支边界薄圆板结构为例,对比焊接残余应力的不同分布形式对薄圆板结构固有频率及振型的影响。数值计算结果验证了所提方法的有效性,可应用于解决任意分布预应力问题。     

活塞声源膜板在弹性边界条件下的线谱分析

平行四边形活塞声源模拟舰船声场线谱特征时,为了实现其具有较高的效率,应保证声源膜板结构的固有频率与线谱频率相等,因此,分析膜板结构的振动特性具有重要意义。采用改进Fourier级数的方法建立平行四边形膜板结构的振动模型,通过在膜板结构的四边上布置弹簧来模拟任意弹性边界条件,结构的振动位移函数表示为标准的二维Fourier余弦级数和辅助级数的线性组合。通过辅助级数的引入,解决了位移函数的导数在边界潜在的不连续的问题,从而使此法适用于任意的弹性边界条件。结合Hamilton原理,推导出平行四边形板结构振动方程的矩阵表达示,板结构的振动参数可通过求解矩阵值得到。最后进行了数值仿真,求解出结构在不同参数下的线谱频率,并与文献以及有限元结果进行对比,验证了该方法的精确性。     

任意边界条件下弹性梁耦合振动特性分析EI北大核心CSCD

采用谱几何法建立了任意边界条件下弹性梁横向、纵向和扭转耦合振动分析模型。将弹性梁的横向、纵向和扭转振动位移函数分别描述为一种辅助函数为三角级数的改进傅里叶级数;在弹性梁两端引入边界约束弹簧组,通过改变其刚度值模拟任意边界条件;应用Hamilton原理从能量角度推导整个结构的拉格朗日函数;采用Ritz法对其进行求解。计算了弹性梁模型不同边界下前6阶固有频率,与文献解对比最大误差为0.02%,验证了该方法的正确性和较快的收敛性。该模型统一了弹性梁横向、纵向和扭转振动的位移函数表示形式和模态特性求解方程,通过改变边界约束弹簧刚度系数可以实现对弹性梁耦合振动特性进行调整,为弹性梁动力学性能优化提供了一种参数化的研究方法。     

Vibration analyses of FGM plates with in-plane material inhomogeneity by Ritz method

In this study, functionally graded plates which the properties of material varying through the in-plane direction is considered. The analysis is based on a five-degree-of-freedom shear deformable plate theory with different boundary conditions. The vibration solutions are obtained using the Ritz method and assumed displacement functions are in the form of the Chebyshev polynomials. The material properties are assumed to vary as a power form of the in-plane direction. The convergence and comparison studies demonstrate the accuracy and correctness of the present method. Effects of the different material composition, the Poisson ratio and the plate geometry (side-side, side-thickness) on the free vibration frequencies and mode shapes are investigated.     

On new symplectic elasticity approach for exact free vibration solutions of rectangular Kirchhoff plates

In the classical approach, it has been common to treat free vibration of rectangular Kirchhoff or thin plates in the Euclidian space using the Lagrange system such as the Timoshenko’s method or Lévy’s method and such methods are the semi-inverse methods. Because of various shortcomings of the classical approach leading to unavailability of analytical solutions in certain basic plate vibration problems, it is now proposed here a new symplectic elasticity approach based on the conservative energy principle and constructed within a new symplectic space. Employing the Hamiltonian variational principle with Legendre’s transformation, exact analytical solutions within the framework of the classical Kirchhoff plate theory are established here by eigenvalue analysis and expansion of eigenfunctions in both perpendicular in-plane directions. Unlike the classical semi-inverse methods where a trial shape function required to satisfy the geometric boundary conditions is pre-determined at the outset, this symplectic approach proceeds without any shape functions and it is rigorously rational to facilitate analytical solutions which are not completely covered by the semi-inverse counterparts. Exact frequency equations for Lévy-type thin plates are presented as a special case. Numerical results are calculated and excellent agreement with the classical solutions is presented. As derivation of the formulation is independent on the assumption of displacement field, the present method is applicable not only for other types of boundary conditions, but also for thick plates based on various higher-order plate theories, as well as buckling, wave propagation, and forced vibration, etc.     

On the exact in-plane and out-of-plane free vibration analysis of thick functionally graded rectangular plates: Explicit 3-D elasticity solutions

In this paper exact closed-form solutions of 3-D elasticity theory are presented to study both in-plane and out-of-plane free vibrations for thick functionally graded simply supported rectangular plates. The solution procedure of the transverse vibration utilizes Levinson’s representation form to describe the displacement; in this way, the 3-D elasto-dynamic equations are written in terms of some suitable independent functions satisfying ordinary differential equations. A similar procedure is presented for in-plane vibration by introducing an appropriate displacement field. In each case, the obtained ordinary differential equations are analytically solved and boundary conditions are satisfied. The proposed solutions are validated by comparing some of the present results with corresponding results known in the literature as well as with 3-D Finite Element Method. Finally, the influence of inhomogeneity on the natural frequencies for a thick functionally graded rectangular plate is discussed.     

Finite element method for non-linear forced vibrations of circular plates

Geometric non-linearities for large amplitude free and forced vibrations of circular plates are investigated. In-plane displacement and in-plane inertia are included in the formulation. The finite element method is used. An harmonic force matrix for non-linear forced vibration analysis is introduced and derived. Various out-of-plane and in-plane boundary conditions are considered. The relations of amplitude and frequency ratio for different boundary conditions and various load conditions are presented.     

Nonlocal buckling and vibration analysis of thick rectangular nanoplates using finite strip method based on refined plate theory

The buckling and vibration of thick rectangular nanoplates is analyzed in this article. A graphene sheet is theoretically assumed and modeled as a nanoplate in this study. The two-variable refined plate theory (RPT) is applied to obtain the differential equations of the nanoplate. The theory accounts for parabolic variation of transverse shear stress through the thickness of the plate without using a shear correction factor. Besides, the analysis is based on the nonlocal theory of elasticity to take the small-scale effects into account. For the first time, the finite strip method (FSM) based on RPT is employed to study the vibration and buckling behavior of nanoplates and graphene sheets. Hamilton’s principle is employed to obtain the differential equations of the nanoplate. The stiffness, stability and mass matrices of the nanoplate are formed using the FSM. The displacement functions of the strips are evaluated using continuous harmonic function series which satisfy the boundary conditions in one direction and a piecewise interpolation polynomial in the other direction. A matrix eigenvalue problem is solved to find the free vibration frequency and buckling load of the nanoplates subjected to different types of in-plane loadings including the uniform and nonuniform uni-axial and biaxial compression. Comparison studies are presented to verify the validity and accuracy of the proposed nonlocal refined finite strip method. Furthermore, a number of examples are presented to investigate the effects of various parameters (e.g., boundary conditions, nonlocal parameter, aspect ratio, type of loading) on the results.     

Influence of in-plane pre-load on the vibration frequency of circular graphene sheet via nonlocal continuum theory

In this study, the free vibration behavior of circular graphene sheet under in-plane pre-load is studied. By using the nonlocal elasticity theory and Kirchhoff plate theory, the governing equation is derived for single-layered graphene sheets (SLGSs). The closed-form solution for frequency vibration of circular graphene sheets under in-plane pre-load has been obtained and nonlocal parameter appears into arguments of Bessel functions. The results are subsequently compared with valid result reported in the literature. The effects of the small scale, pre-load, mode number and boundary conditions on natural frequencies are investigated. The results are shown that at smaller radius of circular nanoplate, the effect of in-plane pre-loads is more importance.     

复杂隔振结构激励下弹性基础振动及声辐射分析

针对隔振结构-弹性基础耦合结构向外声辐射问题,本文采用刚体理论及改进的傅里叶级数方法建立以任意边界弹性板为基础的双层隔振耦合结构数学模型。采用瑞利-里兹方法得到整个耦合结构的强迫振动响应,继而通过提取表面振速分布计算基础弹性板向外的辐射声功率。结合隔振结构的布置情况,以隔振器安装点的振动作为表征,探讨了耦合结构振动模态与基础板声辐射模态之间的耦合对应关系。最后计算并分析了基础边界条件对基础板向外辐射声功率的影响。     

Vibration of non-ideal simply supported laminated plate on an elastic foundation subjected to in-plane stresses

In this paper, the effect of non-ideal boundary conditions and initial stresses on the vibration of laminated plates on Pasternak foundation is studied. The plate has simply supported boundary conditions and is assumed that one of the edges of the plate allows a small non-zero deflection and moment. The initial stresses are due to in-plane loads. The vibration problem is solved analytically using the Lindstedt–Poincare perturbation technique. So the frequencies and mode shapes of the plate with non-ideal boundary condition is extracted by considering the Pasternak foundation and in-plane stresses. The results of finite element simulation, using ANSYS software, are presented and compared with the analytical solution. The effect of various parameters like stiffness of foundation, boundary conditions and in-plane stresses on the vibration of the plate is discussed. Dependency of non-ideal boundary conditions on the aspect ratio of the plate for changing the frequencies of vibrations is presented. The relation between the shear modulus of elastic foundation and the frequencies of the plate is investigated.     

Effects of in-plane constraints on the free vibration of a symmetrically laminated doubly curved panel

Summary. For a symmetrically laminated curved panel, although the stretching-bending anisotropic coupling stiffnesses are zero, but due to presence of the curvature, the in-plane and out-of-plane behaviors of the panel are still coupled, and hence the in-plane constraints at the boundaries have influences on the transverse behavior of the panel. Such effects of in-plane constraints on the free vibration of the symmetrically laminated curved panel are investigated using a modified Galerkin method in this study. Transverse shear deformation of the panel is considered by using first-order shear deformation theory. Numerical results of the symmetric angle-ply and cross-ply laminated panel with simply supported boundary conditions (SS2 and SS3) are presented. Results show that the in-plane boundary constraints have significant effects on the vibration behavior of the symmetrically laminated curved panel, and the effects strongly depend on the radius of curvature, thickness and lamination schemes, etc. Effects of bending-twisting anisotropic coupling of symmetric angle-ply laminate on the vibration behavior are also discussed.     

点支撑预应力中厚矩形板的横向振动

基于Reissner-Mindlin一阶剪切变形板理论,讨论在预加面内机械荷载或温度场作用下,点支撑中厚矩形板的横向振动。温度场假定沿板表面为均布,沿板厚方向为线性分布的。利用考虑剪切变形影响的Timoshenko梁函数,采用Rayleigh-Ritz法给出不同边界条件下点支撑中厚板的自振频率。结果表明,温度升高与预加面内压力将使板的自振频率下降,支撑点位置的变化、边界约束条件和横向剪切变形效应都对板的自振频率有显著影响。