截锥壳颤振分析的微分求积法

引入微分求积法(Differential Quadrature Method,简称DQM)对截锥壳气动弹性方程离散,采用一阶活塞理论气动力,运用特征值分析方法求解系统的颤振临界动压。研究了半顶角、径厚比、长径比等几何参数对颤振临界动压的影响。结果表明,DQM求解截锥壳气动弹性方程具有良好的精度和计算效率,结构产生1阶~2阶耦合型颤振的最低临界动压对应的周向波数较大,并因几何参数而异;颤振临界动压参数随半顶角的增大而减小,随着径厚比的增大而增大,随长径比的增大而减小。     

载荷脉宽对圆柱壳瞬态响应的影响分析

为认识载荷脉宽对圆柱壳瞬态响应及其对X射线冲击响应模拟等效性的影响规律,定义了等效性评价指标即平均应变差异。以四种不同尺寸的典型圆柱壳为对象,分别加载六种冲量相同、脉宽不同的三角形脉冲载荷,通过数值模拟,获得了平均应变差异Δε随脉宽变化的关系,从结构特性角度分析了变化的原因。发现Δε主要受t/τ(脉宽占比)控制,t/τ≤0.45时,平均应变差异在20%以内。所得结果可为模拟X射线冲击环境的试验设计、结果评估和数值模拟提供参考。     

微分求积法处理轴向变速黏弹性梁混杂边界条件

给出了一种利用微分求积法处理非线性轴向变速黏弹性梁的混杂边界条件的方法。利用微分求积法数值求解具有混杂边界轴向变速黏弹性梁的控制微分方程,将混杂边界条件直接引入到控制微分方程高阶导数的微分求积解权系数矩阵中。使用这种方法研究了非线性轴向变速黏弹性梁主参数共振的稳态幅频响应,并对算例的微分求积解和解析近似解做了比较。     

微分求积时间单元方法

基于微分求积法则,提出了一种求解动力学常微分方程的高效高精度微分求积时间单元方法(DQTEM).给出了DQTEM施加初始位移和初始速度的方法,其结果相当于构造了C1时间单元.与递推格式的直接积分方法不同,对于考虑的时间域通常只需用一个微分求积时间单元.与RK法和Newmark法相比,用少量时间结点的DQTEM结果就与精确解吻合.稳定性分析表明,DQTEM通常是条件稳定的.     

用微分求积法求解梁的弹塑性问题

根据梁塑性弯曲的工程理论,采用微分求积法进行了梁的弹塑性平面弯曲分析。微分求积法是一种直接求解微分方程(组)的数值方法,不依赖于变分原理,且能以较少的网格点求得微分方程的高精度数值解。与有限元分析结果的比较,表明了微分求积法求解梁的弹塑性问题的计算效率和精度。微分求积法的计算结果不受荷载步长的限制,也不需要迭代求解,特别对于承受非线性分布荷载作用的梁的弹塑性分析具有很大的优越性。通过选用不同的网格点数目,分析了微分求积法的稳定性和收敛性。     

非轴对称移动载荷下有限长圆柱厚壳的动力响应

本文在介绍圆柱厚壳应力与位移理论分析发展的前提下,建立了有限长圆柱厚壳在非轴对称移动载荷作用下的三维力学模型,假设沿厚度方向径向剪切应变二次分布、径向正应变线性分布,且建立了为满足边界条件待定的位移表达式,采用Heaviside函数和Dirac函数表达移动和作用变化着的移动载荷的基础上,用最小势能原理建立了该圆柱厚壳的动力学微分方程组,应用Galerkin法和修正的Runge–Kutta–Fehlberg法,求得了非轴对称移动载荷作用下的圆柱厚壳的动力响应。通过具体算例,对有限长圆柱厚壳的位移响应和应力状态进行了分析,并将动态响应的理论解与ANSYS数值解进行了对比,从而相互印证了解的可靠性。     

结构动力响应微分求积分析方法的基本特性

以结构动力响应微分求积(DQ)分析方法的基本数值格式为基础,探讨了时步内时间点分别为均匀分布、Chebyshev分布和Chebyshev-Gauss-Lobatto(CGL)分布时该方法的数值稳定性与数值耗散性,并通过等效一阶模型严格推导出方法的代数精度阶数。研究表明,该方法的数值稳定性与时步内时间点分布情况密切相关,不均匀分布格式明显优于均匀分布格式,但体系阻尼比对方法的稳定性具有重大影响;代数精度由离散时间点数决定,一般情况下都能实现比较高的数值精度;两种不均匀时间点分布格式,即Chebyshev格式和CGL格式的DQ分析方法,均具有极佳的数值耗散特性。     

基于弹性圆柱壳的柔性齿轮副建模及动力学分析

基于弹性圆柱壳理论,建立柔性齿轮副等效简化模型.首先采用具有时变刚度的弹簧模拟齿轮交替啮合过程,其中时变啮合刚度通过解析模型得到;同时采用径向和切向支撑弹簧模拟轴和轴承的柔性.接着根据能量原理,推导柔性齿轮副系统的动能、应变能、啮合弹簧势能以及支撑弹簧势能.随后基于微分求积有限法(DQFEM)对能量表达式进行离散,分别...     

摄动微分求积法解复合材料层合板非线性振动

以摄动法将层合板的非线性振动偏微分方程线性化,从摄动方程中分离出时域函数并求解。将场函数设定为含时域函数的待定函数,通过微分求积法对空间域的摄动方程进行离散,将其转化成一系列的线性方程并通过编程求解。算例结果分析说明算法精度良好且效率高。     

几何参数对旋转薄壁圆柱壳振动特性的影响

摘 要: 本文基于Love壳体理论对旋转薄壁圆柱壳的自由振动特性进行分析,讨论几何参数对圆柱壳振动特性的影响。针对五种边界条件,分别分析厚度与半径之比、半径与长度之比对旋转薄壁圆柱壳固有频率特性的影响;探讨半径与长度之比对系统振型比的影响。分析结果表明：圆柱壳固有频率随着厚度与半径之比的增加而单调增加,增加幅度较小。半径与长度之比对圆柱壳固有频率与振型比的影响显著,且随其增大固有频率及振型比均不单调变化。由此可知,细长圆柱壳的振动特性与短粗圆柱壳的振动特性差异显著,研究结果为圆柱壳的动力学分析提供理论依据。     

The elastic response of functionally graded cylindrical shells to low-velocity impact

This paper deals with the problem of functionally graded (FG) cylindrical shells subjected to low-velocity impact by a solid striker. An analytic solution to predict the impact response of the FG cylindrical shells with one layer or multi-layers is presented. The solution includes both contact deformation and transverse shear deformation. The effective material properties of functionally graded materials (FGMs) for the cylindrical shells are assumed to vary continuously through the shell thickness and are graded in the shell thickness direction according to a volume fraction power law distribution. This is implemented in the governing equation of motion and thus included in the present solution. Four types of FG cylindrical shells composed of stainless steel and silicon nitride are configured and their transient responses to impact are computed using the present solution. The effects of the constituent volume fraction and the FGM configuration on the transient response of the laminated cylindrical shell induced by impact are examined.     

粘弹性复合材料层合板壳的动力稳定性分析

分析面内周期激励下粘弹性层合平板以及轴向周期荷载作用下粘弹性层合圆柱壳的动力稳定性。设粘弹性复合材料服从Boltzmann积分型本构关系，其松弛模量由Prony—Dirichlet级数表示，基于薄板与薄壳理论，分别得到对称正交铺设层合板与层合圆柱壳的微分-积分型动力学方程，并应用谐波平衡法直接求解，忽略积分运算所产生的衰减项，导出确定动力不稳定区域边界的特征方程。分析结果表明，主要动力不稳定区域的缩小与材料的粘性参数以及结构横向振动的基频密切相关。     

Axisymmetric response of nonlinearly elastic cylindrical shells to dynamic axial loads

The axisymmetric response of nonlinearly elastic cylindrical shells subjected to dynamic axial loads is analysed by using an incremental formulation. The material elastic nonlinearity is modeled by the generalized Ramberg—Osgood representation. The time-dependent displacements of the shell are assumed to be governed by nonlinear equations of motion based on the von Karman—Donnell kinematic relations; moreover, both in-surface and out-of-surface inertia terms are included. The finite difference method with respect to the spatial coordinate and the Runge—Kutta method with respect to time are employed to derive a solution. Numerical results demonstrate the effect of the material nonlinearity on the deflections, stiffness matrices and dynamic buckling behavior of cylindrical shells.     

On the transient response of cross-ply laminated circular cylindrical shells

Transient response of simply-supported circular cylindrical shells is investigated using a higher-order shear deformation theory (HSDT). The theory is a modification of the Sanders' shell theory and accounts for parabolic distribution of the transverse shear strains through thickness of the shell and tangential stress-free boundary conditions on the bounding surfaces of the shell. The results obtained using the classical shell theory (CST) and the first-order shear deformation theory (FSDT) are compared with those obtained using the higher-order theory. The state-space approach is used to develop the analytical solutions to the equations of motion of the three theories.     

The behavior of angle-ply laminated cylindrical shells with viscoelastic interfaces in cylindrical bending

The behavior of a simply supported angle-ply laminated cylindrical shell in cylindrical bending with viscoelastic interfaces is studied. The Kelvin–Voigt model is adopted to represent the character of interfaces. State-space formulations are developed based on the exact elasticity equations, and in particular, a variable substitution technique is used to derive the state equations with constant coefficients. Since the behavior of this structure under static loading is time-dependent, the power series expansion technique is used to approximate the variations of physical variables with time. The response for a laminated shell with viscous interfaces is also investigated as a particular case. Results show that the displacements as well as the maximum stresses in the panel increase rapidly with time. Thus, the imperfect bonding properties should be considered carefully in the design of laminated structures.     

Flutter of delaminated cross-ply laminated cylindrical shells

In this study, the instability of delaminated cross-ply thin laminated cylindrical shells and panels when subjected to supersonic flow parallel to its length edge is investigated. The delamination is parallel to the shell reference and it extends along the entire length of the cylindrical shell. The Love’s shell theory and Von-Karman–Donnell type of kinematic relations along with first-order potential theory have been employed to construct the aeroelastic equations of motion. The effects of several parameters such as length to radius ratio, delamination position, size and thickness on the critical values are discussed in the details. The results indicate that the presence of delamination reduced the overall stiffness of the structure and thereby decreases the flutter critical boundaries.     

Forced harmonic response of viscoelastic sandwich beams by a reduction method

The aim of this article is to develop a reduction method to determine the forced harmonic response of viscoelastic sandwich structures at a reasonable computational cost. The numerical resolution is based on the asymptotic numerical method. This type of problem is complex, and its number of degrees of freedom is double the number of the undamped structure, leading to a high computational time. To address the problem, three reduction methods are evaluated, which differ from the projection operator. Numerical tests have been performed in the case of cantilever sandwich beams. The comparison of the results obtained by the reduction order resolution with those given by the full order resolution shows both a good agreement and a significant reduction in computational cost.     

基于减基法的结构谐响应快速分析方法

针对大型线弹性结构谐响应分析的计算效率与计算存储的问题,提出了一种基于减基法的快速算法.这种算法把简谐外载荷的频率作为参数,并且对频域进行预采样.把预采样空间对应的解集做成一个训练空间,采用贪婪算法进行减基空间基向量的自适应选取,进而由Galerkin映射得到减缩系统.最后,通过求解减缩系统频域方程来达到结构谐响应快速分析的目的.根据谐响应分析的特点,整个计算过程可以分成离线和在线两个阶段,从而进一步提高减基近似的效率.采用了一个简化机翼模型的谐响应分析来验证该方法的高效性和精确性.     

Dynamic response of functionally graded circular cylindrical shells subjected to radial impulse load

Dynamic response of simply supported circular cylindrical shell made of functionally graded material (FGM) subjected to lateral impulse load is investigated. The effective material properties are assumed to vary continuously along the thickness direction according to a volume fraction power law distribution. First order shear deformation theory and Love’s first approximation theory are utilized in the equilibrium equations. Finally time response of displacement components is derived using mode superposition method. The influence of material composition, FGM configuration and geometrical parameters (length-to-radius and thickness-to-radius ratios) on the dynamic response is investigated. The results show that even though the shell is thin, the value of power law exponent has a considerable effect on the natural frequencies as well as the dynamic response of the functionally graded shell. Verification of the results of natural frequencies and time response of the FGM shell is achieved by making comparison with those available in the literature and those obtained using commercial software.