黏弹性层合悬臂薄壁圆柱壳的模态特性研究

基于薄壳理论和黏弹性理论, 得出了黏弹性层合悬臂薄壁圆柱壳模态特性的半解析解. 根据乐甫薄壳理论, 建立了基层和黏弹性阻尼层薄壁圆柱壳的一阶状态微分方程, 结合黏弹性阻尼层的变形协调关系和层间作用力关系, 利用传递矩阵法得出了整体结构的传递矩阵, 采用高精度的精细积分法得出了固有频率、模态损耗因子和三维模态振型, 最后通过有限元法进行了比较, 通过算例验证了传递矩阵法对黏弹性层合薄壁圆柱壳模态特性研究的有效性.     

考虑弹性地基切向抗力的变截面圆弧壳梁分析

本文根据弹性薄壳理论,考虑了弹性地基径向和切向抗力的影响,解决了变截面圆弧壳地基梁的难题,作者所提出的近似解析法和加权余量法、传递矩阵法较有限单元法简便.     

一类新型受任意载荷的杂交旋转壳单元

本文从弹性力学Reissner变分原理出发推导旋转壳曲线坐标系下内分，位移的二类变量广义变分原理，依据这个原理推导一类旋转壳坐标系中具有独立横向转角的受谐和外载荷下的杂交旋转壳单元，内力模式的选用使刚度矩阵的剪切部份在薄壳情况下能反映Kirchhoff假设，并使单元刚度矩阵满秩，从而保证单元无剪切自锁和零能模式，数例证明这类单元对中厚和薄旋转壳具有良好的通用性和较高的精度。     

用张量分析进行薄壳混杂模型三角形单元的构式

一般常用薄板单元分析薄壳内力,但由于内部边界联接斜率的不连续性而影响到求解精度。本文首先从薄壳的基本理论着手,用张量分析法建立了薄壳的势能原理和混杂变分原理。其次,对任意形状的薄壳,提出了采用混杂模型进行三角形单元的构式方法。最后,以螺旋曲面薄壳为例,导出了性质矩阵的形式。     

旋转圆环动态特性的行波解

基于固体弹性介质中的行波理论,对旋转圆环的固有频率进行了计算.以扩张弯曲梁微元体的运动方程为基础,分析了运动条件下该波导中行波的色散关系.通过分离正行波数和负行波数,解决了行波法计算旋转圆环的固有频率问题.同时给出了波数分离的判断依据,并结合简谐波动的相位封闭原理和传递矩阵建立了旋转圆环的特征方程.数值模拟研究了旋转体...     

轴对称薄壳弹塑性大变形有限元分析

本文讨论任意形状旋转薄壳的轴对称变形问题,用增量有限元位移法对其弹塑性大变形行为进行了分析。同时考虑材料和几何两方面的非线性。提出在每级载荷下用解析法确定弹塑性交界面的弹塑性刚度计算方案,这对提高计算精度和效率都是有益的。六个算例和解析解吻合很好。     

前屈曲应力状态对组合加肋旋转壳失稳临界压力影响的探讨

推导了包含前屈曲弯矩和横剪力的旋转壳弹性稳定性基本方程.运用Riccati传递矩阵法对组合加肋旋转壳算例进行了稳定性分析,并与假设前屈曲状态为薄膜应力状态计算出的失稳临界压力进行了比较.结果表明,前屈曲弯矩和横剪力对组合加肋旋转壳失稳临界压力的影响较小,随着壳板厚度和肋骨尺寸的增大及肋骨间距的缩短,影响略有增大.因而,分析组合加肋旋转壳弹性稳定性时,前屈曲状态采用薄膜应力状态的假设是合理的.     

多体系统传递矩阵法研究进展

作为一种多体系统动力学新方法, 多体系统传递矩阵法由于其无需系统总体动力学方程和快速计算的特点, 已被广泛用于各种多管火箭、自行火炮、舰炮等复杂大型机械系统动力学分析与设计. 本文介绍了该方法的研究进展, 包括: 线性多体系统传递矩阵法、多体系统离散时间传递矩阵法、二维系统传递矩阵法、受控多体系统传递矩阵法、多体系统传递矩阵法和通常动力学方法的混合方法等, 给出了该方法解决自行火炮、多管火箭武器多体系统动力学的重大工程应用实例.     

矩形薄板屈曲分析的高阶有限条传递矩阵法

针对矩形薄板屈曲,基于基尔霍夫板理论,采用半解析有限条法和含有中间节线的高阶有限条法推导条元的控制方程。在此基础上,根据传递矩阵形成单元传递方程和系统传递矩阵,形成了分析薄板屈曲临界力和屈曲模态的矩形薄板屈曲分析的高阶有限条传递矩阵法。采用该方法分析了两种边界条件下四边受压矩形板的屈曲临界力,并与理论解和有限元解比较,实例证明该方法有效。此方法在有限条传递矩阵法的基础上可进一步提高计算精度。     

拟协调分层薄壳单元在圆柱薄壳结构弹-塑性分析中的应用

本文基于拟协调元的基本原理,引入薄壳分层子单元的概念,提出了用于圆柱薄壳结构弹-塑性分析的三角形和矩形拟协调分层圆柱薄壳单元的模型,给出了第k层薄壳分层子单元的弹-塑性矩阵和物理矩阵[D~(k)]的表达式,并最后给出了整个薄壳单元的物理矩阵和刚度矩阵的表达式。 根据上述原理和方法用Fortran语言编制了圆柱薄壳结构弹-塑性有限元分析程序,实例计算与实验结果较为吻合,从而说明用本方法进行圆柱薄壳结构的弹-塑性分析是可靠而行之有效的。     

New matrix method for response analysis of circumferentially stiffened non-circular cylindrical shells under harmonic pressure

Based on the governing equation of vibration of a kind of cylindrical shells written in a matrix differential equation of the first order,a new matrix method is pre- sented for steady-state vibration analysis of a noncircular cylindrical shell simply sup- ported at two ends and circumferentially stiffened by rings under harmonic pressure.Its difference from the existing works by Yamada and Irie is that the matrix differential equation is solved by using the extended homogeneous capacity precision integration ap- proach other than the Runge-Kutta-Gill integration method.The transfer matrix can easily be determined by a high precision integration scheme.In addition,besides the normal interacting forces,which were commonly adopted by researchers earlier,the tan- gential interacting forces between the cylindrical shell and the rings are considered at the same time by means of the Dirac-δfunction.The effects of the exciting frequencies on displacements and stresses responses have been investigated.Numerical results show that the proposed method is more efficient than the aforementioned method.     

New matrix method for analyzing vibration and damping effect of sandwich circular cylindrical shell with viscoelastic core

Based on the linear theories of thin cylindrical shells and viscoelastic materials, a governing equation describing vibration of a sandwich circular cylindrical shell with a viscoelastic core under harmonic excitation is derived. The equation can be written as a matrix differential equation of the first order, and is obtained by considering the energy dissipation due to the shear deformation of the viscoelastic core layer and the interaction between all layers. A new matrix method for solving the governing equation is then presented With an extended homogeneous capacity precision integration approach. Having obtained these, vibration characteristics and damping effect of the sandwich cylindrical shell can be studied. The method differs from a recently published work as the state vector in the governing equation is composed of displacements and internal forces of the sandwich shell rather than displacements and their derivatives. So the present method can be applied to solve dynamic problems of the kind of sandwich shells with various boundary conditions and partially constrained layer damping. Numerical examples show that the proposed approach is effective and reliable compared with the existing methods.     

具有约束层阻尼贮液圆柱容器的耦振与减振特性分析

该文在对空圆柱层合壳(不充液)振动分析研究的基础上,借助线性势流理论,进一步考虑液固耦合效应,导出了敷有CLD贮液圆柱层合壳谐耦振的一阶常微分矩阵方程,该方程右边多了液动压力项.由于它不能预先给定,导致方程中出现未知项.为了克服这一困难,文中研究了液动压力的解式,并采用新型齐次扩容精细积分技术,提出了一种高效率和高精度的半解析半数值解法.进而还求解了CLD贮液圆柱容器在地面谐运动激励下的响应;通过大量数值计算分析了CLD的厚度、长度、敷设位置以及粘弹芯的复剪切模量对减振效果的影响.计算还表明了有液体的存在,这些影响和空容器时是不一样的.文中方法为CLD贮液容器的控制优化提供了有力手段.     

NONLINEAR BENDING OF THE SHALLOW SPHERICAL SHELLS WITH VARIABLE THICKNESS UNDER AXISYMMETRICAL LOADS

Based on the differential equation of the nonlinear bending of shallow sphericalshells with variable thickness under axisymmetrical loads,this paper studies thenumerical solution of the nonlinear differential equation by means of interpolatingmatrix method.The analysis of the results indicates that the suggested method is easyto implement and obtains the same high accuracy for both the displacements and theinternal forces.     

求解二维结构-声耦合问题的一种半数值半解析方法

基于传递矩阵法和虚拟源强模拟技术提出了一种求解在谐激励作用下二维结构-声相互作用问题的半数值半解析法．在足够小的积分步长内，文中对任意形状弹性环沿周向曲线坐标的非齐次状态微分方程组，建立了一种齐次扩容方法．对于外声场，采用多圆形虚拟源强配置方案。并在每一条圆形配置曲线上将源强密度函数用Fourier级数展开，同时结合快速Fourier变换法，提出了一种高精度、高效率求解任意形状二维孔穴Helmholtz外问题的快速算法．在耦合方程的求解方面，根据叠加原理，将外激励和虚拟源强的Fourier级数展开项作为广义力分别作用在弹性环上，借助齐次扩容方法和精细积分法求得弹性环的状态向量，再利用流固交接条件和最小二乘法直接建立了耦合系统的求解方程．文中给出了二个典型弹性环在集中谐激励力作用下声辐射算例，计算结果表明该文方法较通常采用的混合FE-BE法更为有效．     

病态代数方程的精细积分解法

基于精细积分思想,提出了一种有效的病态代数方程组求解方法。类似于稳态热传导方程可视为瞬态热传导方程的极限形式,将具有正定对称实系数矩阵的病态代数方程组归结为一个常微分方程组初值问题的极限形式,并在此基础上建立了病态代数方程组的精细积分解法。该方法不仅精度高,而且能以指数速度收敛,具有较高的效率。本文还讨论了病态代数方程...     

薄壳问题的一种数值解法

本文直接从三维弹性力学微分方程出发,依据三维的Kelvin解,应用最小二乘法建立了三维虚边界元法解薄壳问题的一般方法。本方法的显著优点是：不论求解何种壳体问题,思想是不变的,均以三维的Kelvin解来建立方程,而勿需对不同几何形状的壳本采用不同的基本解。文中给出了数值算例,以作为本方法的应用。本文方法与边界元直接法相比,优点在于无需处理奇异积分,且系数阵是对称的;再者,本文方法思想简单,程序实现容易。     

A SEMI－ANALYTICAL AND SEMI－NUMERICAL METHOD FOR SOLVING 2－D SOUND－STRUCTURE INTERACTION PROBLEMS

Based on the transfer matrix method and the virtual source simulation technique,this paper proposes a novel semi-analytical and semi-numerical method for solving 2-D sound-structure interaction problems under a harmonic excitation. Within any integration segment,as long as its length is small enough, along the circumferential curvilinear coordinate, the nonhomogeneous matrix differential equation of an elastic ring of complex geometrical shape can be rewritten in terms of the homogeneous one by the method of extended homogeneous capacity proposed in this paper. For the exterior fluid domain, the multi-circular virtual source simulation technique is adopted. The source density distributed on each virtual circular curve may be ex-panded as the Fourier‘‘s series. Combining with the inverse fast Fourier transformation, a higher accuracy and efficiency method for solving 2-D exterior Helmholtz‘s problems is presented in this paper. In the aspect of solution to the coupling equations, the state vectors of elastic ring induced by the given harmonic excitation and generalized forces of coefficients of the Fourier series can be obtained respectively by using a high precision integration scheme combined with the method of extended homogeneous capacity put forward in this paper. According to the superposition principle and compatibility conditions at the interface between the elastic ring and fluid, the algebraic equation of system can be directly constructed by using the least square approximation. Examples of acoustic radiation from two typical fluid-loaded elastic rings under a harmonic concentrated force are presented. Numerical results show that the method proposed is more efficient than the mixed FE-BE method in common use.     

圆锥壳自由振动传递函数解

本文在线性弹性理论基础上，给出了一种求解圆锥薄壳自由振动的渐进传递函数解法，壳体的三个位移分量，外力和边界条件首先沿环向展开的Ｆｏｕｒｉｅｒ级数，然后关于时间变量进行Ｌａｐｌａｃｅ变换，这样就将壳体的控制方程化为一系列含复参数ｓ的变系数常微分方程组，通过定义状态变量。得到了壳体动力学问题的状态空间控制微分方程，引入一小参数，并利用摄动技术就可以得到微分方程的渐进传递函数解，将各于锥段的解进行综合，     

NONLINEAR NATURAL FREQUENCY OF SHALLOW CONICAL SHELLS WITH VARIABLE THICKNESS

IntroductionTheplatesandtheshellswithvariablethicknessarewidelyusedinengineering .Theproblemaboutstaticshasbeenstudiedbymanyscholars;therearemanyRefs .[1 -4 ]inthisfield .Papersaboutnonlineardynamicsaremuchless[5 ,6 ].Inthispaper,selectingthemaximumamplitudeinthecenterofshallowconicalshellswithvariablethicknessasperturbationparameter,thenonlinearnaturalfrequencyofshallowconicalshellswithvariablethicknessisobtainedbymethodgiveninRef.[7] .Thenonlinearnaturalfrequencyisnotonlyconnectedwiththeva…