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薄板哈密顿含参变分原理 总被引:1,自引:1,他引:0
将薄板哈密顿变分原理及其泛函),,,(xxxHVMwyP推广为含两个可选参数1h和2h的薄板哈密顿含参变分原理及其含参泛函),,,(21xxxHVMwyPhh。其推导过程为:首先将薄板Hellinger-Reissner变分原理及其泛函}){,(MwHRP推广为含可选参数1h的薄板Hellinger-Reissner含参变分原理及其含参泛函}){,(1MwHRhP。然后采用消元法(消去变量yM和xyM)和换元乘子法(增加变量xy和xV)由含参泛函}){,(1MwHRhP导出含两个可选参数的薄板哈密顿含参泛函),,,(21xxxHVMwyPhh。含参变分原理是多种变分原理的组合形式,并使多种变分原理之间得到沟通和融合。通过对参数1h和2h的合理选取和赋值,可以得到含参泛函的多种退化形式,为建立多种有限元模型创造条件。 相似文献
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陀螺系统辛子空间迭代法 总被引:1,自引:0,他引:1
转子系统的有限元分析可以导出陀螺系统的本征值问题.而陀螺本征值问题可在哈密顿体系下求解。基于辛子空间迭代法的思想,提出了一种求解陀螺系统本征值问题的算法。首先引入对偶变量,将陀螺动力系统导入哈密顿体系,将问题化为了哈密顿矩阵的本征值问题。由于稳定的陀螺系统其本征值必为纯虚数,利用这个特点。提出了对应陀螺系统的辛子空问迭代法,从而可以求出系统任意阶的本征值及其振型。算例证明了这种算法的有效性。 相似文献
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本文介绍弹性力学对偶求解体系的近期研究和进展:(1)提出一种新的正交关系。不用辛几何的概念,直接导出对偶微分方程组;(2)基于新正交关系,建立二维弹性力学特征函数展开直接解法,求得含可对角化边界条件下的显式封闭解:(3)将对偶求解体系推广到多坐标方向,建立多坐标方向的对偶微分方程和求解体系。(4)采用偏微分方程的算子解法,建立了板状弹性体的弯曲理论,把它的解分解为弯曲齐次解、特解、和衰减解:(5)将对偶求解体系推广应用于厚板和薄板问题,建立了有关的对偶微分方程,正交关系和变分原理。 相似文献
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基于弹性力学问题求解的辛方法,结合波传播理论,提出一个薄板结构稳态动力响应分析的新思路。首先,将薄板振动的控制方程导入辛对偶体系,应用分离变量法得到薄板波传播问题的本征值方程,求解得到本征值(波传播参数)与本征向量(波形);然后将物理空间求解体系转换到波空间,进而结合波传播以及波反射关系求解薄板结构的受迫振动问题。算例给出了矩形薄板在四边简支(SSSS)和一对边固支、另一对边简支(CCSS)两种边界条件下的输入点导纳以及动能和应变能;四边简支的结果与模态叠加法给出的解析解以及波有限元法的结果做了对比,对边固支-对边简支边界下的结果与有限元程序系统ABAQUS的参考解以及波有限元法结果做了对比,对比结果验证了该方法的精确性与有效性。 相似文献
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《振动工程学报》2016,(1)
基于薄板理论,采用回传射线矩阵法研究了两对边简支任意角连接有限尺寸V型薄板的功率流透射损失。引入对偶坐标系,在力作用点和板接缝处对结构进行离散,同时考虑弯曲波动与面内波动效应,根据结构连接处的位移协调条件、力平衡条件以及两端边界条件得到V型薄板结构的散射矩阵。根据对偶坐标系的内在物理关系得到整体相位矩阵,最后推导出结构的回转射线矩阵。在此基础上,建立了V型薄板结构的动态响应分析模型以及功率流分析模型,通过对简谐点激励力作用下结构的动态响应进行对比分析,证明回传射线矩阵法具有很高的求解精度与求解效率。最后,分析了V型薄板结构功率流传导问题,研究了不同角度、不同板厚和不同阻尼损耗因子的V型薄板的功率流透射损失变化规律。 相似文献
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根据古典阴阳互补和现代对偶互补的基本思想,系统地建立了分段线性弹性薄板动力学的各类非传统Hamilton增量变分原理.而这种非传统Hamilton型增量变分原理能反映分段线性弹性薄板动力学初值-边值问题的全部特征.文中给出一个重要的积分关系式,可以认为,在力学上它是分段线性弹性薄板动力学增量广义虚功原理的表式.从该式出发,不仅能得到薄板动力学的增量虚功原理,而且通过所给出的一系列广义Legendre变换,能系统地成对导出分段线性弹性薄板动力学的5类变量、3类变量、2类变量非传统Hamilton型增量变分原理的互补泛函,以及1类变量和相空间非传统Hamilton型增量变分原理的泛函.同时,通过这条新途径还能清楚地阐明这些原理之间的内在联系. 相似文献
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为求解机械臂最短路径问题,导出了机械臂末端路径长度的表示式,并将最短路径问题归结为一个泛函极值问题。为简化求解过程,将泛函极值问题转化成另一个同解的泛函极值问题,并利用变分法求出了表示后一问题解的微分方程组。利用上三角矩阵逆矩阵的表示式,将该微分方程组转化成了标准状态方程组,与微分几何方法相比,避免了逆矩阵计算,使转化过程更加简单。利用Matlab进行仿真,求出了3R机械臂最短路径所对应的三个关节角度的位移函数。 相似文献
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Eugenio Oñate Francisco Zárate 《International journal for numerical methods in engineering》2010,83(2):196-227
This paper describes a methodology for extending rotation‐free plate and beam elements to accounting for transverse shear deformation effects. The ingredients for the element formulation are a Hu–Washizu‐type mixed functional, a linear interpolation for the deflection and the shear angles over standard finite elements and a finite volume approach for computing the bending moments and the curvatures over a patch of elements. As a first application of the general procedure, we present an extension of the three‐noded rotation‐free basic plate triangle (BPT) originally developed for thin plate analysis to account for shear deformation effects of relevance for thick plates and composite‐laminated plates. The nodal deflection degrees of freedom (DOFs) of the original BPT element are enhanced with the two shear deformation angles. This allows to compute the bending and shear deformation energies leading to a simple triangular plate element with three DOFs per node (termed BPT+ element). For the thin plate case, the shear angles vanish and the element reproduces the good behaviour of the original thin BPT element. As a consequence the element is applicable to thick and thin plate situations without exhibiting shear locking effects. The numerical solution for the thick case can be found iteratively starting from the deflection values for the Kirchhoff theory using the original thin BPT element. A two‐noded rotation‐free beam element termed CCB+ applicable to slender and thick beams is derived as a particular case of the plate formulation. The examples presented show the robustness and accuracy of the BPT+ and the CCB+ elements for thick and thin plate and beam problems. Copyright © 2010 John Wiley & Sons, Ltd. 相似文献
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Y.-F. Dong J. A. Teixeira De Freitas 《International journal for numerical methods in engineering》1994,37(2):279-296
An hybrid stress element formulation based on internal, incompatible displacements is used to develop efficient Mindlin plate elements. The 4-node quadrilateral Mindlin plate element is derived from a modified energy functional. Both displacements and stresses are defined in the natural co-ordinate interpolation system. The assumed stress field is obtained by tensor transformation and so chosen as to ensure that the element is co-ordinate invariant and stable. Shear locking is avoided through an appropriate identification of the internal, incompatible displacement field. The role played by incompatible displacements in the formulation of hybrid stress elements for thin and moderately thick plates is discussed. Numerical applications are presented to illustrate the accuracy and reliability of the suggested Mindlin plate element. 相似文献
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Robert L. Spilker Nasir I. Munir 《International journal for numerical methods in engineering》1980,15(8):1239-1260
The assumed-stress hybrid finite element model is examined for application to the bending analysis of thin plates. A hybrid-stress functional is defined by using a Mindlin-type displacement assumption and including all components of stress. The Euler equations and matrix formulation corresponding to this functional are examined to assess the effects of plate thickness, and a rationale is presented for the selection of stress assumptions so that locking is avoided in the thin plate limit. To illustrate these concepts, a series of linear displacement quadrilateral elements are derived and tested, and the best of these elements is identified for suggested implementation in general-purpose computer programs. 相似文献
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Huoy-Shyi Tsay Fung-Huei Yeh 《International Journal for Computational Methods in Engineering Science and Mechanics》2017,18(4-5):220-229
Biot's poroelastic theory is used with classic plate theory and plane stress theory to determine the constitutive relationships for a thin poroelastic plate. The dynamic equations for the thin poroelastic plate are derived from the extended Hamilton's principle. The dynamic equations are then transformed to frequency domain and Galerkin's finite element method is used to derive the stiffness matrix of a triangular plate element. When impulsive loads and elastic boundary conditions are applied, the finite element frequency domain analysis for the thin poroelastic plates is achieved. Vibration behavior of thin elastic and poroelastic circular plates is accurately predicted. 相似文献