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Large Deformation Analyses of Space-Frame Structures., Using Explicit Tangent Stiffness Matrices, Based on the Reissner variational principle and a von Karman Type Nonlinear Theory in Rotated Reference Frames

机译:基于显式正切刚度矩阵,基于Reissner变分原理和von Karman型非线性理论的旋转参考框架中的空间框架结构大变形分析

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This paper presents a simple finite element method, based on assumed moments and rotations, for geometrically nonlinear large rotation analyses of space frames consisting of members of arbitrary cross-section. A von Karman type nonlinear theory of deformation is employed in the updated Lagrangian co-rotational reference frame of each beam element, to account for bending, stretching, and torsion of each element. The Reissner variational principle is used in the updated Lagrangian co-rotational reference frame, to derive an explicit expression for the (12×12) symmetric tangent stiffness matrix of the beam element in the co-rotational reference frame. The explicit expression for the finite rotation of the axes of the co-rotational reference frame, from the global Cartesian reference frame is derived from the finite displacement vectors of the 2 nodes of each finite element. Thus, the explicit expressions for the tangent stiffness matrix of each finite element of the beam, in the global Cartesian frame, can be seen to be derived as text-book examples of nonlinear analyses. When compared to the primal (displacement) approach wherein C~1 continuous trial functions (for transverse displacements) over each element are necessary, in the current approach the trial functions for the transverse bending moments and rotations are very simple, and can be assumed to be linear within each element. The present (12×12) symmetric tangent stiffness matrices of the beam, based on the Reissner variational principle and the von Karman type simplified rod theory, are much simpler than those of many others in the literature. The present approach does not involve such numerical procedures as selective reduced integration or suppression of attendant Kinematic modes. The present methodologies can be extended to study the very large deformations of plates and shells as well. Metal plasticity may also be included, through the method of plastic hinges, etc. This paper is a tribute to the collective genius of Theodore von Karman (1881-1963) and Eric Reissner (1913-1996).
机译:本文基于假定的力矩和旋转,提出了一种简单的有限元方法,用于对由任意横截面组成的空间框架进行几何非线性大旋转分析。在每个梁单元的更新的拉格朗日同旋转参考系中采用了von Karman型非线性变形理论,以说明每个单元的弯曲,拉伸和扭转。 Reissner变分原理用于更新的Lagrangian同向旋转参考系中,以得出同向旋转参考系中梁单元的(12×12)对称切线刚度矩阵的显式表达式。从全局笛卡尔坐标系开始,对同旋转参考系的轴进行有限旋转的显式表达式是从每个有限元的2个节点的有限位移矢量中得出的。因此,在整体笛卡尔框架中,梁的每个有限元的切线刚度矩阵的显式可以看作是非线性分析的教科书示例。与原始(位移)方法相比,在每个方法中必须有C〜1个连续试验函数(用于横向位移),在当前方法中,横向弯曲力矩和旋转的试验函数非常简单,可以假定为在每个元素内都是线性的。基于Reissner变分原理和von Karman型简化杆理论的梁的当前(12×12)对称切线刚度矩阵比文献中的许多其他梁要简单得多。本方法不涉及诸如选择性减少积分或抑制伴随运动学模式的数值程序。本方法可以扩展到研究板和壳的很大变形。通过塑料铰链等方法,也可以包括金属可塑性。本文是对西奥多·冯·卡曼(Theodore von Karman,1881-1963年)和埃里克·里斯纳(Eric Reissner,1913-1996年)的共同天才的致敬。

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