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计算曲面壳体等效节点热载荷的新方法
引用本文:刘云飞,吕军,白瑞祥,高效伟.计算曲面壳体等效节点热载荷的新方法[J].力学学报,2015,47(2):328-336.
作者姓名:刘云飞  吕军  白瑞祥  高效伟
作者单位:大连理工大学工业装备结构分析国家重点实验室, 大连116024
基金项目:国家自然科学基金(11172055,11302040);中国博士后科学基金(2014T70244)资助项目~~
摘    要:提出了一种利用平面壳单元计算曲面壳体热应力问题等效节点热载荷的新方法, 具有较高的计算精度. 首先在平面壳元的理论基础上, 在壳单元切平面建立局部坐标系; 然后根据提出的理论, 利用单元节点整体坐标直接计算壳单元等效节点热载荷积分方程中所需的未知量, 如: 形函数对局部坐标的导数、从对局部坐标积分转换到自然坐标积分时的雅可比行列式等; 最后, 根据提出的算法求出从局部坐标转换到整体坐标的转换矩阵, 进而求出整体坐标系下壳单元等效节点热载荷. 通过与商用软件ANSYS 的计算结果进行对比分析, 证明提出的方法是正确而且精确的.

关 键 词:等效节点热载荷  切平面  雅可比行列式  热应力
收稿时间:2014-05-15
修稿时间:2014-07-09

A NEW METHOD TO COMPUTE THERMAL EQUIVALENT NODAL LOADS ON CURVED SURFACES
Liu Yunfei,Lü Jun,Bai Ruixiang,Gao Xiaowei.A NEW METHOD TO COMPUTE THERMAL EQUIVALENT NODAL LOADS ON CURVED SURFACES[J].chinese journal of theoretical and applied mechanics,2015,47(2):328-336.
Authors:Liu Yunfei  Lü Jun  Bai Ruixiang  Gao Xiaowei
Institution:State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China
Abstract:A new method using flat shell element to compute thermal equivalent nodal loads on curved surface is presented. Firstly, the local Cartesian coordinate system is established on the tangential plane to the element surface. Then, the unknowns included in the integrand about thermal equivalent nodal loads are computed in terms of the theory proposed in this paper, which include the derivative of shape functions with respect to the variables of local coordinate system and the Jacobian of the transformation from the local three-dimensional coordinate system to the intrinsic two-dimensional coordinate system of the surface patch. Finally, a matrix transformation formulation is derived from the local Cartesian coordinate system to the global one, based on which the thermal equivalent nodal loads in the global Cartesian coordinate system can be found. Comparison with the results from FEM analysis shows that the proposed method in this paper is correct and accurate.
Keywords:thermal equivalent nodal loads  tangential plane  Jacobian  thermal stress
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