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热弹性正交双曲壳广义H-R变分原理和齐次向量方程
引用本文:李家宇, 徐红波, 刘艳红. 热弹性正交双曲壳广义H-R变分原理和齐次向量方程[J]. 工程力学, 2015, 32(4): 8-14. DOI: 10.6052/j.issn.1000-4750.2013.10.0996
作者姓名:李家宇  徐红波  刘艳红
作者单位:1.广州民航职业技术学院飞机维修工程学院,广州 510403;;2.中国民航大学航空维修工程学院,天津 300300
摘    要:基于热弹性体基本方程,根据弹性体修正后的H-R变分原理,建立正交双曲坐标系下热弹性体在温度梯度下的广义H-R变分原理,并推导了相应的非齐次广义Hamilton正则方程。再根据对偶变量理论,通过增加方程的维数,导出了可独立求解的齐次向量方程。齐次向量方程的导出,大大简化了热弹性层合正交双曲壳的求解过程,提高了计算精度。实例分析验证了该文方法的正确性。

关 键 词:热弹性体  正交双曲壳  广义H-R变分原理  对偶变量理论  齐次向量方程
收稿时间:2013-10-24
修稿时间:2014-05-05

GENEALIZED H-R VARIATION PRINCIPLE AND HOMOGENEOUS VECTOR EQUATION OF THERMO-ELASTIC ORTHOGONAL HYPERBOLIC SHELL
LI Jia-yu, XU Hong-bo, LIU Yan-hong. GENEALIZED H-R VARIATION PRINCIPLE AND HOMOGENEOUS VECTOR EQUATION OF THERMO-ELASTIC ORTHOGONAL HYPERBOLIC SHELL[J]. Engineering Mechanics, 2015, 32(4): 8-14. DOI: 10.6052/j.issn.1000-4750.2013.10.0996
Authors:LI Jia-yu  XU Hong-bo  LIU Yan-hong
Affiliation:1.Aircaft Maintenance College, Civil Aviation College of Guangzhou, Guangzhou 510403, China;;2.Aeronautical Engineering College, Civil Aviation University of China, Tianjin 300300, China
Abstract:By introducing the basic equations and the modified H-R (Hellinger-Reissner) variation principle of thermo-elastic body, a new generalized H-R variation principle, subjected to the orthogonal hyperbolic coordinate and the temperature gradient, is proposed. Meanwhile, the relevant nonhomogeneous generalized Hamilton canonical equation is deduced. According to the symplectic variable theory, the homogeneous vector equation, which could be solved independently, is obtained by increasing the dimension of the nonhomogeneous generalized Hamilton canonical equation. The homogeneous vector equation simplifies the solution procedure, and improves numerical precision of the thermo-elastic laminated orthogonal hyperbolic shell. Numerical examples are used to verify the method.
Keywords:thermo-elastic body  orthogonal hyperbolic shell  generalized H-R variation principle  symplectic variable theory  homogeneous vector equation
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