纵向过载环境下变质量欧拉梁动特性分析方法

邢誉峰; 谢珂; 潘忠文

纵向过载环境下变质量欧拉梁动特性分析方法

1.
北京航空航天大学航空科学与工程学院, 北京 100191
2. 北京宇航系统工程研究所, 北京100076

基金项目: 国防973计划资助项目(613133); 国家自然科学基金资助项目(11172028)

详细信息

中图分类号: O342
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出版历程
- 收稿日期: 2012-07-27
- 修回日期: 2012-12-06
- 网络出版日期: 2013-08-30

Dynamic analysis methods of variable-mass Euler beam under longitudinal overload

1.
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. Beijing Astronautics Systems Engineering Institute, Beijing 100076, China

摘要

摘要: 过载是火箭的真实环境.考虑纵向过载环境,根据Hamilton变分原理,得到了欧拉梁变系数横向自由振动微分方程,证明了该变系数系统存在满足刚度和质量正交条件的本征解,揭示了纵向过载环境下欧拉梁本征函数的非对称性.用本征向量叠加方法和改进欧拉中点直接积分算法求解了该变系数系统的动态响应,二者结果的一致性说明该理论推导的正确性和方法的可行性.
- 过载 /
- 变质量 /
- 变系数 /
- 本征向量 /
- 正交条件
Abstract: Overload is the real environment of launch vehicles. The variable-coefficient transverse differential equation for the free vibration of Euler beam under longitudinal overload was derived on the basis of the Hamiltonian principle. For the variable-coefficient dynamic system, the existence of eigensolutions satisfying the orthogonal conditions of mass and stiffness was proved, and the asymmetry of such eigenfunction was revealed. A modified Euler symplectic midpoint difference method and a modified mode superposition method were employed to solve the equation of variable-mass systems. The numerical results of the two methods agree well, and validate the correctness of present theory and feasibility of the two methods.
- overload /
- variable-mass /
- variable-coefficient /
- eigenvector /
- orthogonal condition

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参考文献(13)

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