Three analysis models of torsional frequency of stiffening cylindrical shell
-
摘要: 为了给火箭等加筋圆柱壳结构的简化计算提供理论基础,研究了加筋圆柱壳面积等效方法中的扭转刚度计算方法,说明了不能直接根据等效厚度计算扭转刚度的物理机理,得到了桁条对圆柱壳扭转刚度的贡献可以忽略的结论.根据等效厚度以及桁条与蒙皮连接关系的不同处理方法,给出了计算扭转固有振动频率的等效梁模型、变厚度壳模型和壳-梁模型,分析了桁条在3种模型中对刚度和质量(包括转动惯量)的不同作用.为了消除根据等效厚度计算扭转刚度和扭转固有振动频率的偏差,分别给出了扭转刚度和扭转固有振动频率的修正方法.数值结果验证了修正方法和所得结论的正确性.Abstract: For simplifying the analysis of stiffening cylindrical shell in rocket, the computational method of torsional rigidity in the area-equivalence method was studied for the stringers in stiffening cylindrical shell, it is shown that the effect of stringers on the torsional rigidity of stiffening cylindrical shell is negligible. The equivalent beam or shell model with uniform thickness, the equivalent shell model with varied thickness and three dimensional (3-D) beam-shell model were proposed to solve the inherent torsional vibration frequency, and the features of these models were discussed. It was theoretically revealed that the obtained equivalent thickness by the area-equivalence method could not be directly used to calculate the torsional rigidity. Two modification methods, namely, the rigidity reduction method and frequency modified method, were presented when the equivalent thickness was directly utilized to solve the torsional frequencies. Numerical comparisons validate the proposed methods and models.
-
Key words:
- cylindrical shell /
- stringer /
- rocket /
- torsional frequency
-
[1] 邱吉宝.航天器计算结构动力学研究情况展望[J].导弹与航天运载技术,1993(4):37-44 Qiu Jibao.Prospect for computational structural dynamics of space vehicle[J].Missiles and Space Vehicles,1993(4):37-44 (in Chinese) [2] 王毅,朱礼文,王明宇,等.大型运载火箭动力学关键技术及其进展综述[J].导弹与航天运载技术,2000(1):29-37 Wang Yi,Zhu Liwen, Wang Mingyu,et al.Summary of some key technologies on dynamics of large launch vehicle[J].Missiles and Space Vehicles,2000(1):29-37 (in Chinese) [3] 邱吉宝,王建民.运载火箭模态试验仿真技术研究新进展[J].宇航学报,2007,28(3):515-521 Qiu Jibao,Wang Jianmin.The recent progresses on research into modal test simulation techniques for launch vehicles[J].Journal of Astronautics,2007,28(3):515-521 (in Chinese) [4] 王龙生,张德文.火箭结构有限元分析的若干问题[J].强度与环境,1988(3):45-53 Wang Longsheng,Zhang Dewen.Several problems in structural finite element analysis of rockets[J].Structure & Environment Engineering,1988(3):45-53 (in Chinese) [5] 龙乐豪.总体设计:上册[M].北京:宇航出版社,1989:469-475 Long Lehao.Systems design:volume I[M].Beijing:Astronautics Press,1989:469-475 (in Chinese) [6] 潘忠文.运载火箭动力学建模及振型斜率预示技术[J].中国科学,E辑:技术科学,2009,39(3):469-473 Pan Zhongwen.The Dynamical modelling and modal slope indicate technique of launch vehicle [J].Science in China,Series E:Technological Sciences[J],2009,39(3):469-473 (in Chinese) [7] 邓魁英,王毅.火箭动特性的缩比模型及建模分析[J].导弹与航天运载技术,2003(3):6-12 Deng Kuiying,Wang Yi.Studies on the scaled model and mathematical model for the overall dynamic characteristics of launch vehicle [J].Missiles and Space Vehicles,2003(3):6-12 (in Chinese) [8] 李道奎,刘林,万军.牵制释放过程中火箭液体推进剂的建模研究[J].强度与环境,2008,35(6):14-18 Li Daokui,Liu lin,Wan Jun.Study of the model of rocket-s liquid propellant in the process of hold-down and release[J].Structure & Environment Engineering,2008,35(6):14-18 (in Chinese) [9] 王建民,荣克林.捆绑火箭全箭动力学特性研究[J].宇航学报,2009,30(3):821-826 Wang Jianmin,Rong Kelin.The research of dynamic characteristics for the strap-on launch vehicle[J].Journal of Astronautics,2009,30(3):821-826(in Chinese) [10] Yoshiki Morino.Vibration test of 1/5 H-II launch vehicle .AIAA-87-0783,1987
点击查看大图
计量
- 文章访问数: 2945
- HTML全文浏览量: 96
- PDF下载量: 682
- 被引次数: 0