| Citation: | Pan Zhongwen, Xing Yufeng, Yang Yanget al. Three analysis models of torsional frequency of stiffening cylindrical shell[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(9): 1156-1159. (in Chinese)
|
|
[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
|
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
Liu Xiaoming, Chen Wanchun, Xing Xiaolan, et al. Terrain following and autonomous landing using optical flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(1): 98-105. (in Chinese)
DownLoad: