1006-3919
2012 Issue 1
Branch modal synthesis method for coupled launch vehicle and spacecraft (Ⅱ)
Qiu Jibao;Zhang Zhengping;Li Haibo;Huang Bo;Zhang Zhong
Qiu Jibao;Zhang Zhengping;Li Haibo;Huang Bo;Zhang Zhong
..............page:1-11
Application of liquid-solid coupled numerical simulation method in transient heat transfer calculation of turbo-blade
Guo Jungang;Wang Chunxia;Hu Liguo
Guo Jungang;Wang Chunxia;Hu Liguo
..............page:22-28
A rapid prediction method for elastic frequency of launch vehicles
Ma Daoyuan;Liu Wei;Li Yufei;Wang Jianmin
Ma Daoyuan;Liu Wei;Li Yufei;Wang Jianmin
..............page:29-33
Reliability based design optimization method of compliant folding mechanisms
Li Yuansheng;Ren Hao;Wen Zhixun;Yue Zhufeng
Li Yuansheng;Ren Hao;Wen Zhixun;Yue Zhufeng
..............page:34-44
Based on aerodynamic/aeroacoustic/structure coupling simulation study
Xu Min;Zhang Ningchuan
Xu Min;Zhang Ningchuan
..............page:12-17
Design of the FPGA-based wireless sensors for field data collection
Zhang Guoyi;Wang Yue;Wang Zhuo;Han Qi
Zhang Guoyi;Wang Yue;Wang Zhuo;Han Qi
..............page:57-64
..............page:49-56
Research on identification of dynamics parameters of water exit of the missile
Zhao Wei;Huang Youxian;Wei Bingfeng
Zhao Wei;Huang Youxian;Wei Bingfeng
..............page:18-21
The effect of deflagrated pressure pulse on intension of pyro-actuator
Du Yonggang;Fu Zhaohui;Xia Chengming;Yang ZhenChun;Yang Yong
Du Yonggang;Fu Zhaohui;Xia Chengming;Yang ZhenChun;Yang Yong
..............page:45-48