1006-3919
2011 Issue 3
..............page:14-18
Aeroelastic analysis of high-aspect ratio wing based on CFD/CSD
Cai Tianxing;Xu Min;Guo Minjie;Yao Weigang
Cai Tianxing;Xu Min;Guo Minjie;Yao Weigang
..............page:19-23
Simulation study for a resonant fixture design
Shi Meng;Ma Aijun;Liu Hongying;Feng Xuemei;Dong Rui;Zhu Jingtao
Shi Meng;Ma Aijun;Liu Hongying;Feng Xuemei;Dong Rui;Zhu Jingtao
..............page:45-49
A study of dynamic response analysis new method for coupled satellite/launch vehicle
Qiu Jibao;Zhang Zhengping;Li Haibo;Han Li;Huang Bo
Qiu Jibao;Zhang Zhengping;Li Haibo;Han Li;Huang Bo
..............page:1-9
The technology of dynamics design and analysis for the structure of advanced composite material
Tan Zhiyong;Min Changwan;Long Liping
Tan Zhiyong;Min Changwan;Long Liping
..............page:24-28
The application of integrating phase resonance and phase separation to modal test for missile
Li Xiaodong;Qi Piqian;Yang Wenqi
Li Xiaodong;Qi Piqian;Yang Wenqi
..............page:10-13
..............page:64
Research situation of multiple site damages aircraft structure
Li Zhengqi;Hu Jianjun;Chen Yueliang
Li Zhengqi;Hu Jianjun;Chen Yueliang
..............page:50-56
Design and application of strength software STRANAS for stiffened panels
Wu Cunli;Zhang Qian;Duan Shihui
Wu Cunli;Zhang Qian;Duan Shihui
..............page:36-44
The nonlinear character of static stiffness in the structure with bolted flanged connection under small deformation
Luan Yu;Liu Song;Guan Zhenqun;Zhang Xi;Wang Lipeng;Yang Zhiguang
Luan Yu;Liu Song;Guan Zhenqun;Zhang Xi;Wang Lipeng;Yang Zhiguang
..............page:29-35
The application of reliability evaluation method in launch vehicle valves
Cui Jingzhi;Sun Faguo;Ding Jianchun;Wang Jianzhong
Cui Jingzhi;Sun Faguo;Ding Jianchun;Wang Jianzhong
..............page:57-63