1006-3919
2012 Issue 3
..............page:32-38
Mechanical performance analysis on wing\'s of Zephyr7 UAV
YIN Chengyue;GAO Puyun;GUO Jian;GUO Zheng;HOU Zhongxi
YIN Chengyue;GAO Puyun;GUO Jian;GUO Zheng;HOU Zhongxi
..............page:19-25
The automation of life reliability analysis for missile suspension structure
HE Xindang;LIU Yongshou;WEI Tao;GAO Zongzhan
HE Xindang;LIU Yongshou;WEI Tao;GAO Zongzhan
..............page:45-51
Unified constitutive modeling of solid propellant materials with evolving damage subjected to pressure loading
SHA Baolin;HOU Xiao
SHA Baolin;HOU Xiao
..............page:13-18
Experimental and finite element investigation on the thermal mechanical coupling of flaps
LI Lixia;WANG Qi
LI Lixia;WANG Qi
..............page:60-63
The mechanical behavior research of C/C composite bolt with tightening torque
MIN Changwan;TAN Zhiyong;LONG Liping
MIN Changwan;TAN Zhiyong;LONG Liping
..............page:1-6
Simulation of the pendulum shock response spectra testing machine
WANG Bing;TLAN Zhenqiang;ZHANG Qiaoshou
WANG Bing;TLAN Zhenqiang;ZHANG Qiaoshou
..............page:26-31
The review of the high temperature modal test for the hypersonic vehicle
CHENG Hao;LI Haibo;JIN Ronghua;WU Zhenqiang;ZHANG Wei
CHENG Hao;LI Haibo;JIN Ronghua;WU Zhenqiang;ZHANG Wei
..............page:52-59
Stiffness analysis of aircraft wing based on finite element method
CHEN Bo;LIU Yang;WANG Aijun
CHEN Bo;LIU Yang;WANG Aijun
..............page:7-12
Analysis of structural vibration and radiated noise of gearbox shells
FAN Yongbo;WANG Duanzhi;CHEN Hongbo;XU Ming;OUYANG Fu
FAN Yongbo;WANG Duanzhi;CHEN Hongbo;XU Ming;OUYANG Fu
..............page:39-44