The consistency of dynamic responses of a full scale spacecraft between ground tests and its space missions(II)
QIU Jibao;,ZHANG Zhengping;,LI Haibo;,ZHANG Zhong;,HAN Li;,REN Fang;

..............page:1-12

Dynamic characteristics analysis of constant pressure valve mounting bracket
ZHANG Lianwan;,WANG Daolian;,ZHAO Tao;,CUI Zhongwei;

..............page:13-19

Effect of ignition pressure peak and rate of pressurization on the strain response of grain
ZHANG Ming;,YANG Le;

..............page:20-25

Fixture design and practice of one type of the head of guided missile for vibration test
WEI Yingkui;,ZHANG Xiaoying;,BI Jingdan;,WEI Guo;

..............page:26-31

Finite element modeling and design variable influence analysis for compound flexible cover
LIU Feng;,AN Qingsheng;,LIN Nan;

..............page:32-37

The analysis of the structure and principle of the straight into water brake shock tower
DONG Rui;,FENG Xuemei;,WANG Jue;,SHI Meng;,AN Meiyan;,LIU Hongying;

..............page:38-44

Control efficiency analysis of aircraft wing based on CFD/CSD coupling technique
ZHANG Junran;,WANG Fusheng;,YUE Zhufeng;

..............page:45-51

The study of thermo-modal test technique based on true-random excitation
LI Xiaodong;,YANG Wenqi;,LIU Hao;

..............page:52-56

Application of single frame FFT method in processing of sine swept structure dynamics test signal
ZHANG Pengfei;,HU Yabing;,FU Wei;,WU JIaju;

..............page:57-63

zhong guo yu hang xue hui jie gou qiang du yu huan jing gong cheng zhuan ye wei yuan hui zuo zhong guo hang tian di ba zhuan ye xin xi wang 2015 nian du ji shu xin xi jiao liu hui zheng wen tong zhi
[1] zhong guo yu hang xue hui jie gou qiang du yu huan jing gong cheng zhuan ye wei yuan hui [2] zhong guo hang tian di ba zhuan ye xin xi wang ;

..............page:64-64