1007-3124
2006 Issue 2
The methods of obtaining lower strength shock wave in shock tube
LIN Jian-min~1;WEI Yi-jia~1;ZHANG Da-you~2
LIN Jian-min~1;WEI Yi-jia~1;ZHANG Da-you~2
..............page:63-67
Design of six-component ablating and rotation balance calibration system
CHEN De-jiang~1;WU Dong~1;LIU Wei-qiang~2
CHEN De-jiang~1;WU Dong~1;LIU Wei-qiang~2
..............page:68-71
Analysis on data precision and influential factors of experiments at high incidence
WANG Yuan-jing;FAN Zhao-lin;L Quan-zhou;HE Zhong;WU Jun-qiang
WANG Yuan-jing;FAN Zhao-lin;L Quan-zhou;HE Zhong;WU Jun-qiang
..............page:12-17
Numerical study of supersonic combustion of ethylene
YIN Yue;YU Gang
YIN Yue;YU Gang
..............page:55-57,77
Measuring nonequilibrium visible radiation of spherical steel model in ballistic range
LIU Jun~1;SHI An-hua~2;LE Jia-ling~2
LIU Jun~1;SHI An-hua~2;LE Jia-ling~2
..............page:58-62
Investigation on the effects of the height of close canard wing on the aerodynamic characteristics of a forward-swept configuration
ZHAN Jing-xia;WANG Jin-jun;ZHAO Xia;LI Tian
ZHAN Jing-xia;WANG Jin-jun;ZHAO Xia;LI Tian
..............page:50-54
The characteristics of the tracer particles used in water flow field for PIV system
RUAN Chi;SUN Chuan-dong;BAI Yong-lin;WANG Yi-shan;REN Ke-hui;FENG Shan
RUAN Chi;SUN Chuan-dong;BAI Yong-lin;WANG Yi-shan;REN Ke-hui;FENG Shan
..............page:72-77
A new method for studying the unsteady vortex frequency characteristics on rotor blades of turbine engine
LI Zhi-ping;LI Qiu-shi;YUAN Wei;HOU An-ping;LU Ya-jun
LI Zhi-ping;LI Qiu-shi;YUAN Wei;HOU An-ping;LU Ya-jun
..............page:7-11
Numerical simulation of interaction of blast wave and supersonic moving body
WANG Hui-ling~1;LI Yu-liang~2;NI Hong-li~1;LE Jia-ling~1
WANG Hui-ling~1;LI Yu-liang~2;NI Hong-li~1;LE Jia-ling~1
..............page:1-6,17
Research and implementation of field bus in wind tunnel
ZHANG Jun;ZHU Ru-song;SHI Hong-chang;ZHU Bo
ZHANG Jun;ZHU Ru-song;SHI Hong-chang;ZHU Bo
..............page:94-96
Research on frequency response of tube pressure measurement system
YANG Yan-jing;CHEN Qing-song;CAI Feng;GU Zhi-fu
YANG Yan-jing;CHEN Qing-song;CAI Feng;GU Zhi-fu
..............page:85-89
Balance development of XX torpedo using the rocket-boosting in the separation test of the torpedo and the rocket in high speed wind tunnel
PENG Chao;SHI Yu-jie
PENG Chao;SHI Yu-jie
..............page:82-84,96
A new method for propeller power simulation test
ZHANG Xi-jin~1;ZHANG Hui~2
ZHANG Xi-jin~1;ZHANG Hui~2
..............page:78-81,93
Research of nonequilibrium structure of strong shock front
ZHANG Ruo-ling~1;LE Jia-ling~1;WANG Su~2;CUI Ji-ping~2
ZHANG Ruo-ling~1;LE Jia-ling~1;WANG Su~2;CUI Ji-ping~2
..............page:36-40,49
Investigation on application of Gurney flap to triplane configuration aircraft lift-enhancement
WANG Jin-jun;CAI Ze-ming;LIU Tie-zhong;LI Ya-chen
WANG Jin-jun;CAI Ze-ming;LIU Tie-zhong;LI Ya-chen
..............page:30-35
Research of airframe/scramjet integrated design of hypersonic vehicle
CHE Jing;TANG Shuo
CHE Jing;TANG Shuo
..............page:41-44,49
The research on calibration technique of balance in calibration tank of turbine power simulator
FENG Shi-jun~1;BAI Cun-ru~1;LI Cong~2
FENG Shi-jun~1;BAI Cun-ru~1;LI Cong~2
..............page:90-93
Study on high angle of attack test technique of rear sting supports
ZHU Ming-hong;WANG Xun-nian;ZHANG Jun;SUN Chuan-bao
ZHU Ming-hong;WANG Xun-nian;ZHANG Jun;SUN Chuan-bao
..............page:25-29,35
Wind load on the cantilevered-structure of capital new museum's roof
CHEN Qing-song;CHEN Xue-rui;CAI Feng;YANG Yan-jing;GU Zhi-fu
CHEN Qing-song;CHEN Xue-rui;CAI Feng;YANG Yan-jing;GU Zhi-fu
..............page:18-24
Experimental research on infrared radiation from hypersonic blunt cone and wake
SHI An-hua;ZENG Xue-jun;LUO Jin-yang;CHEN Kun
SHI An-hua;ZENG Xue-jun;LUO Jin-yang;CHEN Kun
..............page:45-49