1001-4055
2006 Issue 2
..............page:186
Analysis of thermophysical properties of Daqing RP-3 aviation kerosene
FAN Xue-jun;YU Gang
FAN Xue-jun;YU Gang
..............page:187-192
Impact and friction sensitivity of composite modified double base propellant containing hexanitrohexaazaisowurtzitane (CL-20)
XU Si-yu;ZHAO Feng-qi;LI Shang-wen;HAO Hai-xia;GAO Hong-xu;DANG Yong-zhan
XU Si-yu;ZHAO Feng-qi;LI Shang-wen;HAO Hai-xia;GAO Hong-xu;DANG Yong-zhan
..............page:182-186
Operating characteristics analysis for air-breathing pulse detonation engine
QIU Hua;YAN Chuan-jun;XIONG Cha
QIU Hua;YAN Chuan-jun;XIONG Cha
..............page:176-181
Experimental investigation on devices of flame spreading in pulse detonation engine
FAN Yu-xin;WANG Jia-hua;LI Jian-zhong;ZHANG Yi-ning
FAN Yu-xin;WANG Jia-hua;LI Jian-zhong;ZHANG Yi-ning
..............page:171-175
Coordinative operation design for multiple controllers with variable input parameters
ZHENG Tie-jun;WANG Xi;JIANG Ping-guo;LI Qi-han
ZHENG Tie-jun;WANG Xi;JIANG Ping-guo;LI Qi-han
..............page:166-170
Numerical simulation of working process in turbofan engine on getting surge elimination system
LI Wei;LI Jun
LI Wei;LI Jun
..............page:162-165
Numerical simulation for ramjet cruising stage fuel-supplied oscillation
YANG Xi-wu;HE Bao-cheng;REN Feng-sheng;WANG Bin-yuan;LIU Rui-jie
YANG Xi-wu;HE Bao-cheng;REN Feng-sheng;WANG Bin-yuan;LIU Rui-jie
..............page:158-161
Fault diagnosis based on immunity strategy with similarity measurement of principle component kernel and its application
HOU Sheng-li;LI Ying-hong;WEI Xun-kai
HOU Sheng-li;LI Ying-hong;WEI Xun-kai
..............page:154-157,170
A multivariable decoupling control based on DRNN for aeroengine
ZHU Yu-bin;FAN Si-qi;REN Xin-yu;SHI Rui-jun
ZHU Yu-bin;FAN Si-qi;REN Xin-yu;SHI Rui-jun
..............page:150-153
Extrapolating component maps into the low speed and simulation of windmilling performance of turbofan engine
WANG Zhan-xue;WANG Yong-jie;QIAO Wei-yang;LIU Wen
WANG Zhan-xue;WANG Yong-jie;QIAO Wei-yang;LIU Wen
..............page:146-149,181
Turbopump fault detection system
XIE Guang-jun;HU Niao-qing
XIE Guang-jun;HU Niao-qing
..............page:141-145
Approach in early fault features extraction of aero-engine rotor system
WANG Zhong-sheng;LI Wei
WANG Zhong-sheng;LI Wei
..............page:137-140
Uncertainty optimization design of grain geometry parameters
LI Xiao-bin;ZHANG Wei-hua;WANG Zhong-wei
LI Xiao-bin;ZHANG Wei-hua;WANG Zhong-wei
..............page:132-136
Preliminary investigation on Busemann inlet starting characteristics
SUN Bo;ZHANG Kun-yuan
SUN Bo;ZHANG Kun-yuan
..............page:128-131
Temperature drop of propellant stream in injection-tube of thruster during start process
XIAO Ze-juan;CHENG Hui-er;ZHOU Hong-ling;HUANG Rui-sheng
XIAO Ze-juan;CHENG Hui-er;ZHOU Hong-ling;HUANG Rui-sheng
..............page:124-127,145
Hybrid RANS / LES simulation of the supersonic flow over two-dimensional cavities
SUN Ming-bo;LIANG Jian-han;WANG Zhen-guo
SUN Ming-bo;LIANG Jian-han;WANG Zhen-guo
..............page:119-123
Three-dimensional numerical investigation of vaneless counter-rotating turbine
ZHAO Qing-jun;WANG Hui-she;ZHAO Xiao-lu;XU Jian-zhong
ZHAO Qing-jun;WANG Hui-she;ZHAO Xiao-lu;XU Jian-zhong
..............page:114-118,123
Effect of primary holes on the velocity profiles downstream of a swirl cup
LANG Hong-jian;GUO Zhi-hui;HUANG Yong
LANG Hong-jian;GUO Zhi-hui;HUANG Yong
..............page:110-113
Sonic point position and critical pressure ratio in micro nozzles
HAO Peng-fei;YAO Zhao-hui;DING Ying-tao
HAO Peng-fei;YAO Zhao-hui;DING Ying-tao
..............page:106-109
Reduced chemical reaction kinetic model for combustion of methane
XIAO Bao-guo;QIAN Wei-qi;YANG Shun-hua;LE Jia-ling
XIAO Bao-guo;QIAN Wei-qi;YANG Shun-hua;LE Jia-ling
..............page:101-105
Experimental study for factors affecting rocket ejector performance in SMC combustion mode
LI Yu-fei;HE Guo-qiang;LIU Pei-jin
LI Yu-fei;HE Guo-qiang;LIU Pei-jin
..............page:97-100