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Journals   A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
Journal of Propulsion Technology
1001-4055
2006 Issue 3
Measurement of particle distribution in the solid impulsive thruster exhaust plume
ZHOU Hai-qing;YOU Zheng;ZHANG Ping
..............page:285-288
Effects of partial filling on the impulse of pulse detonation engine
ZHANG Qun;YAN Chuan-jun;FAN Wei;LI Qiang;LI Jiang-hong;YANG Bing-yu
..............page:280-284
Optimization design of multistage axial-flow compressor using multiobjective genetic algorithm
DING Wei;LIU Bo;CAO Zhi-peng;CHEN Yun-yong
..............page:230-233
Variable geometry effects on the scramjet ignition and combustion
PAN Yu;Li Da-peng;LIU Wei-dong;LIANG Jian-han;WANG Zhen-guo
..............page:225-229
Computation and assessment of aerodynamic stability of turbofan engine startup and acceleration
WANG Zhan-xue;QIAO Wei-yang;LI Wen-lan
..............page:221-224
Maneuverable missile and turbofan engine integrated design-constrain analysis and mission analysis
CHEN Yu-chun;LIU Zhen-de;SHI Ya-hong;TU Qiu-ye;WANG Xiao-dong
..............page:216-220
Experimental and theoretical research on performance optimization of turbofan engine
LIU Zhen-de;XUE Liang;CHEN Yu-chun;TU Qiu-ye;DONG Yan-zhao
..............page:211-215
Experimental investigation of vaporizing flameholder at low pressure and high temperature
WANG Jian;ZHANG Li;SU Xiang-rong
..............page:208-210
Experimental validation of flow field in the secondary combustor of a subscale ducted rocket
LIU Pei-jin;DONG Hao;WEI Xiang-geng;LI Yu-fei
..............page:205-207
Design optimization for solid rocket motor based on graph morphing
OU Hai-ying;ZHANG Wei-hua;XIE Hong-yu;LI Xiao-bin
..............page:201-204,207
Numerical optimization simulation on heat transfer in cooling channel of H2/O2 liquid rocket engine thrust chamber
WU Feng;WANG Qiu-wang;LUO Lai-qin;ZENG Min;SUN Ji-guo
..............page:197-200
Modal intervals-based system simulation and application for liquid propellant rocket engine
FAN Jiu-ming;SHEN Yan;ZHANG Min-shu;ZOU Jing-xiang
..............page:193-196
Channel gain schedule method on the aeroengine complex control scheme realization
ZHENG Tie-jun;WANG Xi;LUO Xiu-qin;LI Qi-han
..............page:276-279
Feature extraction based on genetic programming and linear discriminant analysis for fault diagnosis and its application
HOU Sheng-li;LI Ying-hong;WEI Xun-kai
..............page:270-275
Real time mathematical model of supersonic inlet of a turbofan engine
SHI Rui-jun;FAN Si-qi;ZHU Yu-bin;REN Xin-yu
..............page:266-269
Effect of circumferential exit-guide-vane layout to upstream flow field distortion
WANG Yan-gang;LIU Bo;MA Chang-you;GUAN Ji-wei
..............page:262-265
Effect of pressure and temperature distortion on turbine engine stability
CAI Yuan-hu;WANG Peng;WANG Zhan-xue;QIAO Wei-yang
..............page:257-261
Investigation of internal waverider-derived hypersonic inlet
YOU Yan-cheng;LIANG De-wang;HUANG Guo-ping
..............page:252-256
Heat transfer characteristics near a row of film cooling holes in interior of turbine blade
XU Lei;CHANG Hai-ping;CHANG Guo-qiang;ZHANG Jing-yang
..............page:248-251,265
Numerical simulation of inner flow field in centrifugal impeller with long, middle and short blades
CUI Bao-ling;ZHU Zu-chao;CHEN Ying;LIN Yong-gang
..............page:243-247
Numerical simulation of effects of steady circumferential total pressure distortion on a small fan
SUN Peng;FENG Guo-tai
..............page:239-242
Influence of solidity on flow field performance of bowed stator in compressor at low speed
ZHANG Yong-jun;YAN Pei-gang;MA Yan;HUANG Jia-hua;FENG Guo-tai;SU Jie-xian
..............page:234-238,247
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