Journal of Propulsion Technology 2011 Issue 3 Investigation on the influence of jets spout location on detonation initiation via imploding annular shock waves

Investigation on the influence of jets spout location on detonation initiation via imploding annular shock waves
ZENG Hao;HE Li-ming;ZHANG Xiong-wei;LI Hai-peng;CHEN Xin

..............page:437-442

tui jin ji shu tou gao zhi nan

..............page:封3

Review of the development in torpedo thermal power technologies
CHEN Bing;ZHANG Peng-feng;GUO Kun

..............page:447-450

Experiments on high frequency pulse detonation rocket engine
CHEN Wei;FAN Wei;LI Jian-ling;WANG Ke;YAN Chuan-jun

..............page:443-446

Linear modeling of aero engines based on equilibrium manifold model
ZHAO Hui;NIU Jun;JIANG Yun-feng;YU Da-ren

..............page:377-382

Flow field structure and noise for different nozzles
WANG Xing;ZHENG Liu;ZHOU Yue-rong;CHEN Zhi-min

..............page:365-369

Design of a numeric simulation platform for integrated turbo-shaft engine/helicopter control system
ZHANG Hai-bo;YAO Wen-tong;CHEN Guo-qiang

..............page:383-390

Numerical simulation and SEM study on the microstructural damage of composite solid propellants
LIU Zhu-qing;LI Gao-chun;XING Yao-guo;DONG Ke-hai;CHEN Xiao-ming

..............page:412-416

Flight-envelope optimization partition for aeroengines control
HU Wei-hong;LI Shu-qing;SUN Jian-guo

..............page:391-395

Numerical analysis on vortex acoustic coupling characteristics in solid rocket motors
ZHANG Qiao;LI Jun-wei;WANG Wei-chen;SU Wan-xing;WANG Ning-fei

..............page:348-354

Pattern recognition and on-line detection for compressor surge
LI Chang-zheng;HAN Wei;XIONG Bing

..............page:318-322

Numerical simulation of installed performance for parallel turbo-ramjet combined cycle engine
WANG Yong-sheng;WANG Zhan-xue;LIU Zeng-wen;MA Hui-min

..............page:312-317,322

Numerical investigation of the stator hub gap effects on aerodynamic performance of a high-pressure compressor
ZUO Zhi-tao;ZHU Yang-li;ZHANG Dong-yang;TAN Chun-qing

..............page:329-333,338

Regulation experiment on the discharge chamber of electron cyclotron resonance ion thruster
MENG Zhi-qiang;YANG Juan;XU Ying-qiao;LI Peng-fei

..............page:421-424

Simulated altitude experimental investigation for N2O monopropellant micro-thruster
LI Mao;HAN Yue;FANG Jie;SUN Wei;CAI Guo-biao

..............page:307-311

Effects of chamber wall shape on high-pressure gas jet expansion stability in bulk-loaded liquid
MANG Shan-shan;YU Yong-gang

..............page:334-338

Influence of the swirl injection for secondary combustion of boron based ducted rocket
LIU Jie;LI Jin-xian;FENG Xi-ping;ZHENG Ya

..............page:355-359,382

A fault diagnosis method for aero-engine vibration based on fuzzy information entropy
AI Yan-ting;FEI Cheng-wei;WANG Zhi

..............page:407-411

Three-dimensional fuzzy control for turbofan engine based on genetic algorithm optimization
ZHANG Shi-ying;HU Yu;YU Xi-xing;ZHU Jie-tang

..............page:396-400

Experimental study on characteristics of bubble growth and pressure wave propagation by supersonic gas jets under water
TANG Long-sheng;LIU Yu;WU Zhi-feng;ZHAO Wen-sheng

..............page:417-420

Effects of endwall boundary layer suction position on the flow field and load in a high-turning compressor cascade
GUO Shuang;CHEN Fu;LU Hua-wei;CHEN Shao-wen;SONG Yu-fei;SONG Yan-ping;WANG Zhong-qi

..............page:323-328

Ignition algorithm of solid propellant micro-thruster array for orbit control
LIU Xu-hui;FANG Shu-zhou;WANG Yu-lin;LI Hong-mei

..............page:301-306

Numerical investigation of two-phase detonation with the osbstacles
MA Dan-hua;WENG Chun-sheng

..............page:425-430

Numerical calculation on behavior of fuel regression in hybrid rocket motor
SHAN Fan-li;HOU Ling-yun;PIAO Ying

..............page:360-364,406

Heat transfer analysis for a GOX/CH4 vortex cold-wall combustor
SUN De-chuan;YANG Jian-wen;BAI Rong-bo

..............page:401-406

Numerical study of distributor type diffuser performance for combustor
WANG Rong-juan;SUO Jian-qin;LIANG Hong-xia;WANG Tao

..............page:343-347

Numerical study for the thrust-vectoring characteristic of dual synthetic jets with unsymmetrical cavities
WANG Lin;LUO Zhen-bing;LIU Bing;XIA Zhi-xun;WANG De-quan

..............page:370-376

Detailed structure and propagating mechanism research on continuous rotating detonation wave
LIU Shi-jie;QIN Hui;LIN Zhi-yong;SUN Ming-bo;LIU Wei-dong

..............page:431-436

An optimal study on a TVC evaporation tube using moving particle semi-implicit method
XING Fei;ZHANG Shuai;ZHENG Yao

..............page:339-342