Journal of Propulsion Technology 2007 Issue 2 Catalytic combustion properties of a new high burning rate propellant

Catalytic combustion properties of a new high burning rate propellant
GUO Xiao-de;LI Feng-sheng;SONG Hong-chang;LIU Guan-peng

..............page:220-224

Study on decreasing the burning rate of nitrate ester plasticized polyether propellant
GUAN Huan-xiang;LIU Yun-fei;YAO Wei-shang;TAN Hui-min

..............page:216-219

Control methods for supersonic jet screech tones
WANG Yang-hai;LI Xiao-dong

..............page:211-215

A PID neural network decoupling control of aeroengine
FU Qiang;FAN Ding

..............page:208-210

Analysis for internal drag in sidewall-compression inlet
LUO Xiao-chen;ZHANG Kun-yuan

..............page:204-207

A simulation method based on SIMULINK for a supersonic inlet
HE Bao-cheng;YAO Zhao-hui;BAO Wen;CHANG Jun-tao

..............page:199-203

Identification of aero-engines model based on T-S fuzzy model
CAI Kai-long;XIE Shou-sheng;WU Yong

..............page:194-198

Calculation and analysis of pulse detonation engine flight performance
JIN Tao;HE Li-ming

..............page:190-193

Numerical computation of two phase flow combustion in the water ramjet
MIAO Wan-bo;XIA Zhi-xun;HU Jian-xin;ZHAO Jian-min;LUO Zhen-bing

..............page:186-189

Theoretical performance analysis of the powdered fuel ramjet
SHEN Hui-jun;XIA Zhi-xun;HU Jian-xin;MIAO Wan-bo

..............page:181-185

Multi-objective aerodynamic optimization design process of multistage axial turbine
ZHAO Hong-lei;YAN Pei-gang;HAN Wan-jin

..............page:176-180

Automated design optimization of single expansion ramp nozzle for hypersonic vehicle
HE Xu-zhao;ZHANG Yong;WANG Guang-yuan;NI Hong-li;LE Jia-ling

..............page:148-151,224

Effect of secondary flow injection on flow field and performance of nozzle
LIU Ai-hua;WANG Zhan-xue

..............page:144-147

Local heat transfer characteristics near film cooling holes on cooling side in film cooling
XU Lei;CHANG Hai-ping;MAO Jun-kui;ZHANG Jing-yang

..............page:141-143,203

Numerical studies on cavity flame holders for supersonic combustors
CHEN Fang;CHEN Li-hong;ZHANG Xin-yu

..............page:135-140

Three-dimensional numerical simulation of oblique detonation wave standing on an accelerating projectile
DAI Shu-Lan;XU Hou-Qian

..............page:132-134

Experimental investigation on combustion instability of liquid oxygen and methane flame
HONG Liu;Fusetti A;Rosa M D;Oschwald M

..............page:127-131,175

Numerical study of two-phase field and combustion performance in annual combustor with cylindrical heads
CAI Wen-xiang;ZHAO Jian-xing;ZHANG Jing-zhou

..............page:122-126

Numerical simulation for unsteady flow field induced by rocket engine jet and shield board
ZHOU Song-bai;GUO Zheng;GAO Song;LIU Jun

..............page:118-121

Numerical simulation of the initial stage flowfields for the stage separation of the multi-stage rocket
HUANG Si-yuan;QUAN Xiao-bo;GUO Feng-mei;FU Song

..............page:113-117

Aerodynamic performance study of curved compressor cascades with different camber angles
CHEN Shao-wen;CHEN Fu;WANG Ke-li;GU Jun;WANG Zhong-qi

..............page:170-175

Effects of uneven blade spacing on unsteady blade forcing in an axial compressor
ZHAO Yang-zheng;LIU Qian-zhi;LIAO Ming-fu

..............page:167-169,180

Experimental study on orifice depths effect for synthetic jet with Particle image Velocimetry
XU Jing-lei;SHA Jiang;LIN Chun-feng;LI Nian;ZHANG Kun-yuan

..............page:162-166

Optimum scheme for oblique shocks series of two-dimensional hypersonic compression surface
LI Jian;GU Liang-xian;GUO Xiao-zhi

..............page:157-161

Experiment on spectral infrared radiation characteristics of exhaust jet from 2D nozzle of turbofan engine
LUO Ming-dong;JI Hong-hu;HUANG Wei;CAI Xu;ZHANG Bo;GAO Chao

..............page:152-156