1001-4055
2005 Issue 2
Investigation of vaporized kerosene injection in a supersonic model combustor
YU Gang;LI Jian-guo;ZHAO Zhen;WANG Dong
YU Gang;LI Jian-guo;ZHAO Zhen;WANG Dong
..............page:97-100
Combustion flow of kerosene-fueled scramjet with 3D cavity (Ⅲ) Multi-step chemistry characteristics of kerosene
HUANG Sheng-hong;XU Sheng-li;LIU Xiao-yong
HUANG Sheng-hong;XU Sheng-li;LIU Xiao-yong
..............page:101-105
Numerical study on chemical reactive jet interaction flows in the two-dimensional transitional regime by DSMC/EPSM method
LI Jie;CHEN Wei-fang;REN Bing
LI Jie;CHEN Wei-fang;REN Bing
..............page:106-110
Three dimension numerical simulation of heat transfer in regeneratively cooled nozzle
LI Jun-wei;LIU Yu
LI Jun-wei;LIU Yu
..............page:111-115
Temperature drop analysis on the monopropellant thruster in the vacuum cryogenic environment
XIAO Ze-juan;LI Peng;CHENG Hui-er;ZHOU Hong-ling;HUANG Rui-sheng
XIAO Ze-juan;LI Peng;CHENG Hui-er;ZHOU Hong-ling;HUANG Rui-sheng
..............page:116-119
Observation of transient interaction of lateral impulse jet
XU Min;CHEN Gang;CHEN Zhi-min;CHEN Shi-lu
XU Min;CHEN Gang;CHEN Zhi-min;CHEN Shi-lu
..............page:120-124
Effects of Reynolds number on control schedule and performance of HALE engine
TU Qiu-ye;CHEN Yu-chun;SU San-mai;SHANG Xu-sheng
TU Qiu-ye;CHEN Yu-chun;SU San-mai;SHANG Xu-sheng
..............page:125-128
Experimental investigation on aerodynamic instability of axial flow engine
ZHANG Pu;LI Ying-hong;WEI Xun-kai;WU Yun
ZHANG Pu;LI Ying-hong;WEI Xun-kai;WU Yun
..............page:129-133
Computation and assessment of aerodynamic stability of turbofan engine for missile
WANG Zhan-xue;QIAO Wei-yang;LI Wen-lan
WANG Zhan-xue;QIAO Wei-yang;LI Wen-lan
..............page:134-138
Analysis of secondary vortex in a 2-D typical scramjet inlet
LIANG De-wang;LI Bo
LIANG De-wang;LI Bo
..............page:139-143
Experimental investigation of static internal performance for an axisymmetric vectoring thrust nozzle
JIN Jie;ZHAO Jing-yun;ZHANG Ming-heng;LAI Chuan-xing
JIN Jie;ZHAO Jing-yun;ZHANG Ming-heng;LAI Chuan-xing
..............page:144-146
Investigation of a general module simulation method for liquid propellant rocket engines
WEI Peng-fei;WU Jian-jun;LIU Hong-gang;CHEN Qi-zhi
WEI Peng-fei;WU Jian-jun;LIU Hong-gang;CHEN Qi-zhi
..............page:147-150
Numerical simulation of redesigned turbine matching in turbojet engine
HUANG Jia-hua;FENG Guo-tai;YU Ting-chen;ZHOU Chi
HUANG Jia-hua;FENG Guo-tai;YU Ting-chen;ZHOU Chi
..............page:151-154,183
Method to identify the multimode linear model of aeroengine based on nonlinear response
SONG Zhi-ping;HAN Chong-zhao;WEI Rui-xuan
SONG Zhi-ping;HAN Chong-zhao;WEI Rui-xuan
..............page:155-157
Robust controller design and experiment of turbofan
BAO Wen;CHANG Jun-tao;MA Zhao-xiang;YU Da-ren
BAO Wen;CHANG Jun-tao;MA Zhao-xiang;YU Da-ren
..............page:158-161
Turbojet modeling and simulation in wind milling based on ANFIS
WU Zhi-wen;YU Da-ren;NIU Jun;GUO Yu-feng
WU Zhi-wen;YU Da-ren;NIU Jun;GUO Yu-feng
..............page:162-166
Simulation test of natural circulation precooling for cryogenic pump system
LI Qi-fen;CHEN Guo-bang;XIE Xue-mei;ZHONG Yi-kui;ZHENG Xi-liang;BAO Rui
LI Qi-fen;CHEN Guo-bang;XIE Xue-mei;ZHONG Yi-kui;ZHENG Xi-liang;BAO Rui
..............page:167-173
Analysis of damping characteristics of squeeze film damper with metal rubber
JIANG Hong-yuan;ZHANG Rui-hua;ZHAO Ke-ding;Novikov D K
JIANG Hong-yuan;ZHANG Rui-hua;ZHAO Ke-ding;Novikov D K
..............page:174-177
Investigation on combustion mechanism of fuel-rich propellant based on boron
WANG Ying-hong;LI Bao-xuan;LI Jin-xian;LIU Hong-cheng;XIAO Xiu-you
WANG Ying-hong;LI Bao-xuan;LI Jin-xian;LIU Hong-cheng;XIAO Xiu-you
..............page:178-183
Study on dispersion of nano-aluminum powder in kerosene
LIU Xiang-cui;ZHU Hui;ZHANG Wei;WANG Chun-hua
LIU Xiang-cui;ZHU Hui;ZHANG Wei;WANG Chun-hua
..............page:184-187
Geometrical design and tool-path generation of three dimensional impeller
CAO Li-xin;SU Yun-ling;JIN Yu-shu
CAO Li-xin;SU Yun-ling;JIN Yu-shu
..............page:188-192
..............page:100