Journal of Propulsion Technology 2007 Issue 1 Web-based integrated design platform for solid rocket motor

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Journal of Propulsion Technology
1001-4055
2007 Issue 1

Web-based integrated design platform for solid rocket motor
XIE Hong-yu;ZHANG Wei-hua;WANG Zhong-wei;LI Xiao-bin

..............page:108-112

Nonlinear dynamic analysis of viscoelastic panel flutter
ZHANG Yun-feng;LIU Zhan-sheng

..............page:103-107

Experimental analysis on cycle processes of two-phase valveless pulse detonation engine
LI Mu;YAN Chuan-jun;WANG Zhi-wu;QIU Hua

..............page:97-102

An adaptive control for a class of nonlinear systems and application to aeroengine control
ZHA Xu;GUO Fa-tao

..............page:92-96

Sensor fault diagnosis for aircraft engine based on artificial immune networks
HOU Sheng-li;LI Ying-hong;LI Ming-kui;WEI Xun-kai

..............page:86-91

Selection of design parameters for streamtraced hypersonic Busemann inlets
SUN Bo;ZHANG Kun-yuan;JIN Zhi-guang;WANG Cheng-peng

..............page:55-59

Effects of side-inlet location on the performance of boron-based propellant ducted rocket
HU Jian-xin;XIA Zhi-xun;FANG Ding-you;GUO Jian;ZHANG Wei;JIANG Chun-lin

..............page:50-54

Multi-disciplinary feasible decoupling in multidisciplinary design optimization for turbine blade
WANG Jing-chao;LI Li-zhou;YUE Zhu-feng

..............page:45-49

Analysis for technique challenges on counter-rotating turbomachinery
JI Lu-cheng

..............page:40-44

Effect of bowed blades on the separation structures in high-turning compressor cascades
ZHANG Hua-liang;WANG Song-tao;WANG Zhong-qi

..............page:36-39,54

Numerical analysis for the unsteady flow and casing treatment in a low speed centrifugal compressor
GAO Peng;CHU Wu-li;YANG Yong

..............page:32-35

Experimental investigation on catalytic ignition of N2O hybrid rocket motor
WAN Ke;LI Lu-ming;Vadim ZAKIROV;HUO Xue-liang

..............page:1-3,85

Aeroengine fault diagnoisis based on one-class classification and wavlet-fractal
LUO Jun;HE Li-ming;CHEN Chao

..............page:82-85

Thrust vector control for solid plug nozzle based on secondary injection
JU Chun-guang;LIU Yu;LIAO Yun-fei

..............page:78-81

Tests on GH2/GO2 model engine with aerospike nozzle
WANG Chang-hui;LIU Yu;WANG Yi-bai;LIAO Yun-fei

..............page:73-77

Effects of geometry design on micro nozzle's performance
YANG Hai-wei;ZHAO Yang

..............page:68-72

Calculation and comparison of forward/backward swept sidewall compression scramjet inlets
LI Hua;JIA Di;FAN Xiao-qiang;LI Xiao-yu

..............page:65-67,91

Experimental investigation on starting process of hypersonic inlet in gun tunnel
FAN Xiao-qiang;JIA Di;FENG Ding-hua;LI Hua

..............page:60-64

Application of high-turning bowed compressor stator for redesign of a highly loaded fan stage
LI Shao-bin;SU Jie-xian;WANG Zhong-qi

..............page:26-31

Aerodynamic stability assessment for compression component running in turbofan engine with distorted flow
WANG Zhan-xue;WANG Peng;QIAO Wei-yang

..............page:20-25

Experimental studies for the aerodynamic loss in gas turbine with film cooling
QIAO Wei-yang;ZENG Jun;ZENG Wen-yan;HUANG Kang-cai;SUN Da-wei;ZHANG Man

..............page:14-19

Development of Kalman filter and genetic algorithm for aero-engine performance diagnostics
YUAN Chun-fei;YAO Hua

..............page:9-13

Numerical study for end-burning solid motor embedded with wire
ZHANG You-wei;WANG Xiao-hong;YANG Ju-xian

..............page:4-8