Journal of Aerospace Power 2008 Issue 6 State parameter image identification method based on fuzzy mathematical morphology and immune intelligence for rotating machinery

State parameter image identification method based on fuzzy mathematical morphology and immune intelligence for rotating machinery
DOU Wei;LIU Zhan-sheng;WANG Zheng-xian;HE Peng

..............page:1151-1160

hang kong dong li xue bao zheng gao jian ze

..............page:封3

Computation of nozzle two-phase flow in a N2O/HTPB hybrid rocket motor
TIAN Hui;CAI Guo-biao;SUN Zai-yong

..............page:1146-1150

Investigations of the bleed air anti-icing system for an aircraft wing
CHANG Shi-nan;YUAN Mei-ming;HUO Xi-heng;ZHANG Quan

..............page:1141-1145

Cold flow research in scramjet combustor
WANG Dian;SONG Wen-yan;LI Jian-ping;CAI Yuan-hu

..............page:1135-1140

Automatic code generation technology for control method based on RTWEC
LU Jun;GUO Ying-qing;WANG Bin-zheng

..............page:1131-1134

Quasi-3D simulation of aero engine full flow field
YU Long-jiang;CHEN Mei-ning;PIAO Ying

..............page:1008-1013

Numerical simulation of shock wave/flat-plate turbulent boundary-layer interaction
LI Zhi-qiang;LI Zheng-qiang;YAN Wen-hui

..............page:1003-1007

Critical starting characteristics of hypersonic inlets
WANG Cheng-peng;CHENG Ke-ming

..............page:997-1002

Pollutant emission and development of low-emission combustion technology for civil aero engine
ZHAO Jian-xing

..............page:986-996

Significant impact of engine technical innovation on airplane performance advancement
CHEN Da-guang

..............page:981-985

Fan/compressor aero design trend and challenge on the development of high bypass ratio turbofan
CHEN Mao-zhang;LIU Bao-jie

..............page:961-975

Summarization of development status and key technologies for large airplane engines
LIU Da-xiang;JIN Jie;PENG You-mei;HU Xiao-yu

..............page:976-980

Extracting algorithm for diagnostic parameters of aero-engine based on fuzzy-rough sets
SONG Yun-xue;ZHANG Chuan-chao;SHI Yong-sheng

..............page:1127-1130

Fault diagnosis and adaptive reconfiguration control for sensors in aeroengine based on improved least squares support vector machine
CAI Kai-long;XIE Shou-sheng;YANG Wei;WU Yong

..............page:1118-1126

Fault diagnosis for gas turbine engines based on Kalman filter and neural networks
YAO Hua;SHAN Gui-ping;SUN Jian-guo

..............page:1111-1117

Numerical analysis of the damage of bird impaction against composite laminates and the influence factors on absorbing energy
YU Lian-chao;CHEN Wei;GUAN Yu-pu;WEN Hai-tao

..............page:1106-1110

Conservative fuzzy reliability design of engine connecting rod
WANG Tie;WU Jing;ZHOU Shu-wen;ZHANG Guo-zhong;BA De-chun

..............page:1102-1105

Blade wake excitation caused by twin-shaft engine speed difference
ZHAO Fu-xing;SHI Hai-qiu;YANG Xing-yu

..............page:1098-1101

Improved fault diagnosis method for aero engine rotor-sator rubs
HE Tian;LIU Xian-dong;LI Qi-han

..............page:1093-1097

Influence of magnetic damper on dynamic characteristics of magnetic bearing system
XIE Zhen-yu;LI Ke-lei;ZHAO Qing-quan;HUANG Pei-zhen

..............page:1087-1092

Way to evaluate fatigue life of fillet weld of plate with flange based on stress field intensity
GUO Hai-ding;WU Qi

..............page:1082-1086

Effect of slot width on the aerodynamic performance of compressor cascade
ZHOU Min;WANG Ru-gen;ZENG Ling-jun;ZHAO Ying-wu

..............page:1077-1081

Improved streamline curvature throughflow method and its application in a bypass compression system design
SHAO Fu-yong;YANG Jin-guang;LIU Zhen-de;HU Jun

..............page:1072-1076

Role of tip leakage flow on flow instability and its control with circumferential groove casing treatment
WANG Pei;ZHU Jun-qiang;HUANG Wei-guang

..............page:1067-1071

Experiment and design improvement of an axial flow blood pump
ZHAN Zhao;ZHANG Yan;GUI Xing-min

..............page:1061-1066

Numerical research of two-dimensional flow-path in ram-rotor
HAN Jiang;YAN Hong-ming;ZHONG Jing-jun;SUN Peng;YU Yang

..............page:1054-1060

Modification design and flowfield analysis of a centrifugal turbine stage with discrete nozzles
LIU Jing;SHAN Peng

..............page:1047-1053

Numerical study on combination flow field of axisymmetric convergent-divergent nozzle under transonic and supersonic conditions
HU Hai-yang;WANG Qiang

..............page:1041-1046

Uncertainty of quality being produced in the course of manufacture management of aerospace power system
MAO Jing-li

..............page:1031-1040

Influence of magnetic plasma on performances of the convergent nozzle
ZHANG Yan;HUANG Hu-lin

..............page:1024-1030

Aerodynamic optimization of transonic cascade using global aerodynamic optimization method
SONG Li-ming;LUO Chang;LI Jun;FENG Zhen-ping

..............page:1019-1023

Experimental investigation on the starting characteristics of a hypersonic inlet with moving entrance door
WANG Yi;FAN Xiao-qiang;LIANG Jian-han;LIU Wei-dong;WANG Zhen-guo

..............page:1014-1018