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Aeroengine
1672-3147
2009 Issue 1
Interview of Academician CAO Chun-xiao
..............page:7-10
Self-Excited Threshold Auto-Regressive Simulation Model of Aeroengine Combustor Acoustic Loading
WU Zhao-qi;GUAN Peng-lai;WU Xiao-ming
..............page:40-42
Performance Deterioration and Control of Military Turbofan Engine
CHEN Dai-fu;SONG Ying-jun
..............page:43-46
Application of CBR and Neural Network for Steady-State Model of Aeroengine
CAO Yang;FU Ye;LI Wen-feng;QIAO Li
..............page:47-49,10
Probability Analysis for Low Cycle Fatigue Life of Turbine Disk
ZHAO He-yang;BAI Guang-chen;WANG Ke
..............page:53-56
Application of MCrAlY+AlSiY Composite Coating for Aeroengine
PENG Xin;HOU Hui-wen;LIN Dong;LIU Jian-ping
..............page:57-59
Derivative Development of "Kunlun" Aeroengine
YAN Cheng-zhong
..............page:11-17
Structural Characteristics and Design of Serrated Shroud
LI Wen-ming
..............page:18-22
Numerical Calculation of Infrared Characteristics for Aeroengine Exhaust System
DENG Hong-wei;ZHOU Sheng-tian;SHAO Wan-ren;LIU You-hong
..............page:27-29,17
Calculation Method of Rotor Pump Resistance Moment for Aeroengine
TIAN Wen-zheng;LI Guo-quan
..............page:30-32
Experimental Investigation of Vibration Transmission for Propeller
QU Yu-chi;ZHANG Yong-feng;ZHAO Shu-yuan;SONG Wei-gang
..............page:33-36
Fault Diagnosis Technology for Aeroengine Based on Spectrum D-S Evidence Fusion
CUI Xiao-fei;ZHANG Gai-hu;JIANG Ke-yi;MA Li
..............page:37-39,56