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Aeroengine
1672-3147
2008 Issue 3
Investigation of General Structure and Mode Transition Mechanism of Variable Cycle Engine
LIU Hong-bo;WANG Rong-qiao
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page:1-5
Application of 502 Glue in Room Temperature Strain Electrical Measurement
HAO Bing;LI Cheng-gang;WANG De-you
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page:6-7,11
Investigation of Test Process Management System for Aeroengine Test
CHEN Zhen-yu;GE Zhi-mei;QIAO Li;DU Jian-hong
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page:8-11
Application of Distributed Network Technology in Gas Turbine Performance Test System
MEI Fan;LIU Guo-ku;WANG Shu-yun
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page:12-14
Fatigue Test of an Aeroengine compressor IGVs
WAN Li;LI Shun-ming;JIN Ye-zhuang
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page:15-17
Life prediction Model of Operating State for Aeroengine Main Bearing
HONG Jie;MIAO Xue-wen;MA Yan-hong
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page:18-21
Investigation of Rotor Blade Technology Life for a Series of Aeroengine Compressor
GAO Qing
..............
page:22-26
θ Mapping Model of High Temperature Creep of Nickel- Base Single Crystal Alloy
SHI Duo-qi;YANG Xiao-guang;YE Zheng;BAI Lu
..............
page:27-30,5
Repaire Method of Blade Tip Crack for an Engine High Pressure Turbine
LIU Jun-he;TANG Xiao-hui;WANG Ke-liang
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page:31-34,26
Numerical Simulation of Combustion Flow Field of Supersonic Combustor with Cavity
YANG Shi-min;TANG Hao;HUANG Yue
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page:35-38
Experimental Investigation of Fuel Nozzle Operational Characteristics for a Heavy Gas Turbine
ZHAI Wei-kuo;ZHANG Bao-cheng;LIU Kai;MA Hong-an
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page:39-41,45
Effect of CFM56 -3 Engine Variable Geometry Control System on Aerongine Performance
XIA Cun-jiang
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page:42-45
Investigation of Micro-Turbojet Engine Control Algorithm
SHI Wei;HAN Shu-jun;DING Shui-ting
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page:46-48
Fault Diagnosis Approach of Performance for Civil Aeroengine
SHI Xiu-yu
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page:49-51
Development of Thermal Barrier Coating for Foreign Turbofan Engine Turbine Blade
XU Qing-ze;LIANG Chun-hua;SUN Guang-hua;WANG Zhi-hong
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page:52-56
Superiority of Aircraft Infrared Stealth on Turbofan Engine
ZHANG Dong-mei;ZHU Chun-ting;CAO Wen-jie;ZHAO Sheng-hong
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page:57-58