Aeroengine 2003 Issue 2 hang kong fa dong ji bai nian fa zhan lue ying ( er )

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Aeroengine
1672-3147
2003 Issue 2

hang kong fa dong ji bai nian fa zhan lue ying ( er )

..............page:封三

shen yang fa dong ji she ji yan jiu suo fu zong she ji shi li wen ming

..............page:封二

ihptet ji hua xin ji shu de kai fa he yan zheng de jin zhan

..............page:58

ihptet ji hua xin ji shu de zui xin yi zhi

..............page:54

ej200 fa dong ji de san huan ding xiang tui li shi liang pen guan

..............page:28

ej200 fa dong ji wei lai de quan zheng ti ye pan jie gou ya qi ji

..............page:24

ej200 fa dong ji ji qi fa zhan

..............page:4

A Century of Aircraft Power Plant in Retrospect(2)
ji he ming

..............page:55-58

Summary of Model Reference Adaptive Control of Aeroengine
pan mu xuan ; huang jin quan

..............page:51-54

Application of AMB Part Two: Fundamentals and Design of Active Magnetic Bearing in Aeroengine
chang chun jiang ; yang rong

..............page:44-50

Analysis of Noise Spectrum and Identification of Acoustic Excitation Sources in Annular Combustion Chamber of Aeroengine
sheng yuan sheng ; wang ke ming ; wu xiao ming

..............page:38-43

New Material for Aeroengine-16Cr3NiWMoVNbE Gear Steel
zuo bai qiu ; chang chun jiang

..............page:34-37

Characteristic and Calculation of Eddy Scale in Total Pressure Distortion Flow at Typical Engine Inlet
wang qin ; liu shi guan ; wang zhen hua

..............page:29-33

Integral H∞ Robust Servo Control of Turbojet Engine
wang zuo ; liu de hong

..............page:25-28

Analysis of Typical Turbofan Engine Surge in Ground Bed Test
zhang zhi shu ; li yong fan ; chen jin guo

..............page:21-24

Troublshooting for Cone Gear Spoke Fracture in Typical Turbofan
li fu yi ; liao xue jun ; cai xian xin

..............page:16-20

The Effect of Defects, Damage and Micro Crack on Total Life and Reliability of Aeroengine Components in Service
xu zuo jun

..............page:11-15

Application of Short Time Fourier Transform to LP Compressor Aerodynamic Unstability Analysis
liu shi guan ; wang qin ; yang xue guang

..............page:8-10

Design of a New Main Fuel Pump for Aeroengine
liu shang qin ; wang lei

..............page:5-7

Recent Progress of IHPTET--The Role of Pervasive Technology and Demonstrator in Aircraft Engine Development
wu da guan

..............page:1-4