Aeroengine 2007 Issue 2 yuan shi feng cai

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Aeroengine
1672-3147
2007 Issue 2

yuan shi feng cai

..............page:封2

Advanced Technology Program on High Bypass Ratio Turbofan Engine in EU
Liang Chunhua

..............page:57-58,48

Management Structure of Scientific and Technical Research under the Frame of Integrated Information and Archive
Zhao Junwu;Qian Xiaofeng

..............page:53-56

Dynamic Hybrid RANS/LES simulation of supersonic flow over back-facing step
Huang Ran;Sun Mingbo;Liu Weidong

..............page:49-52,34

Application of Elman Neural Network in Aeroengine Fault Diagnosis
Peng Jingbo;Xie Shousheng

..............page:46-48

Design of Aeroengine Hydraulic System Actuator Based on UG Software
Wang Yan;Qu Shan;Luan Dong

..............page:44-45,43

Application of Symbolic Operation Method in Dynamic Modeling of Twin-Spool Turbojet
Wang Hua;Wang Xi

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

Effects of Weapon Launch on an Aeroengine Operation
Liu Jianjun

..............page:35-37,4

Analysis and Modeling for Cruise Missile Engine Integrated Controller Based on Analog Circuit
Zhang Shiying;Li Renbing

..............page:31-34

Analysis of Test Data Difference for Similar Domestic and Foreign Combustor Facility
Yang Zhimin;Huang Weibing;Zhao Yu;Wang Keliang

..............page:27-30

Relationship of Elastic Constants between DS and Corresponding SC Material
Guo Li;Wang Yanrong

..............page:22-26

Effects of Friction Damper Parameters on Blade Vibration Response
Hao Yanping;Zhu Zigen

..............page:18-21

Design of Automatic Instrumentation System of Aeroengine Test Bench
Du Jianhong;Qiao li

..............page:15-17

Automatic Temperature Interpretation and Digital Image Processing Systems of Temperature-Sensitive Paints
Ma Chunwu;Jiang Bin;Chen Fuyang

..............page:12-14,11

Test Methods on Thermal/Mechanical Fatigue(TMF) of Turbine Blade
Wang Hongbin

..............page:7-11

Design Improvement of Bleed Valve and Pipe for a Heavy Duty Gas Turbine
Liang Ruan;Li Shunming

..............page:5-6

Preliminary Investigation of Scramjet Engine Performance
Liu Xingzhou

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