1672-3147
2006 Issue 3
..............page:封3
..............page:封2
..............page:4,7,9,20,26,30,41
..............page:53-58
..............page:48-52
..............page:44-47
Microstructure Damage Analysis of an Aeroengine Combustor Liner
Li Ming;Xie Yujiang;Wang Dongsheng
Li Ming;Xie Yujiang;Wang Dongsheng
..............page:42-43,47
Application of Simulation Technology in Aeropropulsion Control System
Chen Yun;Zhang Tianhong
Chen Yun;Zhang Tianhong
..............page:39-41
Performance Analysis and Calculation of an Aeroengine Screw Centrifugal Pump
He Haiqiang;Guo Yingqing;Liu Xueying;Xia Zongji
He Haiqiang;Guo Yingqing;Liu Xueying;Xia Zongji
..............page:36-38,52
Lubrication Temperature Calculation of the Oil Outlet for Accessory Gearbox Based on ANSYS
Wu Hong;Li Guoquan;Qi Lehua
Wu Hong;Li Guoquan;Qi Lehua
..............page:31-35
Effect of Nozzle and Swirler Number on Short Annular Combustor Performance
Zou Baohua;Hu Chunbo;Zhang Bailing
Zou Baohua;Hu Chunbo;Zhang Bailing
..............page:27-30
Performance Advantages of Annular Ejector
Li Dehai;Xiao Xinying
Li Dehai;Xiao Xinying
..............page:25-26
Conversion of Typical Turbine Component Dimensions in Cold and Hot States
Niu Dongsheng;Chen Wei
Niu Dongsheng;Chen Wei
..............page:21-24
Numerical Simulation of 3D Flow Field in Turbine Stages and Nozzle of a Gas Turbine Starter
Yao Siwei;Ge Ning
Yao Siwei;Ge Ning
..............page:17-20
A Blade/Vane Twisting Method to Increase the Partial Speed Performance of Multistage Axial Flow Compressor
Hao Shucheng
Hao Shucheng
..............page:14-16
..............page:10-13
Interview of Wen Xueyou
li hua wen
li hua wen
..............page:8-9
Interview of Ma Hengru
li hua wen
li hua wen
..............page:5-7
..............page:1-4