1672-3147
2002 Issue 2
..............page:封三
..............page:封二
..............page:56-56
..............page:26-26
..............page:57-58
Review on Multiphysics Coupling Analysis in Turbomachinery Design
li hai bin ; feng guo tai
li hai bin ; feng guo tai
..............page:51-56
..............page:46-50
..............page:43-45,58
A Centre Ejector with Backflow
yin qun ; shen zhen hua
yin qun ; shen zhen hua
..............page:12-13
Measurements of Dynamic Total Pressure Distortion for Engine Inlet and Analysis of Effective Factors
wang qin ; liu shi guan ; li cheng hui ; wang zhen hua
wang qin ; liu shi guan ; li cheng hui ; wang zhen hua
..............page:6-11
Stability Analysis of Experimental AMB Prototype for Aircraft Engine
zhang gang ; wang xi ping
zhang gang ; wang xi ping
..............page:1-5
Servo Tracking Control of Turbojet Engine
wang zuo ; liu de hong
wang zuo ; liu de hong
..............page:39-42
Improvement of Bearing Bush Fixture in Accessory Gearbox for a Typical Engine
wang xiao wei ; zhao zong jian ; zhang xiang dong
wang xiao wei ; zhao zong jian ; zhang xiang dong
..............page:35-38
Fatigue - Fracture Mechanism of Main Bearing Cage for Aircraft Engine
xing chang xi ; sun min
xing chang xi ; sun min
..............page:32-34
New Technique for Eliminating Fault of Tenon of Fan Blade with Mid-Span Shroud
li hong xin ; huang zhi jian ; zhang li ; yu shuang xi
li hong xin ; huang zhi jian ; zhang li ; yu shuang xi
..............page:27-31
..............page:22-26
Talking about the Way to Increase Aeroengine Reliability
zhang lian xiang
zhang lian xiang
..............page:17-21
Comprehensive Analysis of Low Pressure Condition Established with Ejection or Compressor Extraction for Afterburner Nozzle
xiao xin ying ; zhao zuo
xiao xin ying ; zhao zuo
..............page:14-16,31