1672-3147
2002 Issue 3
..............page:封三
..............page:封二
Development of Spherical Convergent Flap Nozzle
liang chun hua ; jin bao lin ; li yu tong
liang chun hua ; jin bao lin ; li yu tong
..............page:55-58
..............page:52-54,58
CISA 3D Navier-Stokes Code Calibration and Application in Compressor
gao shan ; jiang hao xing
gao shan ; jiang hao xing
..............page:47-51,46
Calculation of Additive Drag of Supersonic Inlet under Subcritical Operating Condition
zhou jian hua ; dong jin zhong ; huang xi jun ; li xin
zhou jian hua ; dong jin zhong ; huang xi jun ; li xin
..............page:42-46
..............page:37-41
Control and Prediction of NOx Formation in Aircraft Gas Turbine Engine Combustor
hu yi ; zhang bao cheng
hu yi ; zhang bao cheng
..............page:30-36
Operational Reliability Analysis of Typical Engine Starter
yan cheng hong ; bo ji xing
yan cheng hong ; bo ji xing
..............page:27-29
The Structure Failure Analysis of Centrifugal Ventilator Shell
ke cheng he ; dong ben han ; gao peng fei ; huo cheng min ; liao lian fang
ke cheng he ; dong ben han ; gao peng fei ; huo cheng min ; liao lian fang
..............page:21-26
Prediction of Low Cycle Fatigue Life for Turbine Disc by Small Sample——Webayes Method
song zhao zuo ; fu xiao ping ; wu shu xiong
song zhao zuo ; fu xiao ping ; wu shu xiong
..............page:18-20
A Computational Method for Surge Caused Transverse Load in Engine Rotor
feng guo quan ; zhu zuo gen
feng guo quan ; zhu zuo gen
..............page:13-17
Application of Bonded Strain Gauge to External Engine Piping Vibrational Measurement
hao bing ; li cheng gang ; wang hao
hao bing ; li cheng gang ; wang hao
..............page:9-12
A Gas Turbine 3D Design System Capable of Analyzing Flow Field Structure in Bowed-Twist-Sweep Blade Cascade
feng guo tai ; gu zhong hua ; wang song tao
feng guo tai ; gu zhong hua ; wang song tao
..............page:5-8,4
..............page:1-4