Aeroengine 2012 Issue 4 Influence of Fuel-staging Ratio on TAPS Combustor Performance

Journals A B C D E F G H I J K L M N O P Q R S T U V W X Y Z

Aeroengine
1672-3147
2012 Issue 4

Influence of Fuel-staging Ratio on TAPS Combustor Performance
cheng ming ; shang shou tang ; liu dian chun ; gao jia chun ; guo rui qing ; zhang shan shan ; li feng

..............page:6-10

..............page:11-16

Influence of Primary Zone Outlet Feature on Combustor Outlet Temperature Field
ding guo yu ; he xiao min ; jin yi ; wu ze jun ; ge jia wei

..............page:17-21

..............page:22-27

..............page:38-41

..............page:28-30,41

Component-Level Modeling and Analysis of Aeroengine Based on Matlab/Simulink
xia chao ; wang ji qiang ; shang guo jun ; zhou zuo

..............page:31-33,52

Effect of Total Pressure Distortion on Aeroengine Stability
hao bi si ga la tu ; zhou sheng tian ; zhang zhi shu ; hu jun

..............page:34-37,46

..............page:42-46

Supersonic Turbine Rotor Blade Design Method
liu yang ; zhong yi cheng ; hui guang zuo ; xu wei zu

..............page:47-52

..............page:53-58

..............page:59-62

..............page:F0003-F0003

..............page:F0002-F0002

Integrated Design System of Aeroengine Combustors
yan hong ; yan chuan jun

..............page:1-5