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Gas Turbine Experiment and Research
1672-2620
2010 Issue 1
Research on Aircraft Engine Inlet Pressure Compound Control in Altitude Simulation Test
zhao yong ; hou min jie ; huang zhen nan ; zhang song ; peng ju
..............page:37-41
Design and Experimental Investigation of Low Pressure Compressor for Civil Aeroplane
yu hua wei ; cheng rong hui ; xia lian
..............page:1-8
Measurement of the Tip Clearance Flow in a Small Axial Compressor Rotor
wan qian jun ; shi xiao jiang ; li hao ; chen hong min
..............page:22-25
Numerical Analyses for the Performance of Straight Labyrinth Seal of Aircraft Engine
zhao hai gang ; liu zhen xia
..............page:26-30
Effect of Air Injection on Aerodynamic Performance of a Highly-loaded Compressor Cascade at Different Incidences
feng dong min ; chen fu ; chen huan long ; wang zhong qi
..............page:9-14
Aerodynamic Design of a Round to Rectangle Air Meter in the Simulated Altitude Test Facility
zhuang huan ; guo zuo ; ma qian rong
..............page:59-62
Numerical Simulation of Two-phase Flow inside the Oil-gas Separator of Aero-engine
jia chun qiang ; xu rang shu ; ma qian rong
..............page:47-50,14
Design and Application of Closed-loop Simulation Tester for Turbine Power Unit
jiang qun ; wang dao bo ; li meng
..............page:55-58
xin chun xian ci
guo zuo
..............page:封2
Study of Icing Effect on Airfoil Flow-field
wang zhi guo ; yang jun ; lou de cang
..............page:31-36
Study of Airfoil Pressure Measurement Technology
fan jia feng ; huang ming jing ; zhong min ; tang lei ; wu chen
..............page:51-54,41
Effect of Incidence Angle on Unsteady Flow of Oscillating Turbine Blades
zhang zheng qiu ; zou zheng ping ; wang yan rong ; liu huo xing
..............page:15-21
NEWS & EVENTS
..............page:21,36