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Gas Turbine Experiment and Research
1672-2620
2013 Issue 4
Failure Analysis on Adjustable Parameter Deviation of Aero- Engine′s Compressor Inlet Guide Vane Angle
FAN Shi-xin;HUANG Meng;ZHENG Ming
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page:48-50
An Overview of Aero- Engine Aerodynamics Overseas Research
LIU Xiao-bo;SUN Zong-xiang;ZHONG Ping;CHEN Li-yan
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page:58-62
Numerical Simulation of Two- Phase Combustion Fields in a Model Combustor Using Two Different Chemical Reaction Mechanisms of Jet Fuel
WANG Hui-ru;JIN Jie
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page:22-27
Fatigue Life Prediction Model for Nickel- Based Directionally Solidified Superalloy Considered Complex Loading and Orientation
LIU Jin-long;YANG Xiao-guang;SHI Duo-qi
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page:44-47
Innovative Blading Method Based on Calculating Geometry
AN Li-ping;HUANG Ping
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page:8-12,17
Experiment on Tip Flow Property of High Speed Axial Flow Compressor
AO Yong-ping;SHAN Zhi-chao;HE Yi-na;XIONG Bing;FAN Jia-feng
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page:13-17
Measuring Methods of Aero- Engine Inlet Airflow
LI Bing;HAO Xiao-le;SHEN Shi-cai
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page:54-57
Instability Signal Detecting and Early Warning of Aero- Engine
WANG Ke-hong;TANG Shi-jan;QU Wei-dong
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page:51-53,7
Numerical Simulation of Reinforced TMC Properties under Transverse Tensility
LI Guan-da;ZHANG Shao-ping;PEI Hui-ping;AN Li-ping;LIU Xue-wei
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page:37-43
Experimental Investigation of the Sound Generated from the Compressor Blade Airflow
YIN Hong-shun;WANG Yong-ming;YU Hua-wei;JIANG Zheng-li
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page:1-7
Design and Optimization of Low Inertia Turbine Rotor Structure
ZHANG Cheng-qi;HUANG Wen-zhou;LIU Xue-wei;PAN Rong;ZHOU Jiang-feng;YANG Jun-gang
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page:33-36,50
Coherent Structure for the Boundary Layer of MT1 Turbine Vane
SHI Wan-li;GE Ning
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page:28-32,62
Application of Micro- and Mini- Channel Heat Transfer Technology to Liner Cooling in Aero- Engine Combustor
MIAO Hui
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page:18-21,43