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Gas Turbine Experiment and Research
1672-2620
2016 Issue 6
Application of deriving series engines from common core methodology on 5 kg/s air flow class core
LI Gang-tuan;,PAN Shuai-cheng;,LI Xiao-ming;
..............
page:1-5,25
Test investigation on the low cycle fatigue life of a disk with simulated axial load
GUO Xiao-qiang;
..............
page:6-9
External flow field performance study of STOVL aircraft
YUAN Chang-long;,GONG Sheng;,YU Ping;,HAN Jia;
..............
page:10-15
Design technology and experimental verification of a single stage fan with high tip speed and low pressure ratio
HUANG Lei;,ZHOU Bai-hao;,LI Qing-hua;,LUO Xuan;,ZHU Chao-yi;
..............
page:16-20
Flight test data-driven model identification of turbofan engine
PAN Peng-fei;,MA Ming-ming;,XU Yan-zhi;
..............
page:21-25
Aero-engine performance model correction based on component performance map
PAN Shuai-cheng;,LI Gang-tuan;,DING Zhao-xia;,BAI Lei;
..............
page:26-29,33
Experimental troubleshooting analysis and verification study of a multi-stage axial-flow compressor with high speed and load
REN Fei;,XUN Feng;,ZHANG Ya;,LIU Zhi-gang;,XIANG Hong-hui;,SU Ting-ming;,XIA Lian;
..............
page:30-33
Diagnoses and analysis of the failure of an engine nozzle control
ZHOU Yan;,WANG Xi;,JIANG Xiao-feng;,XU Gang-gang;
..............
page:34-37
Dynamic characteristics of variable geometry channel control executive device
ZHANG Wei;,ZHOU Zhen-hua;,ZOU Pin-wen;,HAN Xiao-man;,LV Yu;
..............
page:38-43
Application of laser additive manufacturing technology in turbine blade and vane
TAO Yun-ya;,XUE Wei-peng;,TANG Hong-fei;,SU Yun-liang;,HUANG Shun-zhou;,ZHAO Xiao-ming;
..............
page:44-50,55
Design and experimental investigation of instability identification system for fan and compressor
ZHONG Ming;,CHENG Hong-min;,XIONG Bing;,HAN Wei;
..............
page:51-55
Compliance with pertinent regulations for aero-engine overspeed protection system
CHEN Jun-wei;
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page:56-60
2016 nian 1~6 qi zong mu ci
..............
page:61-62