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Aeroengine
1672-3147
2016 Issue 3
Methods of Tolerance Design for Gears Based on Response Surface Methodology
WANG Gui-hua;,JING Hai-long;,SHI Yan-yan;,CHEN Yun-xia;
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page:1-6
Influence of Supporting Stiffness and Axial Location on Critical Speeds of a Low-Pressure Rotor of a Counter Rotating Engine
DENG Wang-qun;,WANG Yi;,NIE Wei-jian;,HE Ping;,XU You-liang;,YANG Hai;
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page:7-11
Differential Pressure Controller Stability Analysis and Research of Design Parameters
LI Hong-sheng;,WANG Xi;,WANG Hua-wei;,DANG Wei;,ZHANG Geng;
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page:12-16
Design and Application of Turbine Noise Airworthiness Assessment Platform of Aeroengine
ZHANG Hong;,JIANG Chao-zhen;,YAN Guo-hua;
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page:17-20
Study of Differences between Steady and Unsteady Computation for Two-Stage Turbine Internal Flow
YANG Jie;,ZHOU Ying;,PAN Shang-neng;,LU Cong-ming;
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page:21-27
Dynamic Characteristics Study on Transmission Rod with High Speed and Large Aspect Ratio
GUO Xia;,ZHANG Huan-zhang;,CHENG Xiao-yong;,WANG Shao-bo;
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page:28-32
Actuator Fault State Parameter Estimation of Aeroengine Based on On-Board Real Time Model
HE Jia-qian;,LI Jian-rong;,ZHANG Zhi-shu;
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page:33-37
Recognition of Different Vibration States of Aeroengine Based on the Vibration Energy Product SVD
QIN Hai-qin;,XU Ke-jun;
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page:38-42
Design for Two-Dimensional Supersonic Mixed Compression Inlet and Analysis of Inlet-Engine Matching
YU Tian-ning;,WU Hu;
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page:43-47
Analysis of Modal Characteristics and Anti-Resonance of Mistuned Bladed Disk
WANG Yao-wei;,BAI Guang-chen;,BAI Bin;,YAO Wei;,GAO Hai-feng;
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page:48-53
Design and Measurements for a Small Flow Rate Axial Compressor with Stage Work Coefficient of 0.42
WANG Li-zhi;,YANG Cheng-wu;,ZHANG Xiang-hua;,LU Zong-heng;
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page:54-60
Investigation of High and Low Cycle Fatigue Experiment for a Curved Dovetail Assembly
LI Di;,WANG Yan-rong;,LIAO Lian-fang;,WANG Jia-guang;,WEI Fei-fei;
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page:61-66
Application of Seven-Holes Composite Probe in Measurement of Plane Cascade Flow Field
WANG Dong;,LEI Zhi-jun;,LIU Jian-ming;,MA Lei;,WU Hui;,HAO Sheng-chun;
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page:67-73
Conversion Investigation on Blowout Performance for Multi-Sector and Full Annular Combustors
YANG Zhi-min;,ZHAO Ming-long;,LIN Yu-zhen;,GE Xin;,LIU Jin-lin;
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page:74-77
Throttling-Transient Model Identification of Twin Spool Aeroengine Based on Flight Test Data
PAN Peng-fei;,MA Ming-ming;,XU Yan-zhi;
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page:78-81
Formulation and Application for Vibration Test Loading Spectrum of an Aeroengine Revolution Transmitter
WANG Zhi-hui;,LIU Hai-nian;,ZHAI Yue;,ZHANG Sheng;
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page:82-87
Investigation and Experimental Validation on Static Pressure Loss of Aeroengine Hydraulic Pipe
LU Hao;,ZHOU Yi-bo;
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page:88-92
Fracture Failure Analysis for Blade Root of Compressor
LIU Guo-ku;,LIU Dong;
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page:93-97
A Correction Method for Aeroengine Adaptive Model
YANG Tian-nan;,WU Sen;,WANG Zheng;
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page:98-102
Introduction
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page:封2
hang kong fa dong ji zheng gao jian ze
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page:封3