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Journal of Aerospace Power
1000-8055
2016 Issue 3
Review on the blade loss of aero-engine
MA Yan-hong;LIANG Zhi-chao;WANG Gui-hua;ZHANG Da-yi;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:513-526
Effect of interface debonding on matrix multicracking evolution of fiber-reinfroced ceramic-matrix composites
LI Long-biao;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;
..............page:527-538
Creep-fatigue life prediction of single crystal turbine blade with the influence of stress relaxation
GAO Jing-yun;ZHANG Cheng-cheng;HOU Nai-xian;REN Yuan;LI Ying;WEN Zhi-xun;YUE Zhu-feng;Shanghai Engineering Research Center of Commercial Aircraft Engine;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;School of Mechanics;Civil Engineering and Architecture;Northwestern Polytechnical University;
..............page:539-547
Sound absorption characteristics of resonator with multi slits under high sound pressure level
XU Jun;LI Xiao-dong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Research and Development Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:548-554
Model updating in structural dynamics based on radial-Tchebichef moments
JIANG Dan-dan;ZANG Chao-ping;MEI Qing;LU Yan-hui;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:555-566
Analysis of crack propagation for a compressor disk with cracks on pin holes
ZHANG Zhi-xuan;SHI Duo-qi;YANG Xiao-guang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:567-574
Influence of compression ratio on microstructure and mechanical behavior of metal rubber
GAO Di;MA Yan-hong;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:575-580
Coupled simulation of gas radiation and wall temperature in vectored nozzle
LIAO Hua-lin;CHEN Xu-yi;ZHANG Xiao-ying;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Gas Turbine Establishment;Aviation Industry Corporation of China;School of Electric Power;South China University of Technology;Institut Franco-Chinois de I’Energie Nucléaire;Sun Yat-sen University;
..............page:581-587
Experiment on non-self-similar of Mach reflection of gaseous detonation wave
LIU Jie;ZHAO Huan-juan;DU Zhong-hua;CHEN Xi;School of Mechanical Engineering;Nanjing University of Science and Technology;School of Chemical Engineering and Environment;Beijing Institute of Technology;
..............page:588-597
Effects of combustor length on solid fuel scramjet combustor performance
TAO Huan;WEI Zhi-jun;CHI Hong-wei;SUN Wei-wei;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:598-607
Influence of air split of a radial swirler on ignition and extinction characteristics
DAI Wei;LIN Yu-zhen;XU Quan-hong;ZHANG Chi;GONG Jing;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Department of Scientific Research Project;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:608-615
Micro bubble nucleation inside suspended droplet in combustion
LU Qi-zhi;GONG Jing-song;PIAO Ying;YIN Ya-jun;LI Hui;FAN Hong-yu;School of Aerospace Engineering;Tsinghua University;
..............page:616-622
Analysis on combustion instability based on empirical mode decomposition
FU Yu;GUO Zhi-hui;YANG Fu-jiang;CHE Jun-long;National Key Laboratory of Science and Technology on Aero-Engines Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:623-630
Numerical study on aerodynamic performance of multi-stage lobed mixer-ejector
CHEN Geng;TAN Xiao-ming;FU Jun;ZHANG Jin-zhou;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:631-638
Characterization and mechanism analysis of several abnormal aerodynamic phenomena of axial flow compressor experiment
XIANG Hong-hui;HOU Min-jie;GE Ning;LIU Zhi-gang;YANG Rong-fei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Key Laboratory on Aero-engine Altitude Simulation Technology;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:639-646
Influence of blade tip winglet on the off-design performance of a transonic compressor rotor
HAN Shao-bing;ZHONG Jing-jun;Marine Engineering College;Dalian Maritime University;
..............page:647-658
Unsteady calculation of pressure pulsations within hydraulic turbine under different entrance sections
SHI Guang-tai;YANG Jun-hu;MIAO Sen-chun;WANG Xiao-hui;Department of Energy and Power Engineering;Lanzhou University of Technology;
..............page:659-668
Numerical simulation of single-stage transonic compressor with inlet distortion
GUO Jin;HU Jun;YIN Chao;TU Bao-feng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:669-677
Entropy generation control volume method and its application into flow loss evolution in a compressor with near zero tip clearance
LU Qian;NAN Xi;LIN Feng;Key Laboratory of Advanced Energy and Power;Institute of Engineering Thermophysics;Chinese Academy of Sciences;University of Chinese Academy of Sciences;
..............page:678-684
Simulation analysis on performance of a high speed centrifugal oil-air separator
HAN Jin-zai;CHEN Cong-hui;XU Rang-shu;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;Faculty of Aerospace Engineering;Shenyang Aerospace University;
..............page:685-691
Direct thrust control of turbofan engines based on unknown input observer
WANG Bin;WANG Xi;KONG Xiang-xing;YANG Bei;Academy of Aeronautic Propulsion Technology;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:692-699
Robust LPV/PI control for aero-engine based on polynomial sum of squares programming
WU Bin;HUANG Jin-quan;JIANG Rui;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-engine;
..............page:700-707
A model-based fault tolerant control strategy for turbofan engine
HE Xiao-dong;GUO Ying-qing;DU Xian;School of Power and Energy;Northwestern Polytechnical University;
..............page:708-716
Numerical simulation on influence of boundary-layer thickness on the cavity aero-acoustic characteristics
ZHANG Qun-feng;YAN Pan-pan;LI Jun;School of Civil Engineering;Beijing Jiaotong University;Shenyang Aircraft Design and Research Institute;Aviation Industy Corporation of China;
..............page:717-725
Analysis on flow field characteristics of lateral jet on slender body
ZHAO Fa-ming;WANG Jiang-feng;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:726-732
Numerical simulation on re-ingestion characteristics under landing state for thrust reverser
CHEN Zhu;SHAN Yong;SHEN Xi-gang;ZHANG Jing-zhou;SHAO Wan-ren;Jiangsu Province Key Laboratory of Aerospace Power System College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Gas Turbine Establishment;Aviation Industry Corporation of China;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:733-739
Numerical simulation of axial-injection end-burning hybrid rocket motor
LI Xin-tian;LU Xin;LI Yan-cheng;LIU Jun-yi;ZHANG Cheng;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:740-745
Pipe flow resistance characteristics of test system for low-thrust NTO/MMH rocket engines with high chamber pressure
LIU Lie;WEI Qiang;FANG Zhong-jian;LIANG Guo-zhu;ZHANG Xue-jun;School of Astronautics;Beijing University of Aeronautics and Astronautics;Beijing Institute of Aerospace Testing Technology;Academy of Aerospace Propulsion Technology;China Aerospace Science and Technology Corporation;
..............page:746-755
Mechanical erosion characteristics of carbon-based nozzle in solid rocket motor
CHANG Heng;WANG Yi-bai;LIU Yu;XUE Bin;CAO Xi-wei;School of Astronautics;Beijing University of Aeronautics and Astronautics;Research of Development Center;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:756-762
Research on load sharing mechanism of star gear trains for GTF engine
MO Shuai;ZHANG Yi-du;WU Qiong;WANG Fei-ming;State Key Laboratory of Virtual Reality Technology and Systems;Beijing University of Aeronautics and Astronautics;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:763-768