1000-8055
2016 Issue 2
..............page:252
Effect of low cycle fatigue pre-damage on high cycle fatigue strength of TA11 alloy
SHI Duo-qi;LUO Yin-yin;ZHAO Peng-tao;YU Hui-chen;YANG Xiao-guang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;Inspection Center of Materials;Beijing Institute of Aeronautical Materials;
SHI Duo-qi;LUO Yin-yin;ZHAO Peng-tao;YU Hui-chen;YANG Xiao-guang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;Inspection Center of Materials;Beijing Institute of Aeronautical Materials;
..............page:257-265
Experiment on electric discharge machining of cooling holes in superalloy IN718
GUO Yong-feng;ZHANG Guo-wei;WANG Li;GUO Ben-sheng;School of Mechatronics Engineering;Harbin Institute of Technology;
GUO Yong-feng;ZHANG Guo-wei;WANG Li;GUO Ben-sheng;School of Mechatronics Engineering;Harbin Institute of Technology;
..............page:266-273
Assessment method of structural efficiency on bearing system in aero-engine
MA Yan-hong;CAO Chong;LI Xin;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
MA Yan-hong;CAO Chong;LI Xin;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:274-281
Theoretic investigation on vibration characteristics of structure with air film damper
ZHANG Da-yi;HE Yi-feng;CHEN Lu-lu;MA Yan-hong;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
ZHANG Da-yi;HE Yi-feng;CHEN Lu-lu;MA Yan-hong;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:282-288
Crystallographic-orientation-related performance of single crystal turbine blade and optimization design of three-dimensional orientations
GAO Jing-yun;FANG Lei;ZHANG Cheng-cheng;REN Yuan;LI Ying;Shanghai Engineering Research Center for Commercial Aircraft Engine;Commercial Aircraft Engine Compary Limited;Aviation Industry Corporation of China;
GAO Jing-yun;FANG Lei;ZHANG Cheng-cheng;REN Yuan;LI Ying;Shanghai Engineering Research Center for Commercial Aircraft Engine;Commercial Aircraft Engine Compary Limited;Aviation Industry Corporation of China;
..............page:289-298
A thermo-mechanical fatigue life assessment method for single crystal turbine blades
JING Fu-lei;WANG Rong-qiao;HU Dian-yin;Academy of Aeronautic Propulsion Technology;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
JING Fu-lei;WANG Rong-qiao;HU Dian-yin;Academy of Aeronautic Propulsion Technology;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:299-306
Study on imbalance-fixed point rubbing coupling faults of dual-disc cantilever rotor
YANG Yang;CAO Deng-qing;WANG De-you;JIANG Guang-yi;School of Astronautics;Harbin Institute of Technology;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
YANG Yang;CAO Deng-qing;WANG De-you;JIANG Guang-yi;School of Astronautics;Harbin Institute of Technology;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:307-316
Multiaxial fatigue life prediction based on non-proportionality of strain path
ZHONG Bo;WANG Yan-rong;WEI Da-sheng;YANG Long;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
ZHONG Bo;WANG Yan-rong;WEI Da-sheng;YANG Long;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:317-322
Analysis and optimization of helicopter main gearbox housing structural vibration and noise
ZHANG Lin;LI Shu;ZHANG Tao;Large Aircraft Advanced Training Centre;Beijing University of Aeronautics and Astronautics;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Mechatronical Engineering;Beijing Institute of Technology;
ZHANG Lin;LI Shu;ZHANG Tao;Large Aircraft Advanced Training Centre;Beijing University of Aeronautics and Astronautics;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Mechatronical Engineering;Beijing Institute of Technology;
..............page:323-329
Optimization reliability test design modeling based on information fusion
ZHANG An-yang;LIU Qi;College of Information System and Management;National University of Defense Technology;
ZHANG An-yang;LIU Qi;College of Information System and Management;National University of Defense Technology;
..............page:330-336
Numerical analysis on effect of cooling air pocket area on performance of air-cooled fuel injector
LIU You-hong;WANG Xiao-bo;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Power and Energy Engineering;Beijing University of Aeronautics and Astronautics;
LIU You-hong;WANG Xiao-bo;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Power and Energy Engineering;Beijing University of Aeronautics and Astronautics;
..............page:337-344
Aero-engine certification method and safety margin of “drop-in” fuel
YANG Xiao-yi;DING Shui-ting;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
YANG Xiao-yi;DING Shui-ting;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:345-349
Impact of atmospheric and ground infrared radiation on infrared stealth effect of long-wave band low emissivity of high-flying aircraft
HUANG Wei;JI Hong-hu;LU Hao-hao;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
HUANG Wei;JI Hong-hu;LU Hao-hao;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:350-359
Heat transfer characteristics in U-shaped rib-roughened channel at high rotation numbers
ZHANG Hong;TIAN Shu-qing;DENG Hong-wu;LI Yang;Research and Development Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHANG Hong;TIAN Shu-qing;DENG Hong-wu;LI Yang;Research and Development Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:360-368
Thermodynamic cycle performance of detonation gas turbine with variable specific heat capacity
LI Xiao-feng;XIAO Jun-feng;WANG Wei;WANG Feng;WEI Shi-rang;ZHENG Long-xi;Gas Turbine Technology Department;Xi’an Thermal Power Research Institute Company Limited;School of Power and Energy;Northwestern Polytechnical University;
LI Xiao-feng;XIAO Jun-feng;WANG Wei;WANG Feng;WEI Shi-rang;ZHENG Long-xi;Gas Turbine Technology Department;Xi’an Thermal Power Research Institute Company Limited;School of Power and Energy;Northwestern Polytechnical University;
..............page:369-376
Self-ignition in supersonic flow induced by oblique shock wave
XI Wen-xiong;SUN Ming-bo;LI Qing;State Key Laboratory of Laser Propulsion and Application;Equipment Academy;the Chinese People’s Liberation Army;Science and Technology on Scramjet Laboratory;National University of Defense Technology;
XI Wen-xiong;SUN Ming-bo;LI Qing;State Key Laboratory of Laser Propulsion and Application;Equipment Academy;the Chinese People’s Liberation Army;Science and Technology on Scramjet Laboratory;National University of Defense Technology;
..............page:377-382
Tip leakage flow and heat transfer characteristics with effect of trailing edge cutback on squealer tip
CHENG Feng-na;CHANG Hai-ping;ZHANG Jing-yang;TIAN Xing-jiang;DU Zhi-neng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;College of Astronautics;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
CHENG Feng-na;CHANG Hai-ping;ZHANG Jing-yang;TIAN Xing-jiang;DU Zhi-neng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;College of Astronautics;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:383-390
Study on surrogate model of endothermic hydrocarbon fuel RP-3
CHENG Ze-yuan;ZHU Jian-qin;JIN Zhao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
CHENG Ze-yuan;ZHU Jian-qin;JIN Zhao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:391-398
Effects of rotor blade icing on helicopter flight performance
XU Yu-mao;L Shao-jie;CAO Yi-hua;CHEN-Rui;General Design Department;China Helicopter Research and Development Institute;Department of General Demonstration;Army Aviation Institute;School of Aeronautic Science and Technology;Beijing University of Aeronautics and Astronautics;
XU Yu-mao;L Shao-jie;CAO Yi-hua;CHEN-Rui;General Design Department;China Helicopter Research and Development Institute;Department of General Demonstration;Army Aviation Institute;School of Aeronautic Science and Technology;Beijing University of Aeronautics and Astronautics;
..............page:399-404
Simulation test of a powder starting system of a missile engine
ZHU Rong-chuan;LIU Zhi-gang;GU Yang;DAI Guo-zhi;HE Yuan;China Gas Turbine Establishment;Aviation Industry Corporation of China;
ZHU Rong-chuan;LIU Zhi-gang;GU Yang;DAI Guo-zhi;HE Yuan;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:405-412
Power characteristics of the compound helicopter in transition flight mode
CAO Fei;CHEN Ming;TIAN Li;DENG Yang-ping;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Aeronautics;Northwestern Polytechnical University;
CAO Fei;CHEN Ming;TIAN Li;DENG Yang-ping;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Aeronautics;Northwestern Polytechnical University;
..............page:413-420
CFD analyses of aerodynamic characteristics of tilt-rotor under typical flight conditions
LI Peng;ZHAO Qi-jun;National Key Laboratory of Rotorcraft Aeromechanics;Nanjing University of Aeronautics and Astronautics;
LI Peng;ZHAO Qi-jun;National Key Laboratory of Rotorcraft Aeromechanics;Nanjing University of Aeronautics and Astronautics;
..............page:421-431
Effects of synthetic jet frequency on the separated flow in a diffusing S-duct
HE Peng;DONG Jin-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
HE Peng;DONG Jin-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:432-442
Convergence analysis of hypersonic turbulent flow calculation at compression corner
XIA Chen-chao;ZHAO Wen-wen;CHEN Li-hua;CHEN Wei-fang;School of Aeronautics and Astronautics;Zhejiang University;
XIA Chen-chao;ZHAO Wen-wen;CHEN Li-hua;CHEN Wei-fang;School of Aeronautics and Astronautics;Zhejiang University;
..............page:443-450
Consistent capacity research on endothermic hydrocarbon fuels and superalloy
ZHANG Zhong-li;LI Bin;ZHANG Meng-zheng;ZHOU Li-xin;Xi’an Aerospace Propulsion Institute;China Aerospace Science and Technology Corporation;
ZHANG Zhong-li;LI Bin;ZHANG Meng-zheng;ZHOU Li-xin;Xi’an Aerospace Propulsion Institute;China Aerospace Science and Technology Corporation;
..............page:451-458
Effect of inlet internal contraction ratio on performance of solid fuel scramjet
LI Biao;WEI Zhi-jun;CHI Hong-wei;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
LI Biao;WEI Zhi-jun;CHI Hong-wei;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:459-466
Application of SVM in stability of gas pressure reducing regulator
SUN Shi-yuan;WANG Yong-jun;CHEN Yang;WANG Bao-shan;CHEN Jing-lu;School of Mathematics and Systems Science;Beijing University of Aeronautics and Astronautics;School of Astronautics;Beijing University of Aeronautics and Astronautics;
SUN Shi-yuan;WANG Yong-jun;CHEN Yang;WANG Bao-shan;CHEN Jing-lu;School of Mathematics and Systems Science;Beijing University of Aeronautics and Astronautics;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:467-476
FPGA-based autonomous over-speed protection system for aero-engine
JIANG Wen-liang;LU Qian-li;YU Zhen;ZHU Yin-yu;HUANG Jin-quan;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;
JIANG Wen-liang;LU Qian-li;YU Zhen;ZHU Yin-yu;HUANG Jin-quan;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:477-483
Fault diagnosis for actuators of aero-engine fuel system based on NN-ELM
JIANG Jie;LI Qiu-hong;ZHANG Gao-qian;LI Ye-bo;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
JIANG Jie;LI Qiu-hong;ZHANG Gao-qian;LI Ye-bo;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:484-492
Vortex generators control flat boundary layer separation of large eddy simulation
HU Hao;LI Xin-kai;DAI Li-ping;WANG Xiao-dong;KANG Shun;Key Laboratory of Condition Monitoring and Control for Power Plant Equipment of Ministry of Education;School of Energy Power and Mechanical Engineering;North China Electric Power University;School of Electric Power;North China University of Water Resources and Electric Power;Xi’an Modern Control Technology Research Institute;China North Industries Group Corporation;
HU Hao;LI Xin-kai;DAI Li-ping;WANG Xiao-dong;KANG Shun;Key Laboratory of Condition Monitoring and Control for Power Plant Equipment of Ministry of Education;School of Energy Power and Mechanical Engineering;North China Electric Power University;School of Electric Power;North China University of Water Resources and Electric Power;Xi’an Modern Control Technology Research Institute;China North Industries Group Corporation;
..............page:493-502
Coupling optimization design for aspirated compressor airfoil with low Reynolds number in high altitude
LI Jun;LIU Bo;YANG Xiao-dong;LU Xiao-feng;School of Power and Energy;Northwestern Polytechnical University;
LI Jun;LIU Bo;YANG Xiao-dong;LU Xiao-feng;School of Power and Energy;Northwestern Polytechnical University;
..............page:503-512