1000-8055
2016 Issue 9
Temperature field test for aeroengine combustor with five nozzles based on gas analysis
WANG Ming-rui;XIAO Yang;HAN Bing;LI Ya-juan;JIA Lin-yan;MA Zheng;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Power and Energy Engineering;Harbin Engineering University;
WANG Ming-rui;XIAO Yang;HAN Bing;LI Ya-juan;JIA Lin-yan;MA Zheng;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Power and Energy Engineering;Harbin Engineering University;
..............page:2049-2054
Combustion reaction mechanism of three-component simulation surrogate fuel for RP-3 kerosene
LIU Yu;ZENG Wen;MA Hong-an;CHEN Bao-dong;Faculty of Aerospace Engineering;Shenyang Aerospace University;
LIU Yu;ZENG Wen;MA Hong-an;CHEN Bao-dong;Faculty of Aerospace Engineering;Shenyang Aerospace University;
..............page:2055-2064
Numerical investigation of shaped-hole film cooling on turbine rotor blade
ZHU Xing-dan;ZHANG Jing-zhou;TAN Xiao-ming;GUO Wen;SU Yun-liang;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;
ZHU Xing-dan;ZHANG Jing-zhou;TAN Xiao-ming;GUO Wen;SU Yun-liang;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;
..............page:2065-2072
Effect on working characteristic of fuel injection pump in aircrafts of temperature
SHAO Lei;LIU Wei-hua;PAN Jun;LIU Wen-yi;FENG Shi-yu;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration;Nanjing Engineering Institute of Aircraft Systems;Jincheng;Aviation Industry Corporation of China;
SHAO Lei;LIU Wei-hua;PAN Jun;LIU Wen-yi;FENG Shi-yu;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration;Nanjing Engineering Institute of Aircraft Systems;Jincheng;Aviation Industry Corporation of China;
..............page:2073-2079
Influence of chamber length on rotating detonation engine performance
SUN Jian;ZHOU Jin;LIN Zhi-yong;LIU Shi-jie;College of Aerospace Science and Engineering;National University of Defense Technology;
SUN Jian;ZHOU Jin;LIN Zhi-yong;LIU Shi-jie;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:2080-2086
Envelope protection method for pitch attitude holding mode under flight icing conditions
WANG Xiao-long;XUN Hao-jun;XUE Yuan;ZHU He-quan;PEI Bin-bin;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
WANG Xiao-long;XUN Hao-jun;XUE Yuan;ZHU He-quan;PEI Bin-bin;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2087-2094
Effects of sleeve mixing length of swirl cup on the ignition characteristics
KANG Yao;LIN Yu-zhen;JIANG Yao;WANG Xiao-feng;China Aviation Powerplant Research Institute;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;
KANG Yao;LIN Yu-zhen;JIANG Yao;WANG Xiao-feng;China Aviation Powerplant Research Institute;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:2095-2103
Aeroacoustic and flow field features of ultrasonic atomizer based on Hartmann resonance tube
RUAN Can;HUANG Yue;CAI Jiang-qian;LIU Chen;XING Fei;School of Aerospace Engineering;Xiamen University;
RUAN Can;HUANG Yue;CAI Jiang-qian;LIU Chen;XING Fei;School of Aerospace Engineering;Xiamen University;
..............page:2104-2114
Effect of width of skirted mixer on performance of mixing diffuser with par-allel intake
LIU You-hong;CHEN Zhong-yuan;XU Hua-sheng;ZHONG Shi-lin;HUANG Yi-yong;XIE Jian-guang;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Power and Energy Engineering;Beijing University of Aeronautics and Astronautics;China Gas Turbine Establishment;Aviation Industry Corporation of China;
LIU You-hong;CHEN Zhong-yuan;XU Hua-sheng;ZHONG Shi-lin;HUANG Yi-yong;XIE Jian-guang;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Power and Energy Engineering;Beijing University of Aeronautics and Astronautics;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:2115-2123
Optimization design of two dimensional convergent and divergent nozzles’profile based on surrogate models
SHI Xiao-juan;JI Hong-hu;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
SHI Xiao-juan;JI Hong-hu;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2124-2131
Investigation on the performance of a supersonic inlet with diversing flow control on the exit
WEN Yu-fen;YAN Jia-min;CHEN Hao;MA You-lin;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
WEN Yu-fen;YAN Jia-min;CHEN Hao;MA You-lin;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:2132-2139
Wind tunnel side wall boundary layer control based on vortex generator
LIU Guang-yuan;WANG Rui-bo;DENG Ji-long;CHEN Hong-tao;High Speed Aerodynamics Institute;China Aerodynamics Research and Development Center;
LIU Guang-yuan;WANG Rui-bo;DENG Ji-long;CHEN Hong-tao;High Speed Aerodynamics Institute;China Aerodynamics Research and Development Center;
..............page:2140-2145
Investigation of rod-airfoil interaction noise using large eddy simulation and FW-H equation
CHEN Wei-jie;QIAO Wei-yang;WANG Liang-feng;XU Kun-bo;TONG Fan;School of Power and Energy;Northwestern Polytechnical University;
CHEN Wei-jie;QIAO Wei-yang;WANG Liang-feng;XU Kun-bo;TONG Fan;School of Power and Energy;Northwestern Polytechnical University;
..............page:2146-2155
Ionization effects on aerodynamic heat for vehicle in hypersonic rarefied flow
QU Cheng;WANG Jiang-feng;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
QU Cheng;WANG Jiang-feng;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2156-2163
Reconstructing technique of forebody shock system and its applicationin hypersonic inlet
LI Cheng-hong;TAN Hui-jun;NING Le;LI Guang-sheng;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;
LI Cheng-hong;TAN Hui-jun;NING Le;LI Guang-sheng;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:2164-2170
Analysis on damping effect of dry friction damper under wideband multi-harmonic excitation
LI Lin;LIU Jiu-zhou;LI Chao;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
LI Lin;LIU Jiu-zhou;LI Chao;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2171-2180
Impact factors to friction characteristics of space lubricating oil No.4116
WANG Yan-shuang;LI Gang;CHENG Jun-wei;Tianjin Key Laboratory of High Speed Cutting and Precision Machining;College of Mechanical Engineering;Tianjin University of Technology and Education;School of Mechanical Engineering;Tianjin University;
WANG Yan-shuang;LI Gang;CHENG Jun-wei;Tianjin Key Laboratory of High Speed Cutting and Precision Machining;College of Mechanical Engineering;Tianjin University of Technology and Education;School of Mechanical Engineering;Tianjin University;
..............page:2181-2187
Application of cyclic symmetry property in transient response solution of mistuned bladed disks
YAO Jian-yao;XIN Jian-qiang;WANG Jian-jun;College of Aerospace Engineering;Chongqing University;Research and Development Center;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
YAO Jian-yao;XIN Jian-qiang;WANG Jian-jun;College of Aerospace Engineering;Chongqing University;Research and Development Center;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2188-2194
Probabilistic risk assessment method for turbine disk
SUN Yang-hui;YANG Kun;HOU Nai-xian;CHEN Jian;BAI Guo-juan;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
SUN Yang-hui;YANG Kun;HOU Nai-xian;CHEN Jian;BAI Guo-juan;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:2195-2202
Stiffness modification and dynamic modeling of a rod fastening rotor
LU Ming-jian;SUN Yan-hua;ZHOU Jian;ZHAO Shi-quan;GENG Hai-peng;WANG Wei-ming;State Key Laboratory of Strength and Vibration for Mechanical Structure;School of Mechanical Engineering;Xi’an Jiaotong University;Dongfang Turbine Company Limited;Dongfang Electric Corporation;
LU Ming-jian;SUN Yan-hua;ZHOU Jian;ZHAO Shi-quan;GENG Hai-peng;WANG Wei-ming;State Key Laboratory of Strength and Vibration for Mechanical Structure;School of Mechanical Engineering;Xi’an Jiaotong University;Dongfang Turbine Company Limited;Dongfang Electric Corporation;
..............page:2203-2209
Magnetic field analysis and optimization of giant magnetostrictive electro-hydrostatic actuator
YANG Xu-lei;ZHU Yu-chuan;FEI Shang-shu;JI Liang;GUO Ya-zi;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
YANG Xu-lei;ZHU Yu-chuan;FEI Shang-shu;JI Liang;GUO Ya-zi;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2210-2217
Sand erosion damage test on TC4 titanium alloy and TiN/Ti multilayer coating
CAO Xin;WANG Guan;HE Wei-feng;ZHANG Yi-fei;HE Guang-yu;YANG Zhu-fang;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
CAO Xin;WANG Guan;HE Wei-feng;ZHANG Yi-fei;HE Guang-yu;YANG Zhu-fang;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2218-2225
Cross-sectional feature parameters extraction of blade based on unorganized point cloud
LIU Shu-gui;MAO Chen-li;ZHANG Hai-tao;State Key Laboratory of Precision Measuring Technology and Instruments;Tianjin University;
LIU Shu-gui;MAO Chen-li;ZHANG Hai-tao;State Key Laboratory of Precision Measuring Technology and Instruments;Tianjin University;
..............page:2226-2232
Effect of bulk swirl on performance and stability of transonic single rotor
TU Bao-feng;HU Jun;ZHANG Kai;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;
TU Bao-feng;HU Jun;ZHANG Kai;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:2233-2238
Aerodynamic rotating instability and fluctuated characteristics of tip clearance flow in low speed axial flow compressor
WANG Hao;WU Ya-dong;OUYANG Hua;School of Mechanical Engineering;Shanghai Jiao Tong University;School of Aeronautics and Astronautics;Shanghai Jiao Tong University;
WANG Hao;WU Ya-dong;OUYANG Hua;School of Mechanical Engineering;Shanghai Jiao Tong University;School of Aeronautics and Astronautics;Shanghai Jiao Tong University;
..............page:2239-2250
Numerical simulation method of roughness induced transition
LI Hong-yang;ZHENG Yun;LIU Da-xiang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
LI Hong-yang;ZHENG Yun;LIU Da-xiang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2251-2257
Analysis on tip flow structure in transonic fan rotor
YANG Xi-qiong;LIU Bo;CAO Zhi-yuan;MAO Xiao-chen;XIA Shu-dan;School of Power and Energy;Northwestern Polytechnical University;
YANG Xi-qiong;LIU Bo;CAO Zhi-yuan;MAO Xiao-chen;XIA Shu-dan;School of Power and Energy;Northwestern Polytechnical University;
..............page:2258-2267
Modeling and simulation of compressor system with actuators
SU San-mai;SUN Zhan-heng;L Ye;LIU Jun-jie;School of Power and Energy;Northwestern Polytechnical University;China Aviation Publishing and Media Company Limited;Aviation Industry Corporation of China;
SU San-mai;SUN Zhan-heng;L Ye;LIU Jun-jie;School of Power and Energy;Northwestern Polytechnical University;China Aviation Publishing and Media Company Limited;Aviation Industry Corporation of China;
..............page:2268-2275
A multivariable frequency-domain dynamic pseudodiagonalization method and design of aero-engine decoupling controller
PENG Kai;FAN Ding;GUO Ya-nan;BU Zhen-peng;JIAO Chun-bo;XUE Yuan;School of Power and Energy;Northwestern Polytechnical University;Collaborative Innovation Center for Advanced Aero-Engine;Unit 92728of People’s Liberation Army of China;Military Resident Representative Bureau of Rocket Force in Jinzhou;Operating Branch of Xi’an Metro Company Limited;
PENG Kai;FAN Ding;GUO Ya-nan;BU Zhen-peng;JIAO Chun-bo;XUE Yuan;School of Power and Energy;Northwestern Polytechnical University;Collaborative Innovation Center for Advanced Aero-Engine;Unit 92728of People’s Liberation Army of China;Military Resident Representative Bureau of Rocket Force in Jinzhou;Operating Branch of Xi’an Metro Company Limited;
..............page:2276-2282
Effect of momentum ratio on atomization characteristics of unlike-doublet impinging jets injector
ZHENG Gang;FENG Wei;NIE Wan-sheng;ZHOU Li-xin;Department of Space Equipment;Equipment Academy;Technology Department;Xichang Satellite Launch Center;Xi’an Aerospace Propulsion Institute;China Aerospace Science and Technology Corporation;
ZHENG Gang;FENG Wei;NIE Wan-sheng;ZHOU Li-xin;Department of Space Equipment;Equipment Academy;Technology Department;Xichang Satellite Launch Center;Xi’an Aerospace Propulsion Institute;China Aerospace Science and Technology Corporation;
..............page:2283-2289
Numerical simulation of nozzle damping characteristics in solid rocket motor
SUN Bing-bing;LI Jun-wei;SU Wan-xing;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;Research and Development Center;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
SUN Bing-bing;LI Jun-wei;SU Wan-xing;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;Research and Development Center;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:2290-2297
Test rig design and experiment of gas thrust foil bearing
XU Fang-cheng;LIU Zhan-sheng;ZHANG Guang-hui;ZHANG Wen;SUN Yi;School of Energy Science and Engineering;Harbin Institute of Technology;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;School of Astronautics;Harbin Institute of Technology;
XU Fang-cheng;LIU Zhan-sheng;ZHANG Guang-hui;ZHANG Wen;SUN Yi;School of Energy Science and Engineering;Harbin Institute of Technology;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;School of Astronautics;Harbin Institute of Technology;
..............page:2298-2304