1000-8055
2015 Issue 9
..............page:2044
Aero-derivative industrial gas turbine dual fuel lean premixed low emission combustion technology
WEI Shu-ming;SUO Jian-qin;School of Power and Energy;Northwestern Polytechnical University;
WEI Shu-ming;SUO Jian-qin;School of Power and Energy;Northwestern Polytechnical University;
..............page:2049-2057
Heat transfer characteristics of rotor-stator cavity with small mass flow rate
LIN Li;WU Kang;TAN Qin-xue;REN Jing;JIANG Hong-de;Energy-saving Technology Research Center;School of Chemical Engineering;Fuzhou University;Institute of Gas Turbine;School of Mechanical Engineering;Tsinghua University;
LIN Li;WU Kang;TAN Qin-xue;REN Jing;JIANG Hong-de;Energy-saving Technology Research Center;School of Chemical Engineering;Fuzhou University;Institute of Gas Turbine;School of Mechanical Engineering;Tsinghua University;
..............page:2058-2065
Experiment on effect of initial pressure and narrow gap height on detonation initiation distance in narrow gap
ZHANG Peng-gang;PAN Zhen-hua;ZHU Yue-jin;WANG Qian;School of Energy and Power Engineering;Jiangsu University;
ZHANG Peng-gang;PAN Zhen-hua;ZHU Yue-jin;WANG Qian;School of Energy and Power Engineering;Jiangsu University;
..............page:2066-2072
Simulation analysis of air conditioning system of civil aircraft
WU Cheng-yun;WANG Guang-wen;LI Ge-ping;XIN Xu-dong;Shanghai Aircraft Design Research Institute;Commercial Aircraft Corporation of China Limited;
WU Cheng-yun;WANG Guang-wen;LI Ge-ping;XIN Xu-dong;Shanghai Aircraft Design Research Institute;Commercial Aircraft Corporation of China Limited;
..............page:2073-2079
Numerical analysis on infrared radiation characteristics of two-dimensional S-nozzle with small offset
YU Ming-fei;JI Hong-hu;LI Ning;WANG Hao;SI Ren;LIU Jian;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Guizhou Aero-engine Research Institute;Aviation Industry Corporation of China;
YU Ming-fei;JI Hong-hu;LI Ning;WANG Hao;SI Ren;LIU Jian;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Guizhou Aero-engine Research Institute;Aviation Industry Corporation of China;
..............page:2080-2087
Application of pipeline network algorithm in turbine inner cooling blade heat transfer calculation
SHI Liang;XIE Ming;HAN Wan-jin;YAN Pei-gang;School of Energy Science and Engineering;Harbin Institute of Technology;
SHI Liang;XIE Ming;HAN Wan-jin;YAN Pei-gang;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:2088-2099
Mathematical modeling analysis of hollow fiber membrane onboard inert gas generation system
CAI Yan;LIN Gui-ping;ZENG Yu;PENG Long;SHEN Xiao-bin;SUN Bing;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;China Aviation Asset Management Corporation Limited;Aviation Industry Corporation of China;
CAI Yan;LIN Gui-ping;ZENG Yu;PENG Long;SHEN Xiao-bin;SUN Bing;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;China Aviation Asset Management Corporation Limited;Aviation Industry Corporation of China;
..............page:2100-2107
Theoretical model and experiment of convective heat transfer in microchannel heat sinks
ZHAI Yu-ling;XIA Guo-dong;JIANG Jing;LI Yun-fei;Key Laboratory of Enhanced Heat Transfer and Energy Conservation Ministry of Education;College of Environmental and Energy Engineering;Beijing University of Technology;
ZHAI Yu-ling;XIA Guo-dong;JIANG Jing;LI Yun-fei;Key Laboratory of Enhanced Heat Transfer and Energy Conservation Ministry of Education;College of Environmental and Energy Engineering;Beijing University of Technology;
..............page:2108-2114
Experiment on performance of a hyper-combustor utilized in turbine based combined cycle engine
ZHU Zhi-xin;HE Xiao-min;XUE Chong;HONG Liang;QIN Wei-lin;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Science and Technology on Scramjet Laboratory;Beijing Power Machinery Institute;China Aerospace Science and Industry Corporation;
ZHU Zhi-xin;HE Xiao-min;XUE Chong;HONG Liang;QIN Wei-lin;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Science and Technology on Scramjet Laboratory;Beijing Power Machinery Institute;China Aerospace Science and Industry Corporation;
..............page:2115-2121
Thermo-physical properties for surrogate models of aviation kerosene
PEI Xin-yan;HOU Ling-yun;MO Chong-kang;DONG Ning;School of Aerospace Engineering;Tsinghua University;
PEI Xin-yan;HOU Ling-yun;MO Chong-kang;DONG Ning;School of Aerospace Engineering;Tsinghua University;
..............page:2122-2128
Experiment on combustion characteristics of n-heptane droplets in micro-tube
YAO Rong;LI Jun-wei;QIU Zuo-zhen;HUANG Jing-huai;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
YAO Rong;LI Jun-wei;QIU Zuo-zhen;HUANG Jing-huai;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:2129-2139
Applications of anisotropic unstructured mesh adaption in supersonic combustion simulations
ZOU Jian-feng;SHENG Dong;FANG Lei;ZHENG Yao;School of Aeronautics and Astronautics;Zhejiang University;Research and Development Center;China Acedamy of Luanch Vehicle Technology;China Aerospace Science and Technology Corporation;
ZOU Jian-feng;SHENG Dong;FANG Lei;ZHENG Yao;School of Aeronautics and Astronautics;Zhejiang University;Research and Development Center;China Acedamy of Luanch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:2140-2150
Research on limiters of unstructured grid
LI Fang;SUN Wei-zhe;LIU Xin;XU Jin-xiu;Jiangnan Institute of Computing Technology;
LI Fang;SUN Wei-zhe;LIU Xin;XU Jin-xiu;Jiangnan Institute of Computing Technology;
..............page:2151-2159
Geometry regulating law of variable cycle engine during mode transition
ZHOU Hong;WANG Zhan-xue;ZHANG Xiao-bo;ZHANG Ming-yang;School of Power and Energy;Northwestern Polytechnical University;
ZHOU Hong;WANG Zhan-xue;ZHANG Xiao-bo;ZHANG Ming-yang;School of Power and Energy;Northwestern Polytechnical University;
..............page:2160-2166
Partially averaged Navier-Stokes method for simulation of supersonic flow over a ramped-cavity
LUO Da-hai;YAN Chao;WANG Xiao-yong;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
LUO Da-hai;YAN Chao;WANG Xiao-yong;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2167-2173
Initial flow of 2-D planer nozzle
ZHANG Huan-hao;CHEN Zhi-hua;JIANG Xiao-hai;Key Laboratory of Transient Physics;Nanjing University of Science and Technology;
ZHANG Huan-hao;CHEN Zhi-hua;JIANG Xiao-hai;Key Laboratory of Transient Physics;Nanjing University of Science and Technology;
..............page:2174-2180
Mixing characteristics of supersonic mixing layer induced by forced vibration
ZHANG Dong-dong;TAN Jian-guo;L Liang;WANG Qian-cheng;Science and Technology on Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
ZHANG Dong-dong;TAN Jian-guo;L Liang;WANG Qian-cheng;Science and Technology on Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:2181-2188
Comparison and analysis of WENO schemes base on supersonic boundary layer transition
LIU Chao-yang;WANG Zhen-guo;SUN Ming-bo;WANG Hong-bo;College of Aerospace Science and Engineering;National University of Defense Technology;
LIU Chao-yang;WANG Zhen-guo;SUN Ming-bo;WANG Hong-bo;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:2189-2195
Influence on macroscopic stiffness of rotor mesostructure based on finite element method
CHENG Li;GAO Jun-yu;QU Ke;LI Shuai-ying;Aeronautics and Astronautics Engineering College;Air Force Engineering University;Collaborative Innovation Center of Advanced Aero-Engine;School of Aerospace;Xi’an Jiaotong University;
CHENG Li;GAO Jun-yu;QU Ke;LI Shuai-ying;Aeronautics and Astronautics Engineering College;Air Force Engineering University;Collaborative Innovation Center of Advanced Aero-Engine;School of Aerospace;Xi’an Jiaotong University;
..............page:2196-2202
Contact characteristics response analysis of blade-disc dovetail structure under rubbing condition
MA Hui;WANG Di;TAI Xing-yu;NAI Hai-qiang;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;
MA Hui;WANG Di;TAI Xing-yu;NAI Hai-qiang;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;
..............page:2203-2211
Finite element analysis of hard-coating composite structure considering strain-dependent characteristic
SUN Wei;LIU Ying;LI Hui;School of Mechanical Engineering and Automation;Northeastern University;
SUN Wei;LIU Ying;LI Hui;School of Mechanical Engineering and Automation;Northeastern University;
..............page:2212-2218
Principle of exhaust valve ablation at an aero piston engine
ZHANG Hong-tao;MENG Xian-zhao;FENG Yan-peng;Luoyang College;Civil Aviation Flight University of China;Laboratory of Aviation Safety Technology;China Academy of Civil Aviation Science and Technology;
ZHANG Hong-tao;MENG Xian-zhao;FENG Yan-peng;Luoyang College;Civil Aviation Flight University of China;Laboratory of Aviation Safety Technology;China Academy of Civil Aviation Science and Technology;
..............page:2219-2225
Effect of foreign object damage at different impact angles on high cycle fatigue strength of TC4 titanium alloys
BAO Zhen-qiang;HU Xu-teng;SONG Ying-dong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;
BAO Zhen-qiang;HU Xu-teng;SONG Ying-dong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;
..............page:2226-2233
Research on problem of deterministic stress coupling in transonic compressor
ZHAO Jun;LIU Bao-jie;Aviation Engineering Institute;Civil Aviation Flight University of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHAO Jun;LIU Bao-jie;Aviation Engineering Institute;Civil Aviation Flight University of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2234-2240
Three-dimensional body-force model for effect on compressor performance of inlet distortion
YIN Chao;HU Jun;GUO Jin;YAN Wei;ZHANG Chen-kai;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaborative Innovation Center of Advanced Aero-Engine;
YIN Chao;HU Jun;GUO Jin;YAN Wei;ZHANG Chen-kai;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaborative Innovation Center of Advanced Aero-Engine;
..............page:2241-2250
Influence of the U-shape inlet pipe on a centrifugal compressor performance
WANG Lei-lei;LAO Da-zhong;ZHAO Ben;LIU Heng;YANG Ce;Turbomachinery Institute;School of Mechanical Engineering;Beijing Institute of Technology;Mechanical and Electrical Engineering Institute;Hebei University of Engineering;
WANG Lei-lei;LAO Da-zhong;ZHAO Ben;LIU Heng;YANG Ce;Turbomachinery Institute;School of Mechanical Engineering;Beijing Institute of Technology;Mechanical and Electrical Engineering Institute;Hebei University of Engineering;
..............page:2251-2260
Effects of rotating disturbance on aerodynamics stability of axial-flow compressor
MAO Zhi-ming;HU Jun;ZHANG Huan;YAN Wei;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
MAO Zhi-ming;HU Jun;ZHANG Huan;YAN Wei;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2261-2270
Analysis on thermal control method of satellite in orbit based on self-driven thermostatic valve with sensitive wax
GONG Meng-meng;WANG Jin;LI Yun-ze;WANG Jun;Research and Development Center;China Academy of Launch Vehicle Technology;Beijing Institute of Astronautical System Engineering;China Academy of Launch Vehicle Technology;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
GONG Meng-meng;WANG Jin;LI Yun-ze;WANG Jun;Research and Development Center;China Academy of Launch Vehicle Technology;Beijing Institute of Astronautical System Engineering;China Academy of Launch Vehicle Technology;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2271-2277
Design of distributed control system and investigation on bus communication performance of a turbofan engine
TIAN Fei-long;GUO Ying-qing;LI Rui-chao;JIANG Cai-hong;School of Power and Energy;Northwestern Polytechnical University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
TIAN Fei-long;GUO Ying-qing;LI Rui-chao;JIANG Cai-hong;School of Power and Energy;Northwestern Polytechnical University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:2278-2285
Simulation research on compartmental tank propellant management based on AMESim
SU Li-chao;LIU Jian-yong;ZHANG Cheng-liang;SHI Jing-cheng;Science and Technology on Space Physics Laboratory;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
SU Li-chao;LIU Jian-yong;ZHANG Cheng-liang;SHI Jing-cheng;Science and Technology on Space Physics Laboratory;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:2286-2290
ICT local inspection of solid rocket motor’s defects
CHEN Qing-gui;LU Hong-yi;ZHOU Yuan;LI Shen;LI Peng;YU Guang-hui;Department of Airborne Vehicle Engineering;Naval Aeronautical and Astronautical University;No.7Department;Naval Aeronautical and Astronautical University;Unit 91206;Qingdao Branch;Naval Aeronautical and Astronautical University;
CHEN Qing-gui;LU Hong-yi;ZHOU Yuan;LI Shen;LI Peng;YU Guang-hui;Department of Airborne Vehicle Engineering;Naval Aeronautical and Astronautical University;No.7Department;Naval Aeronautical and Astronautical University;Unit 91206;Qingdao Branch;Naval Aeronautical and Astronautical University;
..............page:2291-2297
Vibration mode and dynamical characteristics of helical planetary gear train
LIN He;WANG San-min;DONG Jin-cheng;School of Mechanical Engineering;Northwestern Polytechnical University;
LIN He;WANG San-min;DONG Jin-cheng;School of Mechanical Engineering;Northwestern Polytechnical University;
..............page:2298-2304