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Journal of Aerospace Power
1000-8055
2015 Issue 1
Coupling solutions of flow and heat transfer in the Blasius laminar boundary layer flow over a vertical flat plate
ZHAO Guo-chang;SHAN Long;SONG Li-ping;DU Xia;KONG Jing-ru;ZHAO Heng;Faculty of Aerospace Engineering;Shenyang Aerospace University;Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System;Faulty of Aerospace Engineering;Shenyang Aerospace University;Institute of Higher Education;Shenyang Aerospace University;
..............page:1-9
Performance comparison between high temperature rise triple-swirler combustor and double-swirler combustor
LI Feng;GUO Rui-qing;SHANG Shou-tang;CHENG Ming;TANG Zheng-fu;SONG Bo;GAO Xian-zhi;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Combustion Design Office;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:10-15
Experiment on combustion performance of ramjet engine with trapped-vortex combustor
HE Xiao-min;QIN Wei-lin;ZHU Zhi-xin;NIU Zhi-gang;FEI Li-qun;PENG Li;YANG Cheng-yu;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 Research Institute;China Aerospace Science and Industry Corporation;
..............page:16-21
Numerical simulation and analysis of steady-state performances for face and cylinder gas film seal system
MA Gang;LUO Xian-hai;SHEN Xin-min;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;
..............page:22-28
Effect of inlet temperature and equivalence ratio on working process of pulse detonation engine
JIANG Tao;WENG Chun-sheng;National Key Laboratory of Transient Physics;Nanjing University of Science and Technology;
..............page:29-37
Numerical study on effect of hot jet ignition on flame acceleration and detonation initiation in detonation tube
ZHAO Wei;HAN Qi-xiang;WANG Jia-hua;ZHANG Gui-hua;College of Power and Energy Engineering;Nanjing University of Aeronautics and Astronautics;Department of Mechanical and Electrical Engineering;Hubei Water Resources Technical College;
..............page:38-45
Experiment of combustion performance of internally-staged combustor pilot stage
FU Zhen-bo;LIN Yu-zhen;ZHANG Chi;XU Quan-hong;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:46-52
Effect of fuel-air ratio and inlet parameters on performance of triple swirler combustor
DING Guo-yu;HE Xiao-min;ZHAO Zi-qiang;JIN Yi;WU Ze-jun;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:53-58
Effect of main flow orientation angle on cooling characteristics of single row of cylindrical film cooling holes
NIE Jian-hao;ZHU Hui-ren;School of Power and Energy;Northwestern Polytechnical University;
..............page:59-66
Dynamic characteristics of blades-disk-shaft rotor system with mistuned features
LI Chao-feng;ZHOU Shi-hua;REN Xiang;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;
..............page:67-75
A calculation method of contact stiffness between interfaces based on modal experiment
HU Dian-yin;SI Wu-lin;WEI Jia-ming;WANG Rong-qiao;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:76-81
Nonlinear vibration of rotor systems caused by assembly process of a bearing outer ring of an aero-engine
WANG Si-ji;LIAO Ming-fu;LIU Yong-quan;WANG De-you;JIANG Yun-fan;LIAO Jun;LI Hao;School of Power and Energy;Northwestern Polytechnical University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:82-89
Detail-structure optimization of single crystal turbine blade under the condition of geometric and dynamic constraints
LI Shi-feng;WEI Gang;SUN Fei-yan;LIU Qiang-jun;HE Ai-jie;CHEN Yong-xi;Research Laboratory for Turbine;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:90-95
Vibration analysis of aero-engine casing under radial harmonic excitation
WEN Deng-zhe;CHEN Yu-shu;School of Astronautics;Harbin Institute of Technology;
..............page:96-105
Mesoscopic modeling of three-dimensional four-directional braided composites using energy method
GONG Long-dong;SHEN Xiu-li;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:106-113
Structure research and photoelastic test verification of twin-web turbine disk with high thrust-weight ratio
DONG Shao-jing;SHEN Xiu-li;KANG Bin-peng;FAN Jiang;LI Shou-qiu;LUAN Yong-xian;HUO Cheng-min;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:114-120
Fatigue test of electron beam welding for TA19 in civil aircraft engine
SONG Li;YANG Jun-jie;CHEN Tie-feng;Research and Development Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:121-128
Optimization design of reverse deformation based on measuring results for investment cavity of turbine blade
XIE Xiao-na;WANG Wen-hu;ZHANG Yan;WANG Yuan-bin;Key Laboratory of Contemporary Design and Integrated Manufacturing Technology;Ministry of Education;School of Mechanical Engineering;Northwestern Polytechnical University;
..............page:129-135
A design method for high efficiency propeller
XIANG Song;WANG Ji;ZHANG Li-guo;TONG Sheng-xi;WU Jiang;LIU Yuan-qiang;Liaoning Key Laboratory of General Aviation;Shenyang Aerospace University;Aerodynamics Research Institute;Aviation Industry Corporation of China;
..............page:136-141
Rolling characteristics of vehicle with twist fin
ZHAO Bo-bo;LIU Rong-zhong;GUO Rui;ZHANG Jun;LIU Gao;CHEN Liang;School of Mechanical Engineering;Nanjing University of Science and Technology;The Unit 73917;the Chinese People’s Liberation Army;
..............page:142-148
Unsteady aerodynamic characteristics of dual rotor micro air vehicle
CAI Hong-ming;WU Zhi-lin;ANG Hai-song;XIAO Tian-hang;School of Mechanical Engineering;Nanjing University of Science and Technology;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:149-154
Unsteady aerodynamic force of tilt ducted fan during transition period
YANG Lei;YE Zheng-yin;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;
..............page:155-163
Numerical study of gas-steam ejection gas-liquid two-phase flow field under water
HU Xiao-lei;LE Gui-gao;MA Da-wei;LI Ren-feng;School of Mechanical Engineering;Nanjing University of Science and Technology;
..............page:164-172
Effect of local hump on stability of compressible boundary layer on flat plate
LI Hui;HUANG Zhang-feng;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;Department of Mechanics;School of Mechanical Engineering;Tianjin University;
..............page:173-181
Gray dynamic prediction of large gear tooth profile error measurement under multi-impact factors coupling
LI Qiang;WANG Zhong-yu;YAN Hu;WANG Qian;Key Laboratory of Precision Opto-Mechatronics Technology of Ministry of Education;School of Instrumentation Science and Opto-electronics Engineering;Beijing University of Aeronautics and Astronautics;
..............page:182-194
Ease-off flank topography design for aviation spiral bevel gears with higher-order transmission errors by modification of conjugate flank
CAO Xue-mei;DEND Xiao-zhong;NIE Shao-wu;School of Mechatronics Engineering;Henan University of Science and Technology;
..............page:195-200
Analysis of behavior mechanism and influential factors of load sharing in an epicyclic gear system
LIAO Ying-hua;QIN Da-tong;LIU Chang-zhao;State Key Laboratory of Mechanical Transmissions;College of Mechanical Engineering;Chongqing University;School of Mechanical Engineering;Sichuan University of Science and Engineering;
..............page:201-208
Spirac machine-tool setting calculation method by predetermined contact pattern length factor
XUAN Jia-min;WEI Wen-jun;LIU Ping-yi;DONG Xue-zhu;LI Hai-tao;College of Engineering;China Agricultural University;
..............page:209-218
Dynamic characteristics under various excitations for a helicopter transmission system
LIN He;WANG San-min;DONG Jin-cheng;School of Mechanical Engineering;Northwestern Polytechnical University;
..............page:219-227
Mechanism of improvement on axial-flow compressor stability with assembled casing treatment
ZHANG Hao-guang;WANG Yun-peng;WU Jun;CHU Wu-li;WU Yan-hui;School of Power and Energy;Northwestern Polytechnical University;Collaborative Innovation Center of Advanced Aero-Engine;
..............page:228-236
Low-speed modeling design for tip flow field of compressor rotor blade
LI Yan-kai;HUANG Tian-hao;MENG De-jun;MIAO Yu-lu;YU Wen-sheng;TENG Jin-fang;School of Aeronautics and Astronautics;Shanghai Jiao Tong University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:237-247
Large eddy simulation of unsteady flow field in a two-dimensional moving compressor cascade
ZHAO Long;GENG Shao-juan;ZHANG Hong-wu;Key Laboratory of Advanced Energy and Power;Institute of Engineering Thermophysics;Chinese Academy of Sciences;University of Chinese Academy of Sciences;
..............page:248-256