1000-8055
2013 Issue 9
xian jin de liu chang ce liang ji shu tong shi ce liang su du chang wen du chang ya li chang he mi du chang de s.a.f.e ji shu
fu ting huang ;
fu ting huang ;
..............page:1914
..............page:1915
..............page:1916
Thermal protection of scramjet typical components
JIANG Jin;ZHANG Ruo-ling;YANG Yang;LIU Wei-xiong;Science and Technology on Scramjet Laboratory;Hypervelocity Aerodynamics Institute;China Aerodynamic Research and Development Center;Airbreathing Hypersonic Technology Research Center;China Aerodynamic Research and Development Center;
JIANG Jin;ZHANG Ruo-ling;YANG Yang;LIU Wei-xiong;Science and Technology on Scramjet Laboratory;Hypervelocity Aerodynamics Institute;China Aerodynamic Research and Development Center;Airbreathing Hypersonic Technology Research Center;China Aerodynamic Research and Development Center;
..............page:1921-1926
Experiment on heat transfer enhancement of barium hydroxide octahydrate phase change material
SHENG Qiang;XING Yu-ming;WANG Ze;School of Aeronautics Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Civil Engineering;Heilongjiang University;
SHENG Qiang;XING Yu-ming;WANG Ze;School of Aeronautics Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Civil Engineering;Heilongjiang University;
..............page:1927-1932
Experiment of swirled air effect on spray characteristic of double-line pressure-swirl atomizer
ZHOU Bing;JI Hong-hu;ZHANG Bao-cheng;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;College of Energy and Power Engineering;Shenyang University of Aeronautics and Astronautics;
ZHOU Bing;JI Hong-hu;ZHANG Bao-cheng;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;College of Energy and Power Engineering;Shenyang University of Aeronautics and Astronautics;
..............page:1933-1941
Infrared radiation characteristics of exhaust system using temperature corrected k-ε model
LI Xi-xi;Eriqitai;ZHU Xi-juan;WU Meng;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;The Second Academy of China Aerospace Science and Industry Corporation;Science and Technology on Optical Radiation Laboratory;Chengdu Engine Company Limited;Aviation Industry Corporation of China;
LI Xi-xi;Eriqitai;ZHU Xi-juan;WU Meng;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;The Second Academy of China Aerospace Science and Industry Corporation;Science and Technology on Optical Radiation Laboratory;Chengdu Engine Company Limited;Aviation Industry Corporation of China;
..............page:1942-1948
Experiment of heat transfer in oscillating turbulent flow in a pipe with constant heat flux
LI Ming-zhen;DONG Jin-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
LI Ming-zhen;DONG Jin-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1949-1955
Experiment of transpiration cooling rules of single phase liquid
XIONG Yan-bin;ZHU Yin-hai;JIANG Pei-xue;HUANG Zheng;LIU Yuan-qing;Key Laboratory for Thermal Science and Power Engineering of Ministry of Education;Department of Thermal Engineering;Tsinghua University;Beijing Institute of Astronautical System Engineering;
XIONG Yan-bin;ZHU Yin-hai;JIANG Pei-xue;HUANG Zheng;LIU Yuan-qing;Key Laboratory for Thermal Science and Power Engineering of Ministry of Education;Department of Thermal Engineering;Tsinghua University;Beijing Institute of Astronautical System Engineering;
..............page:1956-1961
Numerical simulation of characteristic of hypersonic ablation flow field containing alkali-metal impurities
CHAI Dong;FANG Yang-wang;TONG Zhong-xiang;GAO Xiang;School of Aeronautic and Astronautic Engineering;Air Force Engineering University;
CHAI Dong;FANG Yang-wang;TONG Zhong-xiang;GAO Xiang;School of Aeronautic and Astronautic Engineering;Air Force Engineering University;
..............page:1962-1966
Self-sustaining mechanism of detonation wave influenced by lateral expansion
ZHOU Zhu-lin;LIU Wei-dong;LIU Shi-jie;LIN Zhi-yong;Science and Technology on Scramjet Laboratory;College of Space Science and Engineering;National University of Defense Technology;
ZHOU Zhu-lin;LIU Wei-dong;LIU Shi-jie;LIN Zhi-yong;Science and Technology on Scramjet Laboratory;College of Space Science and Engineering;National University of Defense Technology;
..............page:1967-1974
Numerical simulation and analysis of leaf seal leakage flow
LIANG Ya-kun;WANG Zhi-li;WANG Wei;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;Lubrication Laboratory;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
LIANG Ya-kun;WANG Zhi-li;WANG Wei;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;Lubrication Laboratory;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1975-1981
Mechanism of film cooling efficiency enhancement by horseshoe plasma actuator
DAI Sheng-ji;HE Li-ming;DING Wei;JIN Tao;DU Hong-liang;College of Aeronautics and Astronautics Engineering;Air Force Engineering University;Department of Training;Air Force Engineering University;95997 unit of People’s Liberation Army;
DAI Sheng-ji;HE Li-ming;DING Wei;JIN Tao;DU Hong-liang;College of Aeronautics and Astronautics Engineering;Air Force Engineering University;Department of Training;Air Force Engineering University;95997 unit of People’s Liberation Army;
..............page:1982-1987
Numerical calculation of dynamic performance of low-bypass ratio turbofan engine
TIAN Jin-hu;QIAO Wei-yang;PENG Sheng-hong;School of Power and Energy;Northwestern Polytechnical University;Aviation Key Laboratory of Science and Technology on Aero-engine Altitude Simulating;China Gas Turbine Establishment;Aviation Industry Corporation of China;
TIAN Jin-hu;QIAO Wei-yang;PENG Sheng-hong;School of Power and Energy;Northwestern Polytechnical University;Aviation Key Laboratory of Science and Technology on Aero-engine Altitude Simulating;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:1988-1996
Correction method of influence of simulation bias on performance of turboshaft engine test in ATF
MA Qian-rong;WU Hu;LIU Tao;ZHOU Wen-xiang;School of Power and Energy;Northwest Polytechnical University;Aero-engine Altitude Simulated Key Laboratory;China Gas Turbine Establishment;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
MA Qian-rong;WU Hu;LIU Tao;ZHOU Wen-xiang;School of Power and Energy;Northwest Polytechnical University;Aero-engine Altitude Simulated Key Laboratory;China Gas Turbine Establishment;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1997-2002
Solving transient second air system in engine by characteristics method
WU Hong;HU Xiao-xiao;National Key Laboratory of Science and Technology on Aero-engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
WU Hong;HU Xiao-xiao;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:2003-2008
Aerodynamic optimization design of wing-body-nacelle-pylon configuration
ZUO Ying-tao;FU Lin;GAO Zheng-hong;SHAO Qi-lin;BAI Jun-qiang;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;Safety Department of Hainan Airlines Company Limited;
ZUO Ying-tao;FU Lin;GAO Zheng-hong;SHAO Qi-lin;BAI Jun-qiang;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;Safety Department of Hainan Airlines Company Limited;
..............page:2009-2015
Tilt-rotor aircraft modeling and its manipulation assignment strategy
XIA Qing-yuan;XU Jin-fa;JIN Kai-bao;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
XIA Qing-yuan;XU Jin-fa;JIN Kai-bao;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2016-2028
Regression study of scramjet nozzle performance on contour parameters
ZHANG Wen-dian;WANG Yi-bai;LIU Yu;QIN Li-zi;ZHANG Xiao-yuan;HE Miao-sheng;School of Astronautics;Beijing University of Aeronautics and Astronautics;
ZHANG Wen-dian;WANG Yi-bai;LIU Yu;QIN Li-zi;ZHANG Xiao-yuan;HE Miao-sheng;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:2029-2036
Numerical simulation of flow field and handling aerodynamic characteristics of ram-air parachute
ZHANG Chun;YANG Qian;YUAN Meng;CAO Yi-hua;School of Astronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Library of Beijing Institute of Space Scientific and Technological Information;The Ninth System Design Department;The Fourth Research Academy;China Aerospace Science and Technology Corporation;
ZHANG Chun;YANG Qian;YUAN Meng;CAO Yi-hua;School of Astronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Library of Beijing Institute of Space Scientific and Technological Information;The Ninth System Design Department;The Fourth Research Academy;China Aerospace Science and Technology Corporation;
..............page:2037-2043
Bistable vibration characteristics of disk-rod-fastening rotor with squeeze film dumper
CHENG Li;LI Shuai-ying;QIAN Zheng-wen;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
CHENG Li;LI Shuai-ying;QIAN Zheng-wen;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2044-2049
Multiple damages detection of structure based on hierarchical genetic algorithm
FAN De-li;ZHENG Shi-jie;WANG Hong-tao;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautic;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
FAN De-li;ZHENG Shi-jie;WANG Hong-tao;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautic;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2050-2054
Literature survey of rub-impact model and experiment of rotating blade and casing
MA Hui;TAI Xing-yu;LI Huan-jun;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;
MA Hui;TAI Xing-yu;LI Huan-jun;WEN Bang-chun;School of Mechanical Engineering and Automation;Northeastern University;
..............page:2055-2069
Experiment on single bolted joints in laminates under multilevel fatigue loading
WANG Dan-yong;WEN Wei-dong;The Institute 53;China North Industries Group Corporation;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
WANG Dan-yong;WEN Wei-dong;The Institute 53;China North Industries Group Corporation;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2070-2075
Effect of mistuned bladed-disk induced by cracked blades on vibration characteristics of aero-engine
ZHANG Huan;ZHU Jing;LIANG En-bo;TENG Guang-rong;China Gas Turbine Establishment;Aviation Industry Corporation of China;
ZHANG Huan;ZHU Jing;LIANG En-bo;TENG Guang-rong;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:2076-2082
A parametric lightweight turbine disk structure CAD/CAE integration method
LUO Bin;DING Shui-ting;LI Guo;Airworthiness Technologies Research Center;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
LUO Bin;DING Shui-ting;LI Guo;Airworthiness Technologies Research Center;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:2083-2089
Bi-directional evolutionary structural optimization method based on self-adaption and random sampling sensitivity analysis
SONG Jian;WEN Wei-dong;ZHANG Hong-jian;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
SONG Jian;WEN Wei-dong;ZHANG Hong-jian;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2090-2099
Influence of fuel injection position and equivalent mixture ratio on chemical non-equilibrium effects of single expansion ramp nozzle
CHENG Cheng;WANG Yi-bai;LIU Yu;QIN Li-zi;School of Astronautics;Beijing University of Aeronautics and Astronautics;
CHENG Cheng;WANG Yi-bai;LIU Yu;QIN Li-zi;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:2100-2111
Research on stability of reverse unloading diaphragm pressure reducing regulator using BP neural network model
CHEN Jing-lu;WANG Yong-jun;CHEN Yang;School of Mathematics and Systems Science;Beijing University of Aeronautics and Astronautics;School of Astronautics;Beijing University of Aeronautics and Astronautics;
CHEN Jing-lu;WANG Yong-jun;CHEN Yang;School of Mathematics and Systems Science;Beijing University of Aeronautics and Astronautics;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:2112-2120
Analysis on variable nozzle turbine performance influenced by multiple factors under pulsating flow conditions
ZHANG Rui;SHI Xin;YANG Ce;MA Chao-chen;QI Ming-xu;School of Mechanical Engineering;Beijing Institute of Technology;
ZHANG Rui;SHI Xin;YANG Ce;MA Chao-chen;QI Ming-xu;School of Mechanical Engineering;Beijing Institute of Technology;
..............page:2121-2128
Experiment of flow separation control in highly loaded compressor cascade corner by endwall plasma aerodynamic actuation
ZHAO Qin;WU Yun;LI Ying-hong;ZHAO Xiao-hu;ZHANG Hai-deng;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
ZHAO Qin;WU Yun;LI Ying-hong;ZHAO Xiao-hu;ZHANG Hai-deng;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2129-2139
System-in-package technology for miniaturization design of aero-engine electronic control system
LIU Bao-hua;HUANG Jin-quan;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;
LIU Bao-hua;HUANG Jin-quan;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;
..............page:2140-2144
High stability control of engine based on surge margin estimation model
WANG Jian-kang;ZHANG Hai-bo;CHEN Ke;SUN Feng-yong;ZHOU Xiao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Beijing Institute of Control Engineering;China Academy of Space Technology;
WANG Jian-kang;ZHANG Hai-bo;CHEN Ke;SUN Feng-yong;ZHOU Xiao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Beijing Institute of Control Engineering;China Academy of Space Technology;
..............page:2145-2154
Calculation of mean friction coefficient in scuffing strength for gear drive with meshing beyond pitch point
SUN Yong-zheng;ZHU Ru-peng;BAO He-yun;Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
SUN Yong-zheng;ZHU Ru-peng;BAO He-yun;Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2155-2160