1000-8055
2016 Issue 8
Design and performance test of a kind of three-blade propeller
XIANG Song;TONG Gang;WU Jiang;ZHAO Wei-ping;YANG Kang;WANG Ji;Liaoning Key Laboratory of General Aviation;Shenyang Aerospace University;Management Office of Science and Research;Liaoning General Aviation Academy;
XIANG Song;TONG Gang;WU Jiang;ZHAO Wei-ping;YANG Kang;WANG Ji;Liaoning Key Laboratory of General Aviation;Shenyang Aerospace University;Management Office of Science and Research;Liaoning General Aviation Academy;
..............page:1793-1798
Numerical investigation of geometric parameters’ influence to aerodynamic performance of two dimensional convergent and divergent nozzle
SHI Xiao-juan;JI Hong-hu;SI Ren;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;SI Ren;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1799-1810
Numerical simulation of powered high-lift jet effects for large transport
GONG Zhi-bin;LI Jie;JIANG Sheng-ju;ZHANG Heng;School of Aeronautics;Northwestern Polytechnical University;Xi’an Modern Control Technology Research Institute;China North Industries Group Corporation;
GONG Zhi-bin;LI Jie;JIANG Sheng-ju;ZHANG Heng;School of Aeronautics;Northwestern Polytechnical University;Xi’an Modern Control Technology Research Institute;China North Industries Group Corporation;
..............page:1811-1819
Aeroelastic analysis of rotor airfoil based on CFD/CSD tight coupling method
HUANG Dao-bo;LI Jian-dong;LIU Yong;National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics;Nanjing University of Aeronautics and Astronautics;Xi’an Advanced Dynamics Technology Incorporation;
HUANG Dao-bo;LI Jian-dong;LIU Yong;National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics;Nanjing University of Aeronautics and Astronautics;Xi’an Advanced Dynamics Technology Incorporation;
..............page:1820-1829
Effect of forced-transition on performance of hypersonic inlet
YI Miao-rong;ZHAO Hui-yong;LE Jia-ling;Science and Technology on Scramjet Laboratory;Hypersonic Aerodynamics Research Institute;China Aerodynamics Research and Development Center;
YI Miao-rong;ZHAO Hui-yong;LE Jia-ling;Science and Technology on Scramjet Laboratory;Hypersonic Aerodynamics Research Institute;China Aerodynamics Research and Development Center;
..............page:1830-1837
Design of an ornithopter with multisection flexible morphing wings
HUANG Ming-yang;XIAO Tian-hang;ANG Hai-song;Ministerial Key Discipline Laboratory of Advanced Design Technology of Aircraft;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
HUANG Ming-yang;XIAO Tian-hang;ANG Hai-song;Ministerial Key Discipline Laboratory of Advanced Design Technology of Aircraft;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1838-1844
Experiment for improving aerodynamic performances of a flying wing by millisecond pulsed plasma actuation
MA Jie;LIANG Hua;WU Yun;HAN Meng-hu;WEI Biao;ZHAO Guang-yin;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
MA Jie;LIANG Hua;WU Yun;HAN Meng-hu;WEI Biao;ZHAO Guang-yin;Science and Technology on Plasma Dynamics Laboratory;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:1845-1851
Experiment and numerical computation of impingement cooling in narrow space with pin fins
RAO Yu;WAN Chao-yi;CHEN Peng;Institute of Turbomachinery;School of Mechanical Engineering;Shanghai Jiao Tong University;
RAO Yu;WAN Chao-yi;CHEN Peng;Institute of Turbomachinery;School of Mechanical Engineering;Shanghai Jiao Tong University;
..............page:1852-1859
Influence of indirect initiation on the thermal efficiency of pulsed detonation engine
QIU Hua;WANG Wei;XIONG Cha;School of Power and Energy;Northwestern Polytechnical University;Xi’an Thermal Power Research Institute Company Limited;China Huaneng Group;
QIU Hua;WANG Wei;XIONG Cha;School of Power and Energy;Northwestern Polytechnical University;Xi’an Thermal Power Research Institute Company Limited;China Huaneng Group;
..............page:1860-1865
Pressure loss characteristics in a rotating cavity with de-swirled nozzles
HU Yan-li;GUO Wen;WANG Lei;LUO Xiang;China Gas Turbine Establishment;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
HU Yan-li;GUO Wen;WANG Lei;LUO Xiang;China Gas Turbine Establishment;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1866-1873
Studies on combustion and emission characteristics of coal-based jet fuel in ground individual can combustor
YANG Wen;ZHANG Dong-mei;CAO Wen-jie;WU Xiu-zhang;WANG Shu-lei;China Shenhua Coal to Liquid and Chemical Co.;Ltd.;State Key Laboratory of Heavy Oil Processing;China University of Petroleum;Beijing Research Institute of Aviation Oil;
YANG Wen;ZHANG Dong-mei;CAO Wen-jie;WU Xiu-zhang;WANG Shu-lei;China Shenhua Coal to Liquid and Chemical Co.;Ltd.;State Key Laboratory of Heavy Oil Processing;China University of Petroleum;Beijing Research Institute of Aviation Oil;
..............page:1874-1882
Effect of carbon deposit removing hole area on the outlet flow field of double-swirler
ZHENG Jian-wen;SONG Shuang-wen;PENG Jian-yong;LIU Tao;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
ZHENG Jian-wen;SONG Shuang-wen;PENG Jian-yong;LIU Tao;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:1883-1888
Numerical investigation of convective heat transfer on a wedge-shaped concave surface subjected to staggered offset impinging jets
GUAN Tao;ZHANG Jing-zhou;SHAN Yong;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;
GUAN Tao;ZHANG Jing-zhou;SHAN Yong;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:1889-1896
Reliability model of aero-engine structural system
HONG Jie;ZHANG Zi;XU Xiao-li;MA Yan-hong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
HONG Jie;ZHANG Zi;XU Xiao-li;MA Yan-hong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1897-1904
Equivalent modeling and vibration isolation design of wing-mounted engine structure
XU Fei;HE Er-ming;LI Jing-xu;School of Aeronautics;Northwestern Polytechnical University;
XU Fei;HE Er-ming;LI Jing-xu;School of Aeronautics;Northwestern Polytechnical University;
..............page:1905-1912
Thermal-structural coupling characteristics of axial piston pump slipper pair
TANG He-sheng;YIN Yao-bao;LI Jing;School of Mechanical Engineering;Tongji University;
TANG He-sheng;YIN Yao-bao;LI Jing;School of Mechanical Engineering;Tongji University;
..............page:1913-1920
Non-deformability evaluation of aero-engine’s case
XU Feng;MA Yan-hong;ZHANG Li;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
XU Feng;MA Yan-hong;ZHANG Li;HONG Jie;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1921-1928
Component mode synthesis for dynamic reduction of 3-D finite element rotor system and its application
ZUO Yan-fei;WANG Jian-jun;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZUO Yan-fei;WANG Jian-jun;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1929-1934
Experiment and numerical simulation of external performances and internal flow of a molten salt pump
SHAO Chun-lei;GU Bo-qin;ZHOU Jian-feng;CHENG Wen-jie;School of Mechanical and Power Engineering;Nanjing Tech University;
SHAO Chun-lei;GU Bo-qin;ZHOU Jian-feng;CHENG Wen-jie;School of Mechanical and Power Engineering;Nanjing Tech University;
..............page:1935-1942
Study on improvement of the compressor anti-swirl distortion capacity with bowed stator
TU Bao-feng;LIU Hua;HU Jun;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;LIU Hua;HU Jun;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:1943-1949
Effect of tip clearance on the operating mechanism of offset splitter blades in a centrifugal compressor
CHEN Jie;HE Min-xiang;HUANG Guo-ping;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
CHEN Jie;HE Min-xiang;HUANG Guo-ping;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1950-1956
Experiment on surge phenomenon of small multi-stage axial compressor
HE Xiang;MA Hong-wei;YIN Yue-qian;SHAN Xiao-ming;YAO Zheng-rong;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;Collaborative Innovation Center for Advanced Aero-Engine;
HE Xiang;MA Hong-wei;YIN Yue-qian;SHAN Xiao-ming;YAO Zheng-rong;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;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1957-1963
Aero-elastic stability analysis of an axial compressor with splitter rotor
HUANG Zhong-shan;WANG Yan-rong;FU Zhi-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
HUANG Zhong-shan;WANG Yan-rong;FU Zhi-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1964-1972
Review of research on solid fuel scramjet engine
L Zhong;XIA Zhi-xun;LIU Bing;LIU Yuan-chun;Science and Technology on Scramjet Laboratory;National University of Defense Technology;College of Aerospace Science and Engineering;National University of Defense Technology;
L Zhong;XIA Zhi-xun;LIU Bing;LIU Yuan-chun;Science and Technology on Scramjet Laboratory;National University of Defense Technology;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:1973-1984
Influence of combustor shape on self-ignition in solid fuel scramjet
CHI Hong-wei;WEI Zhi-jun;LI Biao;WANG Li-he;WANG Ning-fei;School of Aerospace;Beijing Institute of Technology;
CHI Hong-wei;WEI Zhi-jun;LI Biao;WANG Li-he;WANG Ning-fei;School of Aerospace;Beijing Institute of Technology;
..............page:1985-1994
Impact effect of liquid rocket motor exhaust plume on launching platform
CAI Hong-hua;NIE Wan-sheng;HOU Zhi-yong;Department of Aerospace Equipment;The Academy of Equipment;
CAI Hong-hua;NIE Wan-sheng;HOU Zhi-yong;Department of Aerospace Equipment;The Academy of Equipment;
..............page:1995-2001
On-orbit refilling technologies and schemes of liquid propellant
WANG Lei;LI Yan-zhong;MA Yuan;XIE Fu-shou;School of Energy and Power Engineering;Xi’an Jiaotong University;State Key Laboratory of Technologies in Space Cryogenic Propellants;
WANG Lei;LI Yan-zhong;MA Yuan;XIE Fu-shou;School of Energy and Power Engineering;Xi’an Jiaotong University;State Key Laboratory of Technologies in Space Cryogenic Propellants;
..............page:2002-2009
Coupling of dynamics and elastohydrodynamic lubrication for spur gear
ZOU Yu-jing;CHANG De-gong;College of Electromechanical Engineering;Qingdao University of Science and Technology;
ZOU Yu-jing;CHANG De-gong;College of Electromechanical Engineering;Qingdao University of Science and Technology;
..............page:2010-2020
Studies on the effects of structural parameters on jet characteristics of nozzlesin in lubricating aviation gears
ZHANG Rui-qiang;LIU Shao-jun;HU Xiao-zhou;School of Mechanical and Electrical Engineering;Central South University;State Key Laboratory for High Performance Complex Manufacturing;Central South University;
ZHANG Rui-qiang;LIU Shao-jun;HU Xiao-zhou;School of Mechanical and Electrical Engineering;Central South University;State Key Laboratory for High Performance Complex Manufacturing;Central South University;
..............page:2021-2028
Research on model-based safety analysis for aero-engine
BAO Meng-yao;LI Guo;DING Shui-ting;Department of Aircraft Airworthiness Certification;Civil Aviation Management Institute 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;
BAO Meng-yao;LI Guo;DING Shui-ting;Department of Aircraft Airworthiness Certification;Civil Aviation Management Institute 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:2029-2039
Intermediate state control of turbofan engine in full envelope based on switched polytopic LPV approach
WU Bin;HUANG Jin-quan;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;
WU Bin;HUANG Jin-quan;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:2040-2048