1000-8055
2015 Issue 4
..............page:764
Field synergy analysis of highly-intensified piston oscillating cooling
ZHU Hai-rong;ZHANG Wei-zheng;YUAN Yan-peng;School of Mechanical Engineering;Beijing Institute of Technology;School of Mechanical Engineering;Hebei University of Science and Technology;
ZHU Hai-rong;ZHANG Wei-zheng;YUAN Yan-peng;School of Mechanical Engineering;Beijing Institute of Technology;School of Mechanical Engineering;Hebei University of Science and Technology;
..............page:769-774
Flow characteristics in a rotor-stator cavity with cooling air inlet at low radius
CAI Xu;LUO Xiang;ZHAO Xi;XU Guo-qiang;CAI Jun;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Department of Information Network;Dalian Airforce Communicaiton Non-Commissioned Office Academy;Guizhou Aero-Engine Research Institute;Aviation Industry Corporation of China;
CAI Xu;LUO Xiang;ZHAO Xi;XU Guo-qiang;CAI Jun;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Department of Information Network;Dalian Airforce Communicaiton Non-Commissioned Office Academy;Guizhou Aero-Engine Research Institute;Aviation Industry Corporation of China;
..............page:775-783
Infrared radiation characteristics of axisymmetrical ejector convergent nozzle in turbofan engine
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:784-792
Dynamic response characteristic of concentric stage swirling structure
QIN Hao;DING Zhi-lei;LIN Yu-zhen;LI Ji-bao;School of Energy and Power Engineering;Beijing University of Aeronautics of Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
QIN Hao;DING Zhi-lei;LIN Yu-zhen;LI Ji-bao;School of Energy and Power Engineering;Beijing University of Aeronautics of Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:793-799
Experiment and prediction of separation performance of hollow fiber membrane
SHAO Lei;LIU Wei-hua;SUN Bing;ZHAO Hong-tao;FENG Shi-yu;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Hefei Jianghang Aircraft Equipment Company Limited;Aviation Industry Corporation of China;
SHAO Lei;LIU Wei-hua;SUN Bing;ZHAO Hong-tao;FENG Shi-yu;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Hefei Jianghang Aircraft Equipment Company Limited;Aviation Industry Corporation of China;
..............page:800-806
Experiment on effect of dome and dilution holes on outlet temperature distribution for triple swirler combustor
DING Guo-yu;HE Xiao-min;XUE Chong;HONG Liang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
DING Guo-yu;HE Xiao-min;XUE Chong;HONG Liang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:807-813
Experiment of combustion performance in LPP low emission combustor with single dome
YAN Ying-wen;DANG Long-fei;DENG Yuan-hao;XU Rong;XU Hua-sheng;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;
YAN Ying-wen;DANG Long-fei;DENG Yuan-hao;XU Rong;XU Hua-sheng;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:814-822
Film cooling performance with internal coolant channel crossflow
JIA Guang-sen;ZHANG Li;LU Cong-ming;LUO Jian-xia;HUANG Xiao-yang;School of Power and Energy;Northwestern Polytechnical University;China Aviation Power Machinery Research Institute;Aviation Industry Corporation of China;
JIA Guang-sen;ZHANG Li;LU Cong-ming;LUO Jian-xia;HUANG Xiao-yang;School of Power and Energy;Northwestern Polytechnical University;China Aviation Power Machinery Research Institute;Aviation Industry Corporation of China;
..............page:823-830
Nozzle structure’ s influence on fuel flow oscillation in unsteady conditions
TANG Guan-qiong;QIN Hao;LI Lin;LIN Yu-zhen;LI Ji-bao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
TANG Guan-qiong;QIN Hao;LI Lin;LIN Yu-zhen;LI Ji-bao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:831-837
Secondary flow control in high-turning compressor cascade using vortex generator jet
LIU Hua-ping;CHEN Huan-long;LI De-xiong;GUO Yu-jie;CHENG Xiao-qi;CHEN Fu;Institute of Propulsion Theory and Technology;Harbin Institute of Technology;
LIU Hua-ping;CHEN Huan-long;LI De-xiong;GUO Yu-jie;CHENG Xiao-qi;CHEN Fu;Institute of Propulsion Theory and Technology;Harbin Institute of Technology;
..............page:838-845
Engineering research on prediction and suppression of blade flutter in compressor fan
SUN Hai;LI Jian;YANG Lin;CHEN Bao-shi;LIU Yi-xiong;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
SUN Hai;LI Jian;YANG Lin;CHEN Bao-shi;LIU Yi-xiong;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:846-853
Influence of tip clearance heights on the flow field and performances of a supersonic expander
HUANG Zhen-yu;ZHONG Jing-jun;YANG Ling;HAN Ji-ang;Marine Engineering College;Dalian Maritime University;
HUANG Zhen-yu;ZHONG Jing-jun;YANG Ling;HAN Ji-ang;Marine Engineering College;Dalian Maritime University;
..............page:854-864
Numerical simulation of effects of contoured slot seal configuration on turbine performance
ZHANG Jing-hui;MA Hong-wei;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHANG Jing-hui;MA Hong-wei;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:865-874
Relationship between optimum curved blade generate line and blade camber angle in linear compressor cascade
LING Jing;DU Xin;WANG Song-tao;WANG Zhong-qi;School of Energy Science and Engineering;Harbin Institute of Technology;
LING Jing;DU Xin;WANG Song-tao;WANG Zhong-qi;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:875-882
Characteristics under variant working conditions of a supersonic low-reaction aspirated compressor
ZHANG Long-xin;WANG Song-tao;RUAN Guo-hui;LIU Xun;WANG Zhong-qi;Engine Aerodynamics Research Centre;Harbin Institute of Technology;Harbin Boiler and Turbine Institute;China Shipbuilding Industry Corporation;
ZHANG Long-xin;WANG Song-tao;RUAN Guo-hui;LIU Xun;WANG Zhong-qi;Engine Aerodynamics Research Centre;Harbin Institute of Technology;Harbin Boiler and Turbine Institute;China Shipbuilding Industry Corporation;
..............page:883-890
Optimized profile of high subsonic axial flow compressor
CHEN Zhong-liang;JIANG Bin;ZHENG Qun;ZHANG Xiao-long;TAN Chun-lai;College of Power and Energy Engineering;Harbin Engineering University;
CHEN Zhong-liang;JIANG Bin;ZHENG Qun;ZHANG Xiao-long;TAN Chun-lai;College of Power and Energy Engineering;Harbin Engineering University;
..............page:891-900
Effect of inlet preswirl on the aerothermodynamic performance of splitter mixing exhaust system
WU Fei;XIE Yi;SHAO Wan-ren;LIU Kun;RUAN Deng-fang;ZHENG Biao;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;The State Key Laboratory of Mechanical Transmissions;Chongqing University;College of Automotive Engineering;Chongqing University;
WU Fei;XIE Yi;SHAO Wan-ren;LIU Kun;RUAN Deng-fang;ZHENG Biao;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;The State Key Laboratory of Mechanical Transmissions;Chongqing University;College of Automotive Engineering;Chongqing University;
..............page:901-909
Air bridge technology for engine power simulation test in wind tunnel
ZHANG Rong-ping;WANG Xun-nian;HUANG Yong;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;Low Speed Aerodynamics Institute;China Aerodynamics Research and Development Center;
ZHANG Rong-ping;WANG Xun-nian;HUANG Yong;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;Low Speed Aerodynamics Institute;China Aerodynamics Research and Development Center;
..............page:910-915
Effect of lobe number on aerothermodynamic performance of lobed S-shaped two-dimensional nozzle
DU Li-wei;LIU You-hong;SHAO Wan-ren;XU Su;DENG Hong-wei;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
DU Li-wei;LIU You-hong;SHAO Wan-ren;XU Su;DENG Hong-wei;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:916-926
Prediction model of cross-flow instability transition in swept wing boundary layers
XU Jia-kuan;BAI Jun-qiang;QIAO Lei;HUANG Jiang-tao;School of Aeronautics;Northwestern Polytechnical University;Department of General;China Aerodynamics Research and Development Center;
XU Jia-kuan;BAI Jun-qiang;QIAO Lei;HUANG Jiang-tao;School of Aeronautics;Northwestern Polytechnical University;Department of General;China Aerodynamics Research and Development Center;
..............page:927-935
Numerical simulation of implicit fully coupled SST and TNT turbulence models for high speed flows
XIA Chen-chao;CHEN Wei-fang;GUO Zhong-zhou;NIE Liang;School of Aeronautics and Astronautics;Zhejiang University;
XIA Chen-chao;CHEN Wei-fang;GUO Zhong-zhou;NIE Liang;School of Aeronautics and Astronautics;Zhejiang University;
..............page:936-943
Modeling of hypersonic vehicles propulsion system
XIAO Di-bo;LU Yu-ping;YAO Ke-ming;LIU Yan-bin;CHEN Bo-yi;College of Astronautics;Nanjing University of Aeronautics and Astronautics;College of Electrical and Information Engineering;Jiangsu University of Technology;
XIAO Di-bo;LU Yu-ping;YAO Ke-ming;LIU Yan-bin;CHEN Bo-yi;College of Astronautics;Nanjing University of Aeronautics and Astronautics;College of Electrical and Information Engineering;Jiangsu University of Technology;
..............page:944-951
A new blade-casing rubbing model and its verification
CHEN Guo;WANG Hai-fei;LIU Yong-quan;FENG Guo-quan;JIANG Guang-yi;LI Cheng-gang;WANG De-you;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
CHEN Guo;WANG Hai-fei;LIU Yong-quan;FENG Guo-quan;JIANG Guang-yi;LI Cheng-gang;WANG De-you;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:952-965
Damping mechanism of floating ring squeeze film damper
ZHOU Hai-lun;FENG Guo-quan;LUO Gui-huo;AI Yan-ting;Liaoning Key Laboratory of Advanced Test Technology for Aerospace Propulsion System;Faculty of Aerospace Engineering;Shenyang Aerospace University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
ZHOU Hai-lun;FENG Guo-quan;LUO Gui-huo;AI Yan-ting;Liaoning Key Laboratory of Advanced Test Technology for Aerospace Propulsion System;Faculty of Aerospace Engineering;Shenyang Aerospace University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:966-971
Experiment on vibration control of rotor with ring dynamic vibration absorber
ZHANG Bing-kang;HE Li-dong;YANG Xiu-feng;ZHANG Zhen-kun;Engineering Research Center of Chemical Safety;College of Mechanical and Electrical Engineering;Beijing University of Chemical Technology;
ZHANG Bing-kang;HE Li-dong;YANG Xiu-feng;ZHANG Zhen-kun;Engineering Research Center of Chemical Safety;College of Mechanical and Electrical Engineering;Beijing University of Chemical Technology;
..............page:972-978
Frequency domain optimal tuning method of PI control parameters for aero-engine
HUANG Jin-quan;LIU Nan;TANG Yu-ting;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaboration Innovation Center for Advanced Aero-Engine;Shanghai Aircraft Design and Research Institute;Commercial Aircraft Corporation of China Limited;
HUANG Jin-quan;LIU Nan;TANG Yu-ting;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaboration Innovation Center for Advanced Aero-Engine;Shanghai Aircraft Design and Research Institute;Commercial Aircraft Corporation of China Limited;
..............page:979-984
LQ/H_∞ controller design for aero-engine based on improved NSGAⅡ
WANG Yuan;LI Qiu-hong;HUANG Xiang-hua;WU Qian;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
WANG Yuan;LI Qiu-hong;HUANG Xiang-hua;WU Qian;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:985-991
Influential factors of nozzle performance of hot water rocket motor
SUN Wei-wei;WEI Zhi-jun;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
SUN Wei-wei;WEI Zhi-jun;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:992-998
Experiment on thrust adjustment characteristics of fluidic nozzle throat
GUO Chang-chao;YU Xin-yu;LI Bo;XIE Kan;WEI Zhi-jun;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;Beijing Aerospace Propulsion Institute;China Aerospace Science and Technology Corporation;
GUO Chang-chao;YU Xin-yu;LI Bo;XIE Kan;WEI Zhi-jun;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;Beijing Aerospace Propulsion Institute;China Aerospace Science and Technology Corporation;
..............page:999-1007
Mixed lubrication analysis in finite tooth contact surface of filtering reducer
PU Wei;WANG Jia-xu;ZHOU Guang-wu;LI Jun-yang;QIN De-cheng;School of Aeronautics and Astronautics;Sichuan University;Institute of Electromechanical Transmission and Delivery Equipment;Chongqing University;
PU Wei;WANG Jia-xu;ZHOU Guang-wu;LI Jun-yang;QIN De-cheng;School of Aeronautics and Astronautics;Sichuan University;Institute of Electromechanical Transmission and Delivery Equipment;Chongqing University;
..............page:1008-1015
Design of disturbance rejection control system for 5-DOF magnetic bearing
LI Ke-xiang;DENG Zhi-quan;LIU Cheng-zi;HUA Chun;College of Automation Engineering;Nanjing University of Aeronautics and Astronautics;
LI Ke-xiang;DENG Zhi-quan;LIU Cheng-zi;HUA Chun;College of Automation Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1016-1024