1000-8055
2016 Issue 4
..............page:764
Calibration technology of high-temperature thermocouple for combustor exit of an aero-engine
YANG Can;WU Wei-li;XIONG Yi-bin;YAO Zheng-rong;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
YANG Can;WU Wei-li;XIONG Yi-bin;YAO Zheng-rong;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:769-774
Experimental investigation of temperature measurement on the wall of flame tube for a triple combustor
XIONG Qing-rong;ZHU Guo-cheng;ZHONG Ming;China Gas Turbine Establishment;Aviation Industry Corporation of China;
XIONG Qing-rong;ZHU Guo-cheng;ZHONG Ming;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:775-779
Enhanced heat transfer characteristics in a large aspect ratio rectangular channel with inclined perforated rib
ZHU Qiang-hua;CUI Miao;GAO Xiao-wei;State Key Laboratory of Structural Analysis for Industrial Equipment;School of Aeronautics and Astronautics;Dalian University of Technology;
ZHU Qiang-hua;CUI Miao;GAO Xiao-wei;State Key Laboratory of Structural Analysis for Industrial Equipment;School of Aeronautics and Astronautics;Dalian University of Technology;
..............page:780-787
Charge-effect on the homo-heterogeneous condensing flow
CUI Ke;LIU Hua-ping;SONG Yan-ping;CHEN Huan-long;CHEN Fu;School of Energy Science and Engineering;Harbin Institute of Technology;
CUI Ke;LIU Hua-ping;SONG Yan-ping;CHEN Huan-long;CHEN Fu;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:788-799
Penetration characteristics and optimization of transverse jet on condition of vortex generator
ZHAO Yan-hui;LIANG Jian-han;YAN Tian-tian;Science and Technology of Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
ZHAO Yan-hui;LIANG Jian-han;YAN Tian-tian;Science and Technology of Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:800-806
Numerical study on the effect of parallel injection on film-cooling effectiveness at turbine blade tip
JIANG Wei;XIE Dan-mei;School of Power and Mechanical Engineering;Wuhan University;
JIANG Wei;XIE Dan-mei;School of Power and Mechanical Engineering;Wuhan University;
..............page:807-815
Influence of total temperature and pressure at the inlet of convergent exhaust system of turbofan engine on temperature distribution at plume centerline
WANG Feng;JI Hong-hu;YU Ming-fei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
WANG Feng;JI Hong-hu;YU Ming-fei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:816-822
Characteristics of the recirculation zone downstream a dual-swirl cup at varied inlet Reynolds numbers
YU Bo-wen;ZHANG Chi;YANG Qian;XU Quan-hong;LIN Yu-zhen;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
YU Bo-wen;ZHANG Chi;YANG Qian;XU Quan-hong;LIN Yu-zhen;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:823-829
Effects of film hole arrangement on central-cone cooling and infrared radiation characteristics of exhaust system
WANG Xu;ZHANG Jing-zhou;SHAN Yong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing Univerisity of Aeronautics and Astronautics;
WANG Xu;ZHANG Jing-zhou;SHAN Yong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing Univerisity of Aeronautics and Astronautics;
..............page:830-835
Boundary layer control of ultra-high-lift low pressure turbine blade with surface roughness
SUN Shuang;LEI Zhi-jun;LU Xin-gen;LI Wei;FU Yu;DONG Li-hui;Department of Aviation Engineering;Civil Aviation University of China;Gas Turbine Laboratory;Institute of Engineering Thermophyiscs;Chinese Academy of Sciences;
SUN Shuang;LEI Zhi-jun;LU Xin-gen;LI Wei;FU Yu;DONG Li-hui;Department of Aviation Engineering;Civil Aviation University of China;Gas Turbine Laboratory;Institute of Engineering Thermophyiscs;Chinese Academy of Sciences;
..............page:836-846
Experiment on variable tip clearance characteristics of compressor cascade with suction-side winglet
HAN Shao-bing;ZHONG Jing-jun;Marine Engineering College;Dalian Maritime University;
HAN Shao-bing;ZHONG Jing-jun;Marine Engineering College;Dalian Maritime University;
..............page:847-856
Effect of blade sweep on inlet flow in transonic compressor rotors
CHANG Hao;ZHU Fang;JIN Dong-hai;GUI Xing-min;Aero-engine Simulation Research Center;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shanghai Turbine Company Limited;Shanghai Electric Power Generation Group;
CHANG Hao;ZHU Fang;JIN Dong-hai;GUI Xing-min;Aero-engine Simulation Research Center;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shanghai Turbine Company Limited;Shanghai Electric Power Generation Group;
..............page:857-866
Mechanism for the effect of lean on the inlet flow of a single blade row
XU Han;ZHU Fang;JIN Dong-hai;GUI Xing-min;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Gas Turbine Technology Institute;Shanghai Electric Power Generation Research and Development Center;
XU Han;ZHU Fang;JIN Dong-hai;GUI Xing-min;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Gas Turbine Technology Institute;Shanghai Electric Power Generation Research and Development Center;
..............page:867-876
Occurrence mechanism of partial surge
PAN Tian-yu;SUN Tai-lu;LI Zhi-ping;LI Qiu-shi;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;
PAN Tian-yu;SUN Tai-lu;LI Zhi-ping;LI Qiu-shi;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:877-885
Influence of wakes on boundary layer stability in low-pressure turbines
LIANG Yun;LIU Huo-xing;ZOU Zheng-ping;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;
LIANG Yun;LIU Huo-xing;ZOU Zheng-ping;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:886-893
Numerical simulation on noise reduction for the cascade with trailing edge serrations
TONG Fan;QIAO Wei-yang;JI Liang;WANG Liang-feng;XU Kun-bo;WANG Xun-nian;School of Power and Energy;Northwestern Polytechnical University;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;
TONG Fan;QIAO Wei-yang;JI Liang;WANG Liang-feng;XU Kun-bo;WANG Xun-nian;School of Power and Energy;Northwestern Polytechnical University;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;
..............page:894-902
Design and test of a jet flap for a large amphibian
SUN Wei-ping;YANG Kang-zhi;QIN He-jun;General Configuration and Aerodynamics Design Department;China Aviation Industry General Aircraft Research Institute Corporation Limited;Aviation Industry Corporation of China;
SUN Wei-ping;YANG Kang-zhi;QIN He-jun;General Configuration and Aerodynamics Design Department;China Aviation Industry General Aircraft Research Institute Corporation Limited;Aviation Industry Corporation of China;
..............page:903-909
Numerical simulation for optimal design of wide angle diffuser in limited condition
CONG Cheng-hua;REN Ze-bin;YANG Gao-qiang;WANG Ning;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;Facility Design and Instrumentation Institute;China Aerodynamics Research and Development Center;
CONG Cheng-hua;REN Ze-bin;YANG Gao-qiang;WANG Ning;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;Facility Design and Instrumentation Institute;China Aerodynamics Research and Development Center;
..............page:910-917
Numerical investigation on influence of reverser flow to engine inlet flow field
WANG Zhi-qiang;SHEN Xi-gang;HU Jun;GAO Xiang;LIU Li-ping;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
WANG Zhi-qiang;SHEN Xi-gang;HU Jun;GAO Xiang;LIU Li-ping;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:918-926
Numerical solutions of adjoint Green’s function for complex geometries
XU Xi-hai;LI Xiao-dong;HU Fang-qiang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Department of Mathematics and Statistics;Old Dominion University;
XU Xi-hai;LI Xiao-dong;HU Fang-qiang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Department of Mathematics and Statistics;Old Dominion University;
..............page:927-933
Dynamic modeling of helicopter-flexible rope-slung load system based on Kanes method
WAN Shao-feng;CAO Yi-hua;HUANG Lei;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Research and Development Department;710Institute;China Shipbuilding Industry Corporation;The General Office;China Helicopter Research and Development Institute;Aviation Industry Corporation of China;
WAN Shao-feng;CAO Yi-hua;HUANG Lei;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Research and Development Department;710Institute;China Shipbuilding Industry Corporation;The General Office;China Helicopter Research and Development Institute;Aviation Industry Corporation of China;
..............page:934-940
Improved correction methods of aircraft engine fan speed based on similarity theory
XIA Cun-jiang;WANG Dan;Aero Engine Maintenance Training Center;Civil Aviation Flight University of China;Aviation Engineering Institute;Civil Aviation Flight University of China;
XIA Cun-jiang;WANG Dan;Aero Engine Maintenance Training Center;Civil Aviation Flight University of China;Aviation Engineering Institute;Civil Aviation Flight University of China;
..............page:941-947
Aero-engine performance seeking control based on DMOM algorithm
WANG Yuan;LI Qiu-hong;HUANG Xiang-hua;Aviation Motor Control System Institute;Aviation Industry Corporation of China;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;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:948-954
Estimation of unknown input observer disturbance matrix for fault diagnosis of turboshaft engine sensors
YANG Chao;WANG Xi;SHI Rui-jun;ZHOU Jian-bo;GAO Shi-huang;TAN Dao-liang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
YANG Chao;WANG Xi;SHI Rui-jun;ZHOU Jian-bo;GAO Shi-huang;TAN Dao-liang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:955-964
Turbo-shaft engine modeling method based on ADE-ELM
JIAO Yang;LI Qiu-hong;ZHU Zheng-chen;LIAO Guang-huang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
JIAO Yang;LI Qiu-hong;ZHU Zheng-chen;LIAO Guang-huang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:965-973
Reliability evaluation method based on failure data with poor information
XIA Xin-tao;ZHU Wen-huan;MENG Yan-yan;QIU Ming;School of Mechatronics Engineering;Henan University of Science and Technology;
XIA Xin-tao;ZHU Wen-huan;MENG Yan-yan;QIU Ming;School of Mechatronics Engineering;Henan University of Science and Technology;
..............page:974-985
Impact of support stiffness on dynamic load sharing characteristics of planetary train system
ZHU Zeng-bao;JIANG Zhi-xiang;YIN Min;College of Mechanical Engineering;Anhui University of Science and Technology;
ZHU Zeng-bao;JIANG Zhi-xiang;YIN Min;College of Mechanical Engineering;Anhui University of Science and Technology;
..............page:986-992
Reliability analysis of gear vibration based on dimensionality reduction visualization and Kriging
YANG Li;TONG Cao;School of Equipment Engineering;Shenyang Ligong University;Shengyang Institute of Automation;Chinese Academy of Sciences;
YANG Li;TONG Cao;School of Equipment Engineering;Shenyang Ligong University;Shengyang Institute of Automation;Chinese Academy of Sciences;
..............page:993-999
Flutter investigation of small aspect ratio compressor rotor blade
WU Chang-bo;ZHOU Bai-hao;LU Qing-fei;CUI Hai-tao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Gas Turbine Establishment;Aviation Industry Corporation of China;
WU Chang-bo;ZHOU Bai-hao;LU Qing-fei;CUI Hai-tao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:1000-1005
Experiment on mechanical properties of resin matrix composites laminates under various temperatures
SONG Jian;WEN Wei-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;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
SONG Jian;WEN Wei-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;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1006-1018
Self-pressurization modeling of nitrous oxide tank
SONG Chang-qing;XU Wan-wu;CHEN Jian;Science and Technology on Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
SONG Chang-qing;XU Wan-wu;CHEN Jian;Science and Technology on Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:1019-1024