1000-8055
2015 Issue 10
..............page:2300
Structural design and optimization for the deformation approaching to hot pofile of a swept fan blade with smaller hub-to-tip ratio
WANG Yan-rong;HUANG Zhong-shan;FU Zhi-zhong;SHI Liang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
WANG Yan-rong;HUANG Zhong-shan;FU Zhi-zhong;SHI Liang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2305-2311
Approach to construction of fatigue design curve
YANG Xiao-guang;HUANG Fei;MIAO Guo-lei;SHI Duo-qi;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
YANG Xiao-guang;HUANG Fei;MIAO Guo-lei;SHI Duo-qi;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2312-2317
Nonlinear and non-Guassian rank filter method
FU Hui-min;XIAO Qiang;LOU Tai-shan;XIAO Meng-li;Research Center of Small Sample Technology;Beijing University of Aeronautics and Astronautics;
FU Hui-min;XIAO Qiang;LOU Tai-shan;XIAO Meng-li;Research Center of Small Sample Technology;Beijing University of Aeronautics and Astronautics;
..............page:2318-2322
Experiment of surface finishing on aero-engine blisk by magnetic abrasive finishing
CHEN Yan;ZHOU Kun;NIU Feng-li;LI Chang;Institute of Advanced Grinding Technology;School of Mechanical Engineering and Automation;University of Science and Technology Liaoning;
CHEN Yan;ZHOU Kun;NIU Feng-li;LI Chang;Institute of Advanced Grinding Technology;School of Mechanical Engineering and Automation;University of Science and Technology Liaoning;
..............page:2323-2330
Influence of different impact energies on damage and residual strength of laminates
CUI Hai-po;WEN Wei-dong;ZHANG A-long;Shanghai Institute for Minimally Invasive Therapy;University of Shanghai for Science and Technology;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
CUI Hai-po;WEN Wei-dong;ZHANG A-long;Shanghai Institute for Minimally Invasive Therapy;University of Shanghai for Science and Technology;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2331-2337
Probabilistic failure risk assessment method of turbine engine life limited parts for airworthiness requirements
ZHANG Gong;ZHOU Yan-pei;DING Shui-ting;Engine Certification Center;Civil Aviation Administration of China;Aeroengine Airworthiness Certification Center Preparatory Office;China Academy of Civil Aviation Science and Technology;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHANG Gong;ZHOU Yan-pei;DING Shui-ting;Engine Certification Center;Civil Aviation Administration of China;Aeroengine Airworthiness Certification Center Preparatory Office;China Academy of Civil Aviation Science and Technology;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2338-2345
Contact pressure analysis by using singular integral equation method
LIU Chuang;CUI Hai-tao;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Areonautics and Astronautics;
LIU Chuang;CUI Hai-tao;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Areonautics and Astronautics;
..............page:2346-2351
Reliability evaluation method of ion thruster with very few failure data
LI Jun-xing;ZHANG Yong-bo;FU Hui-min;WANG Zhi-hua;Research Center of Small Sample Technology;Beijing University of Aeronautics and Astronautics;
LI Jun-xing;ZHANG Yong-bo;FU Hui-min;WANG Zhi-hua;Research Center of Small Sample Technology;Beijing University of Aeronautics and Astronautics;
..............page:2352-2356
General weight functions for corner quarter-elliptical crack in three-dimensional rectangular plate
JIA Xu;HU Xu-teng;SONG Ying-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;Nanjing University of Aeronautics and Astronautics;
JIA Xu;HU Xu-teng;SONG Ying-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;Nanjing University of Aeronautics and Astronautics;
..............page:2357-2367
Combustion characteristics for direct injection piston aviation engine
HU Chun-ming;GU Jun;ZHOU Hao;Internal Combustion Engine Research Institute;Tianjin University;Stake Key Laboratory of Engines;Tianjin University;
HU Chun-ming;GU Jun;ZHOU Hao;Internal Combustion Engine Research Institute;Tianjin University;Stake Key Laboratory of Engines;Tianjin University;
..............page:2368-2375
Heat transfer enhancement mechanism of transverse direction type serrated fin in turbulent flow based on field synergy principle
LI Juan;LING Xiang;PENG Hao;School of Mechanical and Power Engineering;Nanjing University of Technology;School of Mechanical and Electronic Engineering;Nanjing Forestry University;
LI Juan;LING Xiang;PENG Hao;School of Mechanical and Power Engineering;Nanjing University of Technology;School of Mechanical and Electronic Engineering;Nanjing Forestry University;
..............page:2376-2383
Response characteristics of accumulator pressure in pumped phase-change cooling system
YUAN Jun-fei;TANG Da-wei;CAO Hong-zhang;School of Civil Engineering;Henan University of Science and Technology;Institute of Engineering Thermophysics;Chinese Academy of Sciences;
YUAN Jun-fei;TANG Da-wei;CAO Hong-zhang;School of Civil Engineering;Henan University of Science and Technology;Institute of Engineering Thermophysics;Chinese Academy of Sciences;
..............page:2384-2390
Heat transfer characteristics in two-pass rib-roughened channel at high rotation number with different channel angles
WANG Hui;TIAN Shu-qing;DENG Hong-wu;Research and Design Center;Commercial Aircraft Engine Company Limited;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;
WANG Hui;TIAN Shu-qing;DENG Hong-wu;Research and Design Center;Commercial Aircraft Engine Company Limited;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;
..............page:2391-2400
Experiment on impact of initial diameter on breakup characteristic of single droplet
JIN Ren-han;LIU Yong;ZHU Dong-qing;FENG Zhi-peng;WANG Suo-fang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
JIN Ren-han;LIU Yong;ZHU Dong-qing;FENG Zhi-peng;WANG Suo-fang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2401-2409
Performance test of slinger combustor of turbojet engine running in engine test
LIU Deng-huan;JIN Jie;WANG Fang;PAN Ning-min;JING Wen-ming;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Combustion Design and Research Department;Beijing Huatsing Gas Turbine and Integrated Gasification Combined Cycle Technology Company Limited;
LIU Deng-huan;JIN Jie;WANG Fang;PAN Ning-min;JING Wen-ming;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Combustion Design and Research Department;Beijing Huatsing Gas Turbine and Integrated Gasification Combined Cycle Technology Company Limited;
..............page:2410-2415
Experiment of flow field characteristics in a lean premixed prevaporized low emission combustor
DENG Yuan-hao;YAN Ying-wen;DANG Long-fei;DAI Chao;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;
DENG Yuan-hao;YAN Ying-wen;DANG Long-fei;DAI Chao;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:2416-2424
Numerical research of the ram-rotor test system at off-design conditions
HAN Ji-ang;GUAN Jian;ZHONG Jing-jun;YUAN Chen-guang;Marine Engineering College;Dalian Maritime University;
HAN Ji-ang;GUAN Jian;ZHONG Jing-jun;YUAN Chen-guang;Marine Engineering College;Dalian Maritime University;
..............page:2425-2439
Deterministic stress modelling in transonic compressor based on nonlinear harmonic method
ZHAO Jun;LIU Bao-jie;Aviation Engineering Institute;Civil Aviation Flight University of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHAO Jun;LIU Bao-jie;Aviation Engineering Institute;Civil Aviation Flight University of China;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2440-2449
Numerical simulation of transition flows based on S-A turbulence model and intermittency transport equation
DU Lei;NING Fang-fei;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
DU Lei;NING Fang-fei;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2450-2461
Quick calculation method of internal/external conjugation for steady/unsteady flow field in cooled turbine
TIAN Yong;JI Lu-cheng;SHAO Wei-wei;XIAO Yun-han;Key Laboratory of Advanced Energy and Power;Institute of Engineering Thermophysics;Chinese Academy of Sciences;Research Center for Clean Energy and Power;Chinese Academy of Sciences;School of Physics;University of Chinese Academy of Sciences;School of Aerospace Engineering;Beijing Institute of Technology;
TIAN Yong;JI Lu-cheng;SHAO Wei-wei;XIAO Yun-han;Key Laboratory of Advanced Energy and Power;Institute of Engineering Thermophysics;Chinese Academy of Sciences;Research Center for Clean Energy and Power;Chinese Academy of Sciences;School of Physics;University of Chinese Academy of Sciences;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:2462-2471
Vortex structure of secondary flow in transonic axial compressor with low Reynolds number
HU Jia-guo;WANG Ru-gen;LI Kun;GUO Fei-fei;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
HU Jia-guo;WANG Ru-gen;LI Kun;GUO Fei-fei;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2472-2480
Finite volume compact algorithm suited to computation of supersonic flow field
ZHU Zhi-bin;YUAN Xiang-jiang;CHEN Lin;School of Aerodynamic Theory and Application;China Academy of Aerospace Aerodynamics;
ZHU Zhi-bin;YUAN Xiang-jiang;CHEN Lin;School of Aerodynamic Theory and Application;China Academy of Aerospace Aerodynamics;
..............page:2481-2487
Improvement and verification ofγ-Reθt transition model
QIAO Lei;BAI Jun-qiang;HUA Jun;XU Jing-lei;ZHANG Yang;School of Aeronautics;Northwestern Polytechnical University;Chinese Aeronautical Establishment;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronuatics and Astronautics;
QIAO Lei;BAI Jun-qiang;HUA Jun;XU Jing-lei;ZHANG Yang;School of Aeronautics;Northwestern Polytechnical University;Chinese Aeronautical Establishment;Aviation Industry Corporation of China;School of Energy and Power Engineering;Beijing University of Aeronuatics and Astronautics;
..............page:2488-2497
Blowing control in S-shaped inlet with significant boundary layer ingestion
LIU Lei;CHEN Fu;SONG Yan-ping;CHEN Huan-long;School of Energy Science and Engineering;Harbin Institute of Technology;
LIU Lei;CHEN Fu;SONG Yan-ping;CHEN Huan-long;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:2498-2507
Error analysis of lateral jet interaction flow field of supersonic vehicle with traditional numerical method
YANG Lei;YE Zheng-yin;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;
YANG Lei;YE Zheng-yin;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;
..............page:2508-2515
Research on elastic deformable geometry of hypersonic inlet with multiple forces
YANG Shun-kai;ZHANG Kun-yuan;WANG Lei;LI Yong-zhou;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
YANG Shun-kai;ZHANG Kun-yuan;WANG Lei;LI Yong-zhou;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2516-2522
Identification of unmanned coaxial helicopter model based on UKF
ZHANG Xing-wen;CHEN Ming;MA Yi-min;WANG Bao-bing;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
ZHANG Xing-wen;CHEN Ming;MA Yi-min;WANG Bao-bing;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2523-2530
Research of short take off and vertical landing engine modeling techniques
REN Bing-tao;LI Qiu-hong;KANG Lan;WANG Yuan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Institute of Mining and Coal;Inner Mongolia University of Science and Technology;
REN Bing-tao;LI Qiu-hong;KANG Lan;WANG Yuan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Institute of Mining and Coal;Inner Mongolia University of Science and Technology;
..............page:2531-2538
Research of object-oriented general aero-engine modeling techniques
HU Wei-bo;CHENG Bang-qin;CHEN Zhi-min;ZHAO Hang;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
HU Wei-bo;CHENG Bang-qin;CHEN Zhi-min;ZHAO Hang;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2539-2545
Force and heat effect of shock wave in nozzle interior on nozzle for celestial body outside earth taking off
HE Wei-dong;DANG Hai-yan;School of Aerospace Engineering;Beijing Institute of Technology;Beijing Institute of Specialized Machinery;Aerodynamic Technology Academy of China Aerospace Science and Industry Corporation;
HE Wei-dong;DANG Hai-yan;School of Aerospace Engineering;Beijing Institute of Technology;Beijing Institute of Specialized Machinery;Aerodynamic Technology Academy of China Aerospace Science and Industry Corporation;
..............page:2546-2552
Research on the pressure oscillation characteristics of double pulse solid rocket motor
LIU Wei-kai;HE Guo-qiang;WANG Chun-guang;Science and Technology on Combustion;Internal Flow and Thermal-Structure Laboratory;School of Astronautics;Northwestern Polytechnical University;Xi’an Aerospace Propulsion Institute;Academy of Aerospace Solid Propulsion Technology;China Aerospace Science and Technology Corporation;
LIU Wei-kai;HE Guo-qiang;WANG Chun-guang;Science and Technology on Combustion;Internal Flow and Thermal-Structure Laboratory;School of Astronautics;Northwestern Polytechnical University;Xi’an Aerospace Propulsion Institute;Academy of Aerospace Solid Propulsion Technology;China Aerospace Science and Technology Corporation;
..............page:2553-2560