1000-8055
2015 Issue 11
..............page:2554
..............page:2556
Internal cooling passage of mist/steam two-phase flow enhanced cooling gas turbine blade
SHI Xiao-jun;SHUI Lin-qi;GAO Jian-min;LI Fa-jing;State Key Laboratory for Manufacturing System Engineering;School of Mechanical Engineering;Xi’an Jiaotong University;
SHI Xiao-jun;SHUI Lin-qi;GAO Jian-min;LI Fa-jing;State Key Laboratory for Manufacturing System Engineering;School of Mechanical Engineering;Xi’an Jiaotong University;
..............page:2561-2567
Gas analysis test and calculation method of aeroengine
WANG Ming-rui;XIAO Yang;HAN Bing;JIA Lin-yan;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Power and Energy Engineering;Harbin Engineering University;
WANG Ming-rui;XIAO Yang;HAN Bing;JIA Lin-yan;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;College of Power and Energy Engineering;Harbin Engineering University;
..............page:2568-2574
Analysis of low-swirl injector emissions and combustion stabilization
ZHANG Chi;YU Bo-wen;YANG Qian;LIU Cheng-chuan;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;
ZHANG Chi;YU Bo-wen;YANG Qian;LIU Cheng-chuan;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:2575-2583
Improvement on one-dimensional flow model of rotor-stator cavity with central inlet
LIN Li;TAN Qin-xue;WU Kang;REN Jing;Energy-saving Technology Research Center;School of Chemical Engineering;Fuzhou University;Department of Thermal Engineering;School of Mechanical Engineering;Tsinghua University;
LIN Li;TAN Qin-xue;WU Kang;REN Jing;Energy-saving Technology Research Center;School of Chemical Engineering;Fuzhou University;Department of Thermal Engineering;School of Mechanical Engineering;Tsinghua University;
..............page:2584-2591
Model experiment on pressure drop and thermal efficiency of double U-shaped tubes heat exchanger
LIU Xi-yue;ZHANG Jing-zhou;LI Gang-tuan;KANG 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;China Gas Turbine Establishment;Aviation Industry Corporation of China;
LIU Xi-yue;ZHANG Jing-zhou;LI Gang-tuan;KANG 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;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:2592-2599
Instantaneous propagation characteristics of continuous rotating detonation wave
WANG Chao;LIU Wei-dong;LIU Shi-jie;LIN Zhi-yong;JIANG Lu-xin;Science and Technology on Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
WANG Chao;LIU Wei-dong;LIU Shi-jie;LIN Zhi-yong;JIANG Lu-xin;Science and Technology on Scramjet Laboratory;College of Aerospace Science and Engineering;National University of Defense Technology;
..............page:2600-2606
Cavitation characteristic in aviation fuel pump based on surrogate fuel
XIONG Ying-hua;LIU-Ying;LI Shu-lin;CHEN Tai-ran;WANG Guo-yu;School of Mechanics and Engineering;Beijing Institute of Technology;Aviation Key Laboratory of Science and Technology on Aero Electromechanical System;Nanjing Engineering Insitute of Aircraft Systems;Jincheng;Aviation Industry Corporation of China;
XIONG Ying-hua;LIU-Ying;LI Shu-lin;CHEN Tai-ran;WANG Guo-yu;School of Mechanics and Engineering;Beijing Institute of Technology;Aviation Key Laboratory of Science and Technology on Aero Electromechanical System;Nanjing Engineering Insitute of Aircraft Systems;Jincheng;Aviation Industry Corporation of China;
..............page:2607-2615
Research of fouling deposition influence on heat transfer of blade surface
SHI Hui;LI Liang;FENG Zhen-ping;Institute of Turbomachinery;School of Energy and Power Engeering;Xi’an Jiaotong University;Energy Saving Center;Xi’an Thermal Power Research Institute Company Limited;
SHI Hui;LI Liang;FENG Zhen-ping;Institute of Turbomachinery;School of Energy and Power Engeering;Xi’an Jiaotong University;Energy Saving Center;Xi’an Thermal Power Research Institute Company Limited;
..............page:2616-2622
Realization and verification of the flow characteristic experiment in rotating two-pass square duct with smooth walls
CHEN Hao;DENG Hong-wu;CHENG Jun-hua;LI Yang;TIAN Shu-qing;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;Research and Developing Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
CHEN Hao;DENG Hong-wu;CHENG Jun-hua;LI Yang;TIAN Shu-qing;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;Research and Developing Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:2623-2629
Application of time-inclined method on the unsteady simulation of turbomachinery
GAO Li-min;LI Ping;CHEN Xuan;ZHOU Li;School of Power and Energy;Northwestern Polytechnical University;Collaborative Innovation Center for Advanced Aero-Engine;
GAO Li-min;LI Ping;CHEN Xuan;ZHOU Li;School of Power and Energy;Northwestern Polytechnical University;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2630-2637
Investigations on desensitization of blade tip clearance variation in turbine blades
GAO Jie;ZHENG Qun;LIU Yun-ning;ZHAO Zhan;College of Power and Energy Engineering;Harbin Engineering University;Harbin Marine Boiler and Turbine Research Institute;China Shipbuilding Industry Corporation;
GAO Jie;ZHENG Qun;LIU Yun-ning;ZHAO Zhan;College of Power and Energy Engineering;Harbin Engineering University;Harbin Marine Boiler and Turbine Research Institute;China Shipbuilding Industry Corporation;
..............page:2638-2646
Stall of an axial-compressor rotor with casing treatment
FAN Lin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
FAN Lin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2647-2657
Effects of vortex generator jet on the flow of bowed compressor cascades
LI Long-ting;SONG Yan-ping;LIU Hua-ping;CHEN Fu;School of Energy Science and Engineering;Harbin Institute of Technology;
LI Long-ting;SONG Yan-ping;LIU Hua-ping;CHEN Fu;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:2658-2665
Study on the frequency of partial surge and a frequency prediction method
PAN Tian-yu;HE Lei;WANG Zheng-he;LI Zhi-ping;LI Qiu-shi;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
PAN Tian-yu;HE Lei;WANG Zheng-he;LI Zhi-ping;LI Qiu-shi;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2666-2672
Performance degradation and components deterioration degree estimation for a turboshaft engine
HUANG Kai-ming;LI Yi-Guang;ZHANG Wei;FENG Xing;CAI Jian-bing;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;School of Aerospace;Transport and Manufacturing;Cranfield University;
HUANG Kai-ming;LI Yi-Guang;ZHANG Wei;FENG Xing;CAI Jian-bing;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;School of Aerospace;Transport and Manufacturing;Cranfield University;
..............page:2673-2679
Analytical model of inlet distortion effect on aerodynamic stability of variable cycle engine
YAN Wei;HU Jun;TU Bao-feng;ZHANG Chen-kai;YIN Chao;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;
YAN Wei;HU Jun;TU Bao-feng;ZHANG Chen-kai;YIN Chao;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:2680-2687
3-D numerical simulation of dynamic process of twin nozzle STOVL aircraft lift loss
HONG Liang;Eriqitai;XU Jing-lei;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
HONG Liang;Eriqitai;XU Jing-lei;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2688-2694
Design and simulation of a dual-channel variable geometry turbine based combined cycle inlet
WANG De-peng;ZHUANG Yi;TAN Hui-jun;ZHANG Hong;DU Mo-chen;LI Guang-sheng;Jiangsu Province Key Laboratory of Aerospace Power Systems;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;Sino-European Institute of Aviation Engineering;Civil Aviation University of China;
WANG De-peng;ZHUANG Yi;TAN Hui-jun;ZHANG Hong;DU Mo-chen;LI Guang-sheng;Jiangsu Province Key Laboratory of Aerospace Power Systems;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;Sino-European Institute of Aviation Engineering;Civil Aviation University of China;
..............page:2695-2704
Investigation on wall modeled large eddy simulation of channel turbulent flow in high Reynolds number
LI Meng;TU Zheng-guang;XU Jing-lei;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;The 9th Designing;China Aerospace Science and Industry Corporation;
LI Meng;TU Zheng-guang;XU Jing-lei;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;The 9th Designing;China Aerospace Science and Industry Corporation;
..............page:2705-2712
Research on backup hydromechanical control plan of the turbo-shaft engine’s control system
LIAO Guang-huang;HUANG Jin-quan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;
LIAO Guang-huang;HUANG Jin-quan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:2713-2720
Robust design of external gear pump with trapped oil problem
WU Xiao-feng;LIU Chun-jie;GAN Wei-min;WANG Xiao-jun;HU Shao-gang;JI Jing-jing;School of Mechanical and Vehicle Engineering;Changzhou Institute of Technology;
WU Xiao-feng;LIU Chun-jie;GAN Wei-min;WANG Xiao-jun;HU Shao-gang;JI Jing-jing;School of Mechanical and Vehicle Engineering;Changzhou Institute of Technology;
..............page:2721-2729
Numerical simulation on fuel vapor core configuration in fuel vapor core pump with radial straight blades
WANG Bin;YU Ding-peng;YE Zhi-feng;GUAN Hua-sheng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
WANG Bin;YU Ding-peng;YE Zhi-feng;GUAN Hua-sheng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2730-2737
New robust control method with guardian maps
LI Chen-liang;ZHANG Rui;LIU Meng-ying;LIU Yan-bin;LU Yu-ping;Research Institute of Unmanned Aircraft;Nanjing University of Aeronautics and Astronautics;College of Astronautics;Nanjing University of Aeronautics and Astronautics;
LI Chen-liang;ZHANG Rui;LIU Meng-ying;LIU Yan-bin;LU Yu-ping;Research Institute of Unmanned Aircraft;Nanjing University of Aeronautics and Astronautics;College of Astronautics;Nanjing University of Aeronautics and Astronautics;
..............page:2738-2745
Construction and experiment of intelligent temperature and humidity measurement system for freight spacecraft
CHEN Jun-guang;LI Yun-hua;LI Yun-ze;ZHANG Hong-sheng;ZHONG Ming-liang;School of Automation Science and Electrical Engineering;Beijing University of Aeronautics and Astronautics;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
CHEN Jun-guang;LI Yun-hua;LI Yun-ze;ZHANG Hong-sheng;ZHONG Ming-liang;School of Automation Science and Electrical Engineering;Beijing University of Aeronautics and Astronautics;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2746-2752
Structure and dynamics analysis of rotor system in geared turbofan engine
MA Yan-hong;CAO Chong;HAO Yong;ZHANG Bo;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;
MA Yan-hong;CAO Chong;HAO Yong;ZHANG Bo;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:2753-2761
Design method of squeeze film damper for aero-engine rotors
LIU Zhan-chi;LIAO Ming-fu;CONG Pei-hong;WANG Juan;WANG Si-ji;SHI Bin;LI Yan;School of Power and Energy;Northwestern Polytechnical University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
LIU Zhan-chi;LIAO Ming-fu;CONG Pei-hong;WANG Juan;WANG Si-ji;SHI Bin;LI Yan;School of Power and Energy;Northwestern Polytechnical University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:2762-2770
Analysis of the effect of floating ring squeeze film damper on sudden unbalance response of low pressure rotor
XIA Ye-bao;REN Xing-min;QIN Wei-yang;DENG Wang-qun;Institute of Vibration Engineering;Northwestern Polytechnical University;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
XIA Ye-bao;REN Xing-min;QIN Wei-yang;DENG Wang-qun;Institute of Vibration Engineering;Northwestern Polytechnical University;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:2771-2778
Testability prior information fusion method based on uncertainty measure and supporting degree
ZHANG Xi-shan;HUANG Kao-li;YAN Peng-cheng;LIAN Guang-yao;LI Zhi-yu;Department Four;Ordnance Engineering College;Research Room One;Ordnance Technological Research Institute;General Armament Department;the Chinese People’s Liberation Army;66010Unit;the Chinese People’s Liberation Army;
ZHANG Xi-shan;HUANG Kao-li;YAN Peng-cheng;LIAN Guang-yao;LI Zhi-yu;Department Four;Ordnance Engineering College;Research Room One;Ordnance Technological Research Institute;General Armament Department;the Chinese People’s Liberation Army;66010Unit;the Chinese People’s Liberation Army;
..............page:2779-2786
Rate-dependent cohesive zone model of the interface between HTPB propellant and insulation
CHEN Xiong;NIU Ran-ming;ZHENG Jian;JIA Deng;School of Mechanical Engineering;Nanjing University of Science and Technology;
CHEN Xiong;NIU Ran-ming;ZHENG Jian;JIA Deng;School of Mechanical Engineering;Nanjing University of Science and Technology;
..............page:2787-2793
Investigation on acquisition schemes of cryogenic propellant subcooling for long-term on-orbit storage
WANG Lei;LI Yan-zhong;MA Yuan;XU Meng-jian;Department of Refrigeration and Cryogenic Engineering;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;XU Meng-jian;Department of Refrigeration and Cryogenic Engineering;School of Energy and Power Engineering;Xi’an Jiaotong University;State Key Laboratory of Technologies in Space Cryogenic Propellants;
..............page:2794-2802
Influence predictions of base parameters on noise radiations of face gear drives
LI Zheng-min-qing;CHEN Hong-shang;ZHU Ru-peng;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
LI Zheng-min-qing;CHEN Hong-shang;ZHU Ru-peng;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2803-2809
Optimum design of double-row angular-contact ball bearing with immune algorithm
CHENG Chao;WANG Jiu-gen;College of Mechanical Engineering;Zhejiang University;
CHENG Chao;WANG Jiu-gen;College of Mechanical Engineering;Zhejiang University;
..............page:2810-2816