Helicopter performance improvement by rotor morphing technologies
HAN Dong;LIN Chang-liang;LI Jian-bo;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2017-2023

Aerodynamic structural characteristic of box six-component strain-gauge balance in heat state test
LUO Hua-yun;HOU Min-jie;WANG Yue-gui;GU Yang;Aviation Key Laboratory of Science and Technology on Aero-Engine Altitude Simulation;China Gas Turbine Establishment;Aviation Industry Corporation of China;

..............page:2024-2030

Numerical simulation of two-dimensional curved compression surface with isentropic surface coordinate transformation
ZHANG Lin;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:2031-2039

Aerodynamic characteristics of design Mach number of 5 two-dimensional inlet with mixed-compression under typical condition
WENG Xiao-chai;GUO Rong-wei;ZHU Dan-dan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Unit 94710;the Chinese People’s Liberation Army;Co-Innovation Center for Advanced Aero-Engine;Unit 94627;the Chinese People’s Liberation Army;

..............page:2040-2046

Application of e N method in three-dimensional hypersonic boundary layers
YU Gao-tong;LUO Ji-sheng;Department of Mechanics;School of Mechanical Engineering;Tianjin University;

..............page:2047-2054

Investigation of basic flowfield with center body consisting of four spline curves diffusing reflected shock wave
LI Yong-zhou;ZHANG Kun-yuan;ZHONG Qi-tao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2055-2062

Analysis of aerodynamic characteristics of flexible wing of dragonfly based on CFD/CSD method
MENG Ling-bing;ANG Hai-song;XIAO Tian-hang;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2063-2069

Preliminary analysis of jaws inlet performance under design conditions
GU Tian-lai;FU Lei;ZHANG Shuai;ZHENG Yao;School of Aeronautics and Astronautics;Zhejiang University;

..............page:2070-2078

Flow field and aerodynamic characteristic of deflectable nose projectile at different angles of attack
GUO Yu-jie;CHEN Zhi-hua;HAN Jun-li;National Key Laboratory of Transient Physics;Nanjing University of Science and Technology;Faculty OfficeⅡ;Beijing Institute of Special Electromechanical Technology;

..............page:2079-2084

A dynamic ensemble extreme learning machine model for aircraft engine health condition prediction
ZHONG Shi-sheng;LEI Da;School of Mechatronics Engineering;Harbin Institute of Technology;

..............page:2085-2090

Active control of flexible structure vibration based on fuzzy fractional order PI~λD~μ
SHENG Xian-jun;ZHONG Sheng;JIANG Tao;School of Electrical Engineering;Dalian University of Technology;

..............page:2091-2096

Mass optimization of turbine disk based on sequential sampling algorithm
XU Sheng-li;LIU Hai-tao;WANG Xiao-fang;SONG Yang;School of Energy and Power Engineering;Dalian University of Technology;Key Laboratory of Ocean Energy Utilization and Energy Conservation of Ministry of Education;Dalian University of Technology;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:2097-2103

Experimental test method for high-frequency modal damping of turbomachinery blades
GUO Xue-lian;FAN Yu;LI Lin;Beijing Power Machinery Research Institute;China Aerospace Science and Industry Corporation;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:2104-2112

Fatigue life prediction method of 2.5dimensional woven composites
QIU Rui;WEN Wei-dong;CUI Hai-tao;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:2113-2120

Parameters design of smart spring vibration suppression system based on common point of amplitude frequency characteristic curve cluster
NI De;ZHU Ru-peng;BAO He-yun;LU Feng-xia;FU Qiu-ju;Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2121-2128

Analysis of parameter-nonparametric fusion on space bearing friction moment
XU Yong-zhi;XIA Xin-tao;School of Mechanical Engineering;Northwestern Polytechnical University;School of Mechatronics Engineering;Henan University of Science and Technology;

..............page:2129-2135

An oil flow management valve for solving oil leakage at low rotating speed
GU Zhi-ying;LI Guo-quan;YU Li;MA Fang;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;Key Laboratory for Power Transmission Technology of Aero-Engine;Aviation Industry Corporation of China;Harbin Bearing Manufacturing Limited;Aviation Industry Corporation of China;

..............page:2136-2141

Influence physics of mainstream pressure gradient on film hole discharge coefficient
ZHU Hui-ren;LUO Jian-xia;HUANG Xiao-yang;LIU Zhi-gang;School of Power and Energy;Northwestern Polytechnical University;

..............page:2142-2149

Investigations on ablation failure of high power pistons
QIN Zhao-ju;ZHANG Wei-zheng;SONG Li-ye;YUAN Yan-peng;School of Mechanical Engineering;Beijing Institute of Technology;School of Mechanical Engineering;North China University of Water Resources and Electric Power;

..............page:2150-2156

Numerical simulation of ice accretion on rotor airfoil of helicopter considering effects of centrifugal force
CHEN Xi;ZHAO Qi-jun;ZHAO Guo-qing;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2157-2165

Numerical investigation on particle deposition characteristics in vicinity of film cooling holes
ZHOU Jun-hui;ZHANG Jing-zhou;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2166-2173

Pumping performance for double-stage lobe mixer/ejector
PAN Cheng-xiong;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;Co-Innovation Center for Advanced Aero-Engine;

..............page:2174-2180

Effect of angle between lamilloy and rotation axis on heat transfer capability of limited lamilloy
BAI Guo-qiang;CHANG Hai-ping;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:2181-2187

Experiment on lean blow-out performance of pilot stage in internally-staged combustor
LI Hai-tao;XU Quan-hong;FU Zhen-bo;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:2188-2194

A tip clearance control technology for turbine
YANG Jia-li;TU Meng-pi;ZHANG Yi-li;ZHANG Li-zhang;YANG Cheng-wu;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;Graduate University of Chinese Academy of Sciences;

..............page:2195-2201

Optimization of fan rotor blade in high bypass ratio turbofan engine
WANG Zhi-qiang;SHEN Xi-gang;HU Jun;LIU Zhi-jie;ZHENG Ning;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:2202-2209

Research on S1stream surface for cooling air mixing and variable thickness flow slice in multi-stage
LUO Lei;LU Shao-peng;WANG Song-tao;WANG Long-fei;CUI Tao;School of Energy Science and Engineering;Harbin Institute of Technology;

..............page:2210-2220

Model of tip clearance leakage flow blockage in micro-scale centrifugal impellers
SUN Qian-wei;SONG Xi-zhen;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;Co-Innovation Center for Advanced Aero-Engine;

..............page:2221-2228

Scheme on aerodynamic design of core driven fan stage
LAI An-qing;HU Jun;TU Bao-feng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Engineering Institute;Civil Aviation Flight University of China;

..............page:2229-2238

Radial vortex phenomenon and instability mechanism of transonic axial-flow compressor
HU Jia-guo;WANG Ru-gen;LI Shao-wei;GAN Tian;Aeronautics and Astronautics Engineering College;Air Force Engineering University;

..............page:2239-2246

Load sharing and lightweight optimization design of torque-split transmission system based on FA-NSGA
FU Chen-xi;ZHAO Ning;ZHAO Yong-zhi;FU Bi-bo;Shaanxi Engineering Laboratory for Transmissions and Controls;Northwestern Polytechnical University;Transmission Technology Center;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;

..............page:2247-2255

A fault monitoring technique for wear of aero-engine rolling bearing
WANG Hong-wei;CHEN Guo;CHEN Li-bo;SONG Ke;LI Ai;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;Beijing Aeronautical Technology Research Center;

..............page:2256-2263

Impact of torsional stiffness on dynamic load sharing coefficient of two-input cylindrical gear split-torque transmission system
GUI Yong-fang;ZHU Ru-peng;FU Bi-bo;LI Hai-feng;WANG Qi-bo;JIN Guang-hu;LI Zhi-jun;Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;

..............page:2264-2272