Numerical simulation of flow and heat transfer performance in turntable
YANG Zhi-min;JIA Zhen;ZHAO Yu;ZHANG Shu-hua;GE Xin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;Aerospace Engine Research Institute;Aviation Industry Corporation of China;

..............page:737-747

Combustor design and performance prediction based on parametric model
LI Feng;SHANG Shou-tang;GUO Rui-qing;CHENG Ming;TANG Zheng-fu;SONG Bo;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Combustion Design Office;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:748-754

Numerical simulation of friction torque of rotating disc for rotor-stator system with central inflow
ZHANG Da;HAN Jian-qiao;LUO Xiang;XU Guo-qiang;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:755-762

Three-dimensional combustion numerical simulation of scramjet internal and external flow fields
NIU Dong-sheng;HOU Ling-yun;PAN Peng-fei;MA Xue-song;LU Jin-li;School of Aerospace;Tsinghua University;Science and Technology on Scramjet Laboratory;Beijing Power Machinery Research Institute;the Third Research Academy;China Aerospace Science and Industry Corporation;

..............page:763-769

Experiment of heat transfer in internal cooling channel with tip and trailing edge outflows
LIANG Wei-ying;ZHU Hui-ren;ZHANG Li;XU Du-chun;School of Power and Energy;Northwestern Polytechnical University;

..............page:770-776

Formation mechanism of microbubble emission boiling
TANG Ji-guo;SUN Li-cheng;ZHU Guang-yu;National Defense Key Subject Laboratory for Nuclear Safety and Simulation Technology;College of Nuclear Science and Technology;Harbin Engineering University;

..............page:777-782

Analysis on supercooled large droplet impingement characteristics and ice shape of two-dimensional airfoils
DU Chen-hui;YU Jia;LIN Gui-ping;SHEN Xiao-bin;BU Xue-qin;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;

..............page:783-791

Numerical investigation of two-phase spray combustion performance for LPP low-emission combustor
ZHU Jia-wei;YAN Ying-wen;LI Shi;DENG Yuan-hao;Jiangsu Province Key Laboratory of Aerospace Power Systems;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;the Fifth Electronics Research Institute;Ministry of Industry and Information Technology of the People’s Republic of China;

..............page:792-800

Experiment of blow-out performance of premixed flame on porous media surface
ZHANG Long;XU Quan-hong;ZHANG Chi;LIN Pei-hua;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:801-806

Response of hypersonic flow field on disturbance wave in free-stream and boundary-layer disturbance wave evolution
WANG Zhen-qing;TANG Xiao-jun;MENG Xiang-nan;L Hong-qing;College of Aerospace and Civil Engineering;Harbin Engineering University;

..............page:807-816

Experiment on aero-engine altitude simulated pressure distortion
TIAN Jin-hu;QIAO Wei-yang;PENG Sheng-hong;School of Power and Energy;Northwestern Polytechnical University;Aviation Key Laboratory of Science and Technology and Aero-Engine Altitude Simulation;China Gas Turbine Establishment;Aviation Industry Corporation of China;

..............page:817-823

Analysis and evaluation on RCS characteristics of helicopter considering modulated effect of rotor
JIANG Xiang-wen;ZHAO Qi-jun;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:824-834

Characteristic analysis of unsteady aerodynamic interactions of contra rotating open rotor
XIA Zhen-feng;YANG Yong;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;

..............page:835-843

Multiple parameters dynamic modeling and analysis of helicopter rotor multi-layer elastomeric damper
LI Rui-rui;YANG Wei-dong;YU Zhi-hao;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:844-851

Mechanism of mass flow matching in scramjet
HUANG Xing;CHEN Yu-chun;WANG Xiao-dong;LI Jie;CAI Yuan-hu;School of Power and Energy;Northwestern Polytechnical University;

..............page:852-857

Integrated flow field characteristics of helicopter/particle separator: Part1 influence of advance ratio
ZENG Ping-jun;SUN Shu;HUANG He-xia;DU Mo-chen;CHEN Wei;TAN Hui-jun;LI Guang-sheng;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:858-866

Integrated flow field characteristics of helicopter/particle separator: Part 2 influence of rotor disk load
HUANG He-xia;ZENG Ping-jun;TAN Hui-jun;DU Mo-chen;SUN Shu;CHEN Wei;LI Guang-sheng;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;

..............page:867-874

Structural optimization design method of twin-web turbine disk with tenon
LU Shan;ZHAO Lei;School of Power and Energy;Northwestern Polytechnical University;

..............page:875-880

A method for determination of parameters in total strain life equation
WANG Yan-rong;LI Hong-xin;YUAN Shan-hu;WEI Da-sheng;SHI Liang;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Co-Innovation Center for Advanced Aero-Engine;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:881-886

Signal transmission model with gradient temperature based on finite difference time domain
MEN Xiu-hua;LI Shun-ming;SONG Fang-zhen;XU Jia;School of Mechanical Engineering;University of Jinan;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Xi’an Aircraft Industry Company Limited;Aviation Industry Corporation of China;

..............page:887-893

Rotating substructure method for 3-D finite element rotor model reduction
ZUO Yan-fei;WANG Jian-jun;MA Wei-meng;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:894-900

In-situ experiment on early growth of small fatigue crack of nickel-based superalloy GH4169
ZHANG Li;HUANG Xin-yue;WU Xue-ren;YU Hui-chen;ZHANG Min;LI Hong-liang;Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation;Beijing Institute of Aeronautical Materials;Aviation Industry Corporation of China;National Key Laboratory of Science andTechnology on Advanced High Temperature Structure Materials;Beijing Institute of Aeronautical Materials;Aviation Industry Corporation of China;State Key Laboratory for Advanced Metals and Materials;University of Science and Technology Beijing;

..............page:901-906

Numerical study guide vane coolant on performance of turbine stage
ZHONG Yi-cheng;ZHANG Cun-yuan;XU Wei-zu;PAN Shang-neng;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Technical Department;the Limited Company of Nanjing Puguo Technology;Chinese Avation Powerplant Research Institution;Aviation Industry Corporation of China;

..............page:907-916

In-duct circumferential acoustic mode measurement of axial fan/compressor
WANG Liang-feng;QIAO Wei-yang;JI Liang;YU Suo-yuan;School of Power and Energy;Northwestern Polytechnical University;

..............page:917-926

Numerical investigation of axial seal flow in turbine cavity
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:927-934

Numerical investigation on subsonic axial-flow compressor rotor with implementation of axisymmetric casing contouring optimization
GAO Xiang;CHU Wu-li;School of Power and Energy;Northwestern Polytechnical University;Co-Innovation Center for Advanced Aero-Engine;

..............page:935-943

Parametric research on improved Qiu slip factor model for centrifugal compressor impellers
MENG Fei;TIAN Xiao-pei;SHAN Peng;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:944-952

Aero-engine fault-tolerant control based on mode switch
YANG Zheng-shan;QIU Xiao-jie;ZHUANG Xi-ming;HUANG Jin-quan;Aviation Motor Control System Institute;Aviation Industry Corporation of China;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Military Representatives Office of the Army Aeronautical Department Resident inShanghai Region for the Headquarters of General Staff;

..............page:953-964

Robust fault diagnosis for aero-engine compressor sensor based on LMI and discrete model
HE Chen;ZHANG Xiao-dong;Patton R J;School of Power and Energy;Northwestern Polytechnical University;Control and Intelligent Systems Engineering;Faculty of Science;University of Hull;

..............page:965-972

Active fault tolerant controller designo of aero-engine main fuel metering valve
FU Qiang;FAN Ding;PENG Kai;School of Power and Energy;Northwestern Polytechnical University;

..............page:973-979

Influential factors analysis to additional ejection force in concentric canister launcher
YU Yong;MU Yun-tao;School of Aerospace Engineering;Beijing Institute of Technology;

..............page:980-986

Failure mode of reusable rocket engine based on fuzzy fault tree and factor analysis
HOU Jin-li;JIN Ping;CAI Guo-biao;School of Astronautics;Beijing University of Aeronautics and Astronautics;

..............page:987-992