Solving steady-state temperature fields with axial conduction in moving media using Green’s function method
ZHAO Guo-chang;DU Xia;SONG Li-ping;LI Jing;College of Aerospace Engineering;Shenyang Aerospace University;Institute of Higher Education;Shenyang Aerospace University;

..............page:1249-1260

Thermal protection performances of metallic honeycomb panel structure at transient thermal shock environment
WU Da-fang;ZHOU An-feng;ZHENG Li-ming;PAN Bing;WANG Yue-wu;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Astronautics;Beijing University of Aeronautics and Astronautics;

..............page:1261-1271

Cooling performance and comparison of impingement/effusion cooling lamilloy used as heat shield
LIU You-hong;LI Ying;YANG Xu;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Chengdu Textile College;

..............page:1272-1278

Experiment on effects of mainstream turbulence intensity on film cooling characteristics of turbine vane
ZHOU Zhi-xiang;LIU Cun-liang;ZHANG Zong-wei;ZHU Hui-ren;HE Yi-hong;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;School of Power and Energy;Northwestern Polytechnical University;

..............page:1279-1286

Application of reduced chemical kinetic model for ethylene combustion in combustor calculation of HIFiRE
XIAO Bao-guo;ZHAO Hui-yong;YANG Shun-hua;XING Jian-wen;Science and Technology on Scramjet Laboratory;Hypersonic Aerodynamics Research Institute;China Aerodynamics Research and Development Center;

..............page:1287-1294

Combustion performances of lean direct injection model combustor with three injectors
ZENG Qing-hua;KONG Wen-jun;AI Yu-hua;WANG Bao-rui;Key Laboratory of Light-duty Gas-turbine;Institute of Engineering Thermophysics;Chinese Academy of Sciences;

..............page:1295-1300

Influence of turbine stator blade profiles and film cooling holes optimization on the aerodynamic and cooling performances
LU Shao-peng;CHI Zhong-ran;WANG Long-fei;CAI Le;WANG Song-tao;FENG Guo-tai;WANG Zhong-qi;School of Energy Science and Engineering;Harbin Institute of Technology;Department of Thermal Engineering;Tsinghua University;

..............page:1301-1311

Numerical study of influences of primary jets on turbulent flows and spray combustion in model combustor
XU Rong;ZHAO Jian-xing;WANG Suo-fang;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1312-1322

Numerical investigation on effects of ambient and injection parameters on supercritical injection
JIN Le;FAN Wei;FAN Zhen-cen;ZHOU Zhou;School of Power and Energy;Northwestern Polytechnical University;

..............page:1323-1329

Effect of partial blockage inside film hole on film cooling characteristics
HUANG Ke-nan;ZHANG Jing-zhou;GUO Wen;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Co-Innovation Center of Advanced Aero-Engine;China Gas Turbine Establishment;Aviation Industry Corporation of China;

..............page:1330-1338

Numerical simulation of icing accretion and influence on three-dimensional wing configuration
LU Tian;SANG Wei-min;LIU Xiao-yu;XI Chao;School of Aeronautics;Northwestern Polytechnical University;Institute of Aircraft;Chinese Flight Test Establishment;

..............page:1339-1345

Radial distribution and formation mechanism of the void fraction in an inclined circular tube
LIU Guo-qiang;SUN Li-cheng;YAN Chang-qi;TIAN Dao-gui;National Defense Key Subject Laboratory of Nuclear Safety and Simulation Technology;College of Nuclear Science and Technology;Harbin Engineering University;

..............page:1346-1351

Experiment of ice accrection and shedding on rotating spinner
WANG Jian;HU Ya-ping;JI Hong-hu;CHEN Ning-li;CAO Guang-zhou;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics Astronautics;

..............page:1352-1357

Effect of restricted domain and premixed gas initial temperature on the flame blow-out performance of surface 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:1358-1362

Self-calibration Kalman filter method
FU Hui-min;WU Yun-zhang;LOU Tai-shan;XIAO Qiang;Research Center of Small Sample Technology;Beijing University of Aeronautics and Astronautics;

..............page:1363-1368

Multidisciplinary design optimization of aero-engine turbine flow path in preliminary design phase
SHEN Xiu-li;LONG Dan;DONG Xiao-lin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Co-Innovation Center for Advanced Aero-Engine;Research and Development Center;China Academy of Launch Vehicle Technology;

..............page:1369-1375

Analysis and design of platform damper construction for high pressure turbine blade
WU Xiang-yu;HAN Xu-jun;ZHANG Hai-yang;WANG Jing;LUAN Xu;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:1376-1381

Mechanism motion reliability calculation method considering correlative multi-failure modes
LI Chang;XUAN Cheng-ming;HAN Xing;SONG Hua;School of Mechanical Engineering and Automation;University of Science and Technology Liaoning;

..............page:1382-1387

Low cycle fatigue test of rotating disc under axial loading
LIU Da-cheng;HUANG Fu-zeng;LIU Chuang;HUO Cheng-min;LIU Hai;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:1388-1394

Reduced order computational method for analysis of mistuning bladed disk dynamics characteristic
WANG Pei-yi;LI Lin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:1395-1402

Estimation method for fatigue life under multi-axial random loading
WU Zhi-rong;HU Xu-teng;SONG Ying-dong;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;State Key Laboratory of Mechanics and Control of Mechanical Structures;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1403-1409

Analysis on the system bifurcation and coexistence of multiple solutions for typical airfoil section with freeplay
YIN Lei-lei;ZHANG Si-jin;WEN Gui-lin;XU Hui-dong;College of Mechanical and Vehicle Engineering;Hunan University;

..............page:1410-1416

Geometric configuration on the performance of counterflow thrust vectoring nozzle
LIU Zhao-miao;XU Ying-li;SHEN Feng;College of Mechanical Engineering and Applied Electronics Technology;Beijing University of Technology;

..............page:1417-1425

Experiment on plasma body force of SDBD
TIAN Xi-hui;ZHOU Peng-hui;NIE Wan-sheng;LI Xiao-nan;CHE Xue-ke;HOU Zhi-yong;Department of Space Equipment;Academy of Equipment;The Unit 95927;the Chinese People’s Liberation Army;Department of Foreign Training;Air Force Command College;

..............page:1426-1433

Effect of geometric parameters of rotor on hovering performance of coaxial rotor
WANG Qiang;CHEN Ming;WANG Bao-bing;SU Bing-bing;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Key Laboratory of Rotorcraft Aeromechanics;China Helicopter Research and Development Institute;Aviation Industry Corporation of China;

..............page:1434-1443

Development of inverse characteristic method for matching design of high-speed aircraft forebody/inlet
QIAO Wen-you;HUANG Guo-ping;XIA Chen;WANG Ming-sheng;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1444-1452

Performance calculation and analysis of intercooled recuperated aero-engine
GONG Hao;WANG Zhan-xue;KANG Yong;HUANG Hong-chao;LI Gang-tuan;School of Power and Energy;Northwestern Polytechnical University;China Gas Turbine Establishment;Aviation Industry Corporation of China;

..............page:1453-1461

Suppression of vortex shedding around main circular cylinder by another small control cylinder using immersed boundary method
SONG Li-wei;WU Song-ping;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;National Laboratory for Computational Fluid Dynamics;Beijing University of Aeronautics and Astronautics;Key Laboratory of Fluid Mechanics of Ministry of Education;Beijing University of Aeronautics and Astronautics;

..............page:1462-1467

Influence of tip clearance and propeller separation space on aerodynamic performance of ducted propeller
SU Yun-de;YE Zheng-yin;XU He-yong;National Key Laboratory of Science and Technology on Aerodynamic Design and Research;School of Aeronautics;Northwestern Polytechnical University;

..............page:1468-1475

Three-dimensional blade optimization considering effect of stator seal leakage on end-wall in compressor
HE Liu;JIANG Hong-de;Department of Thermal Engineering;Tsinghua University;

..............page:1476-1481

Mechanism of effect of leading-edge geometry on the turbine blade cascade loss
BAI Tao;ZOU Zheng-ping;ZHANG Wei-hao;ZHOU Kun;LIU Huo-xing;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:1482-1489

Mechanism of self-excited vibration and dynamic stability for pneumatic valves
WANG Jian-zhong;CHEN Er-feng;YU Wu-jiang;YE Chao;SONG Bi-feng;School of Aeronautics;Northwestern Polytechnical University;Beijing Institute of Astronautical Systems Engineering;China Aerospace Science and Technology Corporation;

..............page:1490-1497

Turbo-fan engine fault diagnosis based on adaptive particle filtering
HUANG Jin-quan;FENG Min;LU Feng;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;Aviation Motor Control System Institute;Aviation Industry Corporation of China;

..............page:1498-1504