Numerical study of flapping wing/tail aerodynamic interaction for flapping wing micro air vehicle
WANG Yan-gang;CHEN Wei-xiong;DENG Shuang-hou;ZHAO Xu-min;School of Power and Energy;Northwestern Polytechnical University;Faculty of Aerospace Engineering;Delft University of Technology;

..............page:257-264

Image distortion calibration method of round nozzle based on ZEMAX software
YUE Mao-xiong;XIE Feng;BAI Han-chen;ZHANG Long;YUAN Qiang;Science and Technology on Scramjet Laboratory;Hypervelocity Aerodynamics Institute;China Aerodynamics Research and Development Center;Facility Design and Instrumentation Institute;China Aerodynamics Research and Development Center;

..............page:265-270

Parameter design method of double juxtaposition 3-D asymmetric several-S-shaped nozzles
WEI Yong-bin;AI Jun-qiang;The First Aircraft Institute;Aircraft Corporation;Aviation Industry Corporation of China;

..............page:271-280

Numerical investigation of hypersonic curved shock sidewall compression inlet
ZHANG Lin;ZHANG Kun-yuan;WANG Lei;WANG Yuan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:281-288

Research on inlet distortion under crosswind for civil aircraft
LIU Kai-li;SUN Yi-feng;ZHONG Yuan;ZHANG Kun-yuan;ZHANG Hui-liu;Shanghai Aircraft Design and Research Institute;Commercial Aircraft Corporation of China;Ltd.;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:289-296

Influence of key design parameters on aerodynamics performance of cycloidal propeller
TANG Ji-wei;HU Yu;SONG Bi-feng;School of Aeronautics;Northwestern Polytechnical University;

..............page:297-305

Effect of slot orientation on synthetic jet-based separation control in a serpentine inlet
HE Peng;DONG Jin-zhong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:306-314

Flux splitting DSMC-IP method in near space hypersonic flow field
XU Xiao;WANG Xue-de;TAN Jun-jie;School of Energy and Power Engineering;Nanjing University of Science and Technology;

..............page:315-323

Experiment of noise reduction in separate flow system using chevron nozzles
HE Jing-yu;SHAO Wan-ren;XU Ying-bo;LI Xiao-dong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:324-330

Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor
HAN Ji-ang;LI Xiao-dong;ZHONG Jing-jun;Marine Engineering College;Dalian Maritime University;

..............page:331-340

Correlation analysis of energy and stress distributions on variable thickness turbine disk
DING Shui-ting;WANG Zi-yao;LI Guo;Airworthiness Technologies Research Center;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:341-348

Heat conduction loss correction of thin-skin calorimeter on back surface for state-variable measurement
YANG Qing-tao;BAI Han-chen;LIU Ji-chun;Science and Technology on Scramjet Laboratory;Hypervelocity Aerodynamics Institute;China Aerodynamics Research and Development Center;Hypervelocity Aerodynamics Institute;China Aerodynamics Research and Development Center;

..............page:349-355

Experiment on lean blowout performance of triple axial swirler combustor
DING Guo-yu;AN Bo-kun;HE Xiao-min;ZHAO Zi-qiang;JIN Yi;XUE Chong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Harbin Dongan Engine Corporation Limited;

..............page:356-361

Aerodynamic characteristics analysis of eccentric drum based on three-dimensional model
CHEN Lu-miao;WANG Hong-yu;QIN Zhao-ye;CHU Fu-lei;Department of Mechanical Engineering;Tsinghua University;

..............page:362-367

Numerical simulation of runback film breakup on two-dimensional anti-icing airfoil surface
BU Xue-qin;MA Wen-tao;LIN Gui-ping;School of Aeronautics Science and Engineering;Beijing University of Aeronautics and Astronautics;

..............page:368-375

Visualization experiment on film distribution characteristics of shaped film holes based on thermochromic liquid crystal
WU A-sai;ZHU Hui-ren;LIU Cun-liang;HE Yi-hong;LU Cong-ming;ZHANG Cong-xiao;School of Power and Energy;Northwestern Polytechnical University;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;

..............page:376-383

Control method of inlet turbulent intensity in rotating channel and validation
WU Xue-wang;SUN Ji-ning;ZHANG Chuan-jie;JIN Zhao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;Schoool of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:384-391

Life scatter factor of Birnbaum-Saunders distribution
MA Xiao-bing;CHEN Qin-feng;ZHANG Yuan-xin;School of Reliability and Systems Engineering;Beijing University of Aeronautics and Astronautics;

..............page:392-396

Rotordynamic prediction of mode order transition when rotor has an overhang
Konstantin Shaposhnikov;HONG Jie;ZHANG Da-yi;MA Yan-hong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:397-409

Multiple faults diagnosis method of engine bleed system based on improved signed directed graph
LIU Jun-qiang;WANG Xiao-lei;ZHANG Ma-lan;XIE Ji-wei;ZUO Hong-fu;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;

..............page:410-421

Dynamic characteristics of a open crack in hollow shaft rotor system
LU Zhen-yong;CHEN Yu-shu;HOU Lei;LI Zhong-gang;School of Astronautics;Harbin Institute of Technology;School of Mechatronics Engineering;Harbin Institute of Technology;

..............page:422-430

Remaining useful life estimation method of helicopter’s main retarder based on EM-KF algorithm
SUN Lei;JIA Yun-xian;CAI Li-ying;WANG Wei-guo;LIN Guo-yu;Department of Equipment Command and Management;Ordnance Engineering College;1st Laboratory;Ariation Research Institude for the Headquarters of General Staff;Ordnance Technique Research Institution;Ordnance Engineering College;Department of Research;Ordnance Engineering College;

..............page:431-437

Response model of giant magnetostrictive actuator based on elastic damping pedestal
XUE Guang-ming;HE Zhong-bo;LI Dong-wei;LI Yu-long;YANG Zhao-shu;Vehicles and Electrical Engineering Department;Ordnance Engineering College;

..............page:438-445

Influence on flow field and performance of supersonic expander with different strake wall section shapes
ZHONG Jing-jun;HUANG Zhen-yu;YANG Ling;HAN Ji-ang;Marine Engineering College;Dalian Maritime University;

..............page:446-454

Numerical calculation and analysis of fan turbulence broadband noise’s characteristics
TONG Fan;QIAO Wei-yang;WANG Liang-feng;JI Liang;WANG Xun-nian;School of Power and Energy;Northwestern Polytechnical University;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;

..............page:455-462

Experiment on noise reduction physical mechanism of serrated trailing edge structure
XU Kun-bo;QIAO Wei-yang;JI Liang;CHEN Wei-jie;School of Power and Energy;Northwestern Polytechnical University;

..............page:463-472

Numerical investigation of endwall losses control in turbine by leading edge fillet based on teardrop curves
WEI Zuo-jun;QIAO Wei-yang;ZHAO Lei;SHI Pei-jie;School of Power and Energy;Northwestern Polytechnical University;

..............page:473-482

Numerical study on three-dimensional optimization of low-speed axial compressor rotor blade
ZHANG Chen-kai;HU Jun;WANG Zhi-qiang;YIN Chao;YAN Wei;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:483-490

Judgement method and test verification for tooth surface curvature interference of spiral bevel gears
CAO Xue-mei;DEND Xiao-zhong;GENG Long-long;School of Mechanical and Electronical Engineering;Henan University of Science and Technology;

..............page:491-497

Bifurcation characteristic and modeling of transverse-torsional spur gear vibration considering friction and multiple clearances
SHENG Dong-ping;ZHU Ru-peng;JIN Guang-hu;LU Feng-xia;BAO He-yun;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:498-506

Measurement method of defect maximum diameter vector feature of solid rocket motor in volume space
ZHU Min;LI Peng;LU Hong-yi;YU Guang-hui;NO.7Department;Naval Aeronautical and Astronautical University;Department of Airborne Vehicle Engineering;Naval Aeronautical and Astronautical University;

..............page:507-512