Dynamical properties analysis and vibration fatigue life calculation with consideration of solid-fluid coupling effect for multifunctional spoiler in civil airplane
CHEN Yong;CHEN Ke-jiao;HUA Tao;YIN Zi-dong;XIA Li-qun;XIONG Jun-jiang;School of Transportation Science and Engineering;Beijing University of Aeronautics and Astronautics;Xi’an Flight Autocontrol Research Institute;

..............page:1-5+13

Aerodynamic force loading simulation based on normalization interpolation
CHEN Liang;LI Hong-bo;China Academy of Aerospace Aerodynamics;

..............page:6-9

The prediction of mutiaxial high cycle fatigue based on stress field intensity
WANG Ming-chun;SONG En-peng;ZHAO Qing-hua;Shenyang Aircraft Design & Research Institute;

..............page:10-13

Research on open framework and prototype system for civil aircraft conceptual design
WANG Gang-lin;LIU Yang-hui;LUO Ming-qiang;Flight Physics Research Center;Chinese Aeronautical Establishment;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;

..............page:14-22

Research on reserve design of aircraft structures by CAD
LIU Guo-chun;PANG Jie;ZHANG Yu;ZHANG Wan-cai;Aviation Engineering Institute;Civil Aviation Flight University of China;

..............page:23-26

Antisymmetric deflection of sandwich plates with hardcore
HAO Jia-qiong;PI Zi-zi;LI Ming-cheng;College of Aerospace Engineering;Nanjing University of Aeronautics &Astronautics;

..............page:27-31+36

Effect of hydrothermal environment to load enhancement factor of CCF300/5228A composite laminates
LIU Xu;CHEN Yue-liang;WANG Li;LEI Yuan-ling;Qingdao Branch;Naval Aeronautical Engineering Institute;Nanchang Aeronautical University;

..............page:32-36

The research of approach power compensation control law with the attack of angle regulator
LI Xue;ZHANG Zhi-bing;Shenyang Aerospace University;Shenyang Aircraft Design & Research Institute;

..............page:37-40

A new method for multi-axis notch fatigue life prediction
WU Wen-tao;WANG Ying-yu;Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle;Nanjing University of Aeronautics and Astronautics;

..............page:41-46+60

Improved design of the installation method for a certain type reconnaissance aircraft’s reconnaissance equipments
SUN Zhi-bin;ZHANG Rui-jie;DING Qing-dong;ZHANG Bao-cai;Shenyang Aircraft Design & Research Institute;

..............page:47-50

Generating optimized drilling and riveting sequence based on ant colony algorithm for aircraft’s panel
SUI Hong-jiang;LI Yun-fei;LIU Zhen-xing;XIAO Hong;YU Hai-tao;PLA Military Representative Office in Shenyang Aircraft Industries Co.Ltd.;The Ministry of Education key Lab of Contemporary Design and Integrated Manufacturing;

..............page:51-55

Research on methods of attitude detemination by kalman filter based on FOG/star-sensor combination technology
MA Song;LI Kun;LIU Ling-ju;DAI Chao-qi;Shenyang Aircraft Design & Research Institute;

..............page:56-60

Research for model-based functional hazard assessment method at aircraft level
CHENG Ran;WU Hai-qiao;College of civil aviation;Nanjing University of Aeronautics & Astronautics;

..............page:61-66

Application of simulation technique in the avionics test
WANG Hai-qing;SUI Hong-jiang;WANG Yan;XIE Xiang-jun;Shenyang Aircraft Design & Research Institute;PLA Military Representative Office in Shenyang Aircraft Industries Co.Ltd.;

..............page:67-72

Research summary of mechnical de-icing systems of aircrafts
LI Qing-ying;BAI Tian;ZHU Chun-ling;College of Aeronautic Transportation;Shanghai University of Engineering Science;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:73-77

Study of air-to-surface weapon selection based on generalized ratio of cost to effectiveness
ZANG Xu;SUN Ying;DONG Zhi;PLA Military Representative Office in Shenyang Aircraft Industries Co.Ltd.;

..............page:78-80

fei ji she ji gao yue

..............page:82