1007-5453
2014 Issue 3
Aviation Weapons Trend Analysis from U.S. AirSea Battle
CHAI Jianzhong;,DONG Haifeng;
CHAI Jianzhong;,DONG Haifeng;
..............page:1-4
Analysis and Inspiration of the U.S. Quick Reach Air Launch System
GENG Yansheng;,GUO Zhaodian;,ZHOU Qifa;
GENG Yansheng;,GUO Zhaodian;,ZHOU Qifa;
..............page:5-9
Study on Adaptation System of Carrier-based Aircraft
DUAN Zhuoyi;,GUO Runzhao;,LI Xiaowei;
DUAN Zhuoyi;,GUO Runzhao;,LI Xiaowei;
..............page:10-13
..............page:14-17
Research on Planform Sizing of Wing with High Aspect Ratio and Low Sweep Angle
QU Hao;,SHI Yongqiang;,ZHANG Hong;
QU Hao;,SHI Yongqiang;,ZHANG Hong;
..............page:18-22
Structural Discussion of Pressure Cabin Characterized with Wave-section Surfaces of Fling-wing Aircraft
HUANG Haidong;
HUANG Haidong;
..............page:23-26
Research of Fuselage Tailcone Abutting Design for Transporter
WANG Xiaohui;,WU Xiaoliang;,YAN Xipeng;
WANG Xiaohui;,WU Xiaoliang;,YAN Xipeng;
..............page:27-30
Design of a Software for Aircraft High-lift Control System
HE Jiahang;,LIANG Sen;
HE Jiahang;,LIANG Sen;
..............page:31-34
Design and Simulation of Frequency Measurement Circuit Low Pass Filter for Aircraft AC Power System
HE Bo;,YANG Weipeng;,ZHANG Yong;
HE Bo;,YANG Weipeng;,ZHANG Yong;
..............page:35-39
Development of a Ducted Coaxial Rotor UAV
SU Yunde;,XU Lincheng;,YE Zhengyin;
SU Yunde;,XU Lincheng;,YE Zhengyin;
..............page:40-44
A Method to Estimate Stability Margin of Fly-by-wire Flight Control System
GAO Yakui;,ZHANG Yan;,ZHI Chaoyou;
GAO Yakui;,ZHANG Yan;,ZHI Chaoyou;
..............page:45-48
..............page:49-53
Research on Factors Affecting Precision of Rational Function Aerodynamic Approximation Based on Minimum-state Method
GAO Yining;,PU Lidong;,TAN Shengang;
GAO Yining;,PU Lidong;,TAN Shengang;
..............page:54-58
Analysis of Pulley Block Efifciency for Winch on Military Transporter
CHENG Defeng;,FANG Zhengpeng;
CHENG Defeng;,FANG Zhengpeng;
..............page:59-63
Optimization Design Method on Aircraft Components Force Measurement Test Model
FU Chenghu;,YANG Lianbo;
FU Chenghu;,YANG Lianbo;
..............page:64-66
Research on Ground Test of Aircraft Windshield Heating System
CHANG Hongliang;,DANG Qi;,HU Yang;
CHANG Hongliang;,DANG Qi;,HU Yang;
..............page:67-70
Analysis of Relationship between Airworthiness Design Assurance System and Quality Management System
CAO Jijun;,SI Jixian;
CAO Jijun;,SI Jixian;
..............page:71-74
Application of Aerodynamic Shape Deformation based on NURBS Surface
LEI Wutao;,MA Xiaoyong;,ZHANG Yanjun;
LEI Wutao;,MA Xiaoyong;,ZHANG Yanjun;
..............page:75-78