1673-4599
2013 Issue 6
Conversion of Aerodynamic Load Based on Spring-Cantilever Model with Minimal Strain Energy Criterion
GAO Shang-jun;YU Zhe-feng;WANG Hai;School of Aeronautics and Astronautics;Shanghai Jiao Tong University;
GAO Shang-jun;YU Zhe-feng;WANG Hai;School of Aeronautics and Astronautics;Shanghai Jiao Tong University;
..............page:1-4+32
A New Concept Design of Ducted Fan VTOL Based on Torque Balance
TAO Xiao-yang;HAO Xiang-dong;FU Jie-cheng;Shenyang Aircraft Design & Research Institute;
TAO Xiao-yang;HAO Xiang-dong;FU Jie-cheng;Shenyang Aircraft Design & Research Institute;
..............page:5-11
Path Planning Based on GA in Convex Polygon Regio
XU Qiu-di;ZHANG Yun-fei;School of AeronauticsScience and Engineering;Beijing University of Aeronautics and Astronautics;
XU Qiu-di;ZHANG Yun-fei;School of AeronauticsScience and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:12-15
Numerical Simulation of Nacelle Flow and Temperature Field Using CFD
WANG Yu-mei;Chinese Flight Test Establishment;
WANG Yu-mei;Chinese Flight Test Establishment;
..............page:16-20
The CFD Methods Application During the Design of Back Mounted Air Intake Blocking Taper Wind Tunnel Test Model
DENG Jian;LI Jing-hu;ZHU A-yuan;Research and Development center;Chengdu Aircraft & Industrial Group Ltd. Corp.;
DENG Jian;LI Jing-hu;ZHU A-yuan;Research and Development center;Chengdu Aircraft & Industrial Group Ltd. Corp.;
..............page:21-24
Using the Fixing Angle of Gridfin’s Wall to Study the Engineering Methods of Controlling Pressure Center in State of Replicating and Deploying
LIU Bin;DU Mian-yin;ZHOU Pei-pei;ZHANG Gui-ru;China Academy of Aerospace Aerodynamics;
LIU Bin;DU Mian-yin;ZHOU Pei-pei;ZHANG Gui-ru;China Academy of Aerospace Aerodynamics;
..............page:25-28
The Reserach of Very Light Aeroplane Performance
DAI Gui-cheng;ZU Li-jun;Shenyang Aircraft Design & Research Institute;PLA 133 Manufactory Military Representative Office;
DAI Gui-cheng;ZU Li-jun;Shenyang Aircraft Design & Research Institute;PLA 133 Manufactory Military Representative Office;
..............page:29-32
A Research on Optimal Maneuver of Airborne Single Observer Bearings-Only System
WANG Ti-ming;LI Yan-zhi;ZHAO Li-jie;PLA 93846;Aviation University for Air Force;
WANG Ti-ming;LI Yan-zhi;ZHAO Li-jie;PLA 93846;Aviation University for Air Force;
..............page:33-37
Stability Analysis and Failure Intensity Analysis of Composite Stiffened Wing Panels
LI Ting;HAO Xue-Ping;ZHAO Jie;WU De-feng;Shenyang Aircraft Design & Research Institute;
LI Ting;HAO Xue-Ping;ZHAO Jie;WU De-feng;Shenyang Aircraft Design & Research Institute;
..............page:38-42
Design and Implementation of Maintenance and Support Activities Visualization Software Based on Fuzzy Petri Nets
SHI Yong-sheng;LI Jian-xue;College of Aeronautical Engineering;Civil Aviation University of China;
SHI Yong-sheng;LI Jian-xue;College of Aeronautical Engineering;Civil Aviation University of China;
..............page:43-47
Impact of Visual Condition on the Pilot’s Response Capability to the Carrier-Landing-Guidance Cue
WU Wen-hai;WANG Zi-jian;MEI Dan;BAI Bin;Qingdao Branch;Navy Institute of Aeronautics Engineering;
WU Wen-hai;WANG Zi-jian;MEI Dan;BAI Bin;Qingdao Branch;Navy Institute of Aeronautics Engineering;
..............page:48-52
Preventing Methods of Airplane Structural Mode Coupling
GU Ji-gang;WANG Da-yong;MA Guo-feng;PLA Military Representative Office in Shenyang Aircraft Industries Co.Ltd.;Shenyang Aircraft Design & Research Institute;
GU Ji-gang;WANG Da-yong;MA Guo-feng;PLA Military Representative Office in Shenyang Aircraft Industries Co.Ltd.;Shenyang Aircraft Design & Research Institute;
..............page:53-55+63
The Redundancy Design and Redundancy Management of Avionic Large Screen Display
WANG Yong;Radar and Avionics Institute of AVIC;
WANG Yong;Radar and Avionics Institute of AVIC;
..............page:56-59
Test Method Using Antenna Port Conduction to Verify Receiver Compatible with High Level Electromagnetic Environment
XU Xiao-lin;WANG Ming-hao;LV Zhao-hui;Shenyang Aircraft Design & Research Institute;Environment Effects Aeronautic Science Key Laboratory of Electromagnetic;
XU Xiao-lin;WANG Ming-hao;LV Zhao-hui;Shenyang Aircraft Design & Research Institute;Environment Effects Aeronautic Science Key Laboratory of Electromagnetic;
..............page:60-63
High Altitude Helicopter Tower Hoisting Operation Technology Research
LIU Wei-dong;DUAN Wen-yun;SHEN Jian;WU Yi;State Grid General Aviation Company Limited;
LIU Wei-dong;DUAN Wen-yun;SHEN Jian;WU Yi;State Grid General Aviation Company Limited;
..............page:64-67+80
The Development of Test Device for Electric Control System of Engine Start
ZHANG Bing-ling;GAO Yong;FANG Zhen-xu;Naval Aviation Representative Shenyang Office;Shenyang Aircraft Design & Research Institute;
ZHANG Bing-ling;GAO Yong;FANG Zhen-xu;Naval Aviation Representative Shenyang Office;Shenyang Aircraft Design & Research Institute;
..............page:68-71
Research on Monitoring Model of Test Quality
DONG Zhan-pu;CHI Ying-jun;Airforce Representative Bureau in Shenyang District;PLA Military Representative Office in 117 Factory;
DONG Zhan-pu;CHI Ying-jun;Airforce Representative Bureau in Shenyang District;PLA Military Representative Office in 117 Factory;
..............page:72-75
The Inprovement of Stainless Steel and Titanium Alloy Conduit High Frequency Brazing
SHAO Bing;WU Yi;ZHANG Zhen;Naval Aviation Representative Shenyang Office;Shenyang Aircraft Industries Co.Ltd.;
SHAO Bing;WU Yi;ZHANG Zhen;Naval Aviation Representative Shenyang Office;Shenyang Aircraft Industries Co.Ltd.;
..............page:76-80
..............page:81-90
..............page:92