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Aircraft Design
1673-4599
2015 Issue 3
Aeroelastic and minimum-weight optimization design of a high-aspect-ratio composite wing
ZHU Jiang-hui;CHEN Yan;SUN Yong-jun;Chinese Flight Test Establishment;
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page:1-4
Sensitivity analysis of primary parameters in preliminary design of a large military transport
HAN Fang-yuan;HUANG Jun;Ecole Centrale de Pékin;Beijing University of Aeronautics and Astronautics;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
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page:5-10
Dynamic analysis of composite materials wing structure
ZHANG Ya-bin;GAO Heng-xuan;LI Shu;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
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page:11-15
Kills,Sorties and dollars
ZHANG Yong;Shenyang Aircraft Design & Research Institute;
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page:16-19
Fatigue crack growth behavior in friction stir welded structural joints
WANG Wei;LIU Jing-lin;Naval Aviation Representative Shenyang Office;Shenyang Aircraft Design & Research Institute;
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page:20-23
Macro-structural lightweight analysis for aircraft parts made by additive manufacturing technology
WANG Wei;YUAN Lei;WANG Xiao-wei;Navy Aviation Representative Shenyang Office;Shenyang Aircraft Industries CO.;Ltd;
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page:24-28
The design and simulation of flight control system for UAV based on signed domination
CHEN Yin-jun;WU Wen-hai;WANG Zhong-hua;Nanchang Aeronautical University;Qingdao Branch Naval Aeronautical Engineering Institute;
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page:29-32
Flight control system’s robustness characteristics of structural configuration research
LIU Chang-xiu;LI Ji-guang;DONG Yan-fei;School of Civil Aviation;Nanjing University of Aeronautics and Astronautics;School of Aircraft Engineering;Nanchang Aeronautics University;
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page:33-36
The application study of stainless steel in titanium alloy stabilization craft design
JIANG Jia-yu;SUN Guo-xing;HE Dan;Shenyang Office;Naval Department of Equipment of the PLA;Shenyang Aircraft Design & Research Institute;Shenyang Aerospace University;
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page:37-41
Key technical research of unmanned combat air system
WU Wen-hai;LIU Jin-tao;DIAO Jun;Qingdao Branch;Naval Aeronautical Engineering Institude;
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page:42-46+54
A method to component’s inventory based on the reliability life distribution
LV De-feng;GUO Xiu-cheng;GAO Bin-hua;WANG Cheng;The Unit 94938 of PLA;
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page:47-49+70
Civil aircraft troubleshooting support technology research based on case-based reasoning
HU Yi;LI Fei-min;JIAO Yi;Chinese Flight Test Establishment;
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page:50-54
A two-echelon two-indenture inventory model for repairable spare parts based on VMI
XU Juan;ZUO Hong-fu;SUN Lei;School of Civil Aviation;Nanjing University of Aeronautics and Astronautics;Shanghai Aircraft Customer Service Co.;Ltd;
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page:55-60
Application of eye tracking technology in foreign military aviation
LU Shan-shan;WANG Qing-min;YAO Yong-jie;LI Ke-hua;LIU Qiu-hong;The Naval Medical Research Institute;
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page:61-64
Technical research based of IETM information application
HUANG Yong;Shenyang Aircraft Design & Research Institute;
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page:65-70
Evaluation of uncertainty of measurement of digital pressure gauges
ZHENG Yi;Shenyang Aircraft Design & Research Institute;
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page:71-73
Analysis of the new edition of GJB150A
CHI Ying-jun;LIU Jing-dang;Airforce Representative Bureau in Shenyang District;Shenyang Aircraft Industry Co. Ltd.;
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page:74-80
fei ji she ji gao yue
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page:82