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Aircraft Design
1673-4599
2005 Issue 1
The Characteristic of Preliminary Design of M22 Small Coaxial Helicopter
Chen Ming;Hu Jizhong
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page:71-74
An Expert System of Tailoring Test Items in Laboratory Environmental Tests
Dong Baotong
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page:75-80
Planning of Flight Tests in an Aircraft Engineering Development Program
Qu Guijin
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page:67-70
Requirements for Development of Integrated SupportDesign Techniques for New Aircraft Engineering Development at Home
Liu Dongsheng
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page:62-66
Aeroplane Reliability and Maintainability Distribution Method Based on Multi - type aircrafts
Gao Hongxing;Zuo Hongfu;Wu Jingmin;Li Yanjun
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page:58-61
Design of a Simulated Electronic Warfare System
Wang Haiqing
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page:52-57
Study on Attack Trajectory of Pursuiting Fighter Based on Shooting Method
Wu Wenhai;Zhou Zhigang;Han Qiang;Yang Xiaofan
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page:47-51
EMC Design of a Communications System
Wang Tianshun
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page:40-46
Algorithm of Generating Flight Paths Using Cardinals Spline
Zhang Ruifeng;Ni Shihong;Yu Yingxiao
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page:37-39
Static And Dynamic Stability Analysis of a Flying Wing UCAV in Low Altitude Flight Phase
Wang Yanmin;Lu Yuping;Li Lirong
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page:32-36
Development of new Coupling Clamps for aluminum alloy pipes
Zheng Min;Zheng Yong
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page:26-31
An Applied Study of Repairing an Accumulator Fuel Tank for Prolonged Serivice Life
Wang Keran;Yang Guangshuang;Li Shubai;Yuan Zhongcheng
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page:20-25
An Analysis of Vibration Response of Structures to Aircraft Running
Xu Yan
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page:17-19
Optimal Layout about Wing & Fuselage on Bi - Fuselage Aircraft with High Aspect Ratio Straight Wing
Deng Yangchen;Wu Jingtao;He Jile
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page:14-16
A Study of BP Neural Network Model Based on GA in Fault Diagnosis of Wheel Brake System
Shi Yongsheng;Song Yunxue
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page:10-13
Finite Element Analysis of a Special Beam
Yu Xiukun;Li Qingzhong
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page:8-9
Fatigue Life Test of the Lower Portion of a Main Fuselage - Wing Bulkhead
Liu Chengyi
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page:1-7