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Aircraft Design
1673-4599
2001 Issue 3
THE ALL LIFE-CYCLE PROCESS MODELLING METHOD AND TECHNIQUE FOR AIRCRAFT
Zhang li;Liu Mengzhao;Cui Degang
..............page:1-5
STRUCTURE FAULT DIAGNOSIS BASED ON HIERARCHIC RESIDUAL SORTING NEURAL NETWORK FOR A FIGHTER
Hu Shousong;Wang Chenxi;Zhang Defa
..............page:6-11
CONTROL RECONFIGURATION OF NONLINEAR FLIGHT CONTROL SYSTEMS
Zhang Ping;Chen Zongji
..............page:12-15,21
ADVANCED AND SOME PROBLEMS OF PREDICTIVE TECHNIQUE FOR SERVICE LIFE OF AIRCRAFT
Chen Yueliang;Lu Guozhi;Duan Chengmei
..............page:16-21
THE COMPOSIT S-N CUNVE EQUATION ON MIDDLE AND LONG FATIGUE LIFE RANGE
Deng yangchen;Zhang yining;Li Zhengneng
..............page:26-28
STRUCTURAL FATIGUE LIFE PREDICTION UNDER RANDOM VIBRATION LOADINGS
Dong Baotong;Shi Rongming;Zhu Guangrong
..............page:36-41
OPTIMAL DISPOSAL OF SENSOR FOR MEASURING OIL VOLUME IN AIRCRAFT TANK
Liu Jianmin;Zhuang Damin;Li Degang
..............page:42-45
KINETIC HEATING OF AIRBONE WEAPONS
Gao Zhensheng
..............page:46-54
ANALYSIS ON ELECTRIC BONDING FOR COMPOSITE MATERIALS
Wang Tianshun
..............page:55-60
THE USE OF MULTIPLE THREADS IN AN OBJECT-ORIENTED REAL-TIME SIMULATION
Li Yuezhong;Zhang Yong
..............page:61-65
FIELD RELIABILITY MONITOR FOR MILITARY AIRCRAFT
Chang Wenbing
..............page:66-68
THE EXAMPLE OF FIXING THE VENTRAL FINS BREAKDOWN ON ONE TYPE AIRCRAFT
Chen Zhongming;Wang Xiangming
..............page:69-72
SUEVEY OF MOTION PHOTOGRAPHY OF PLANE-CARRIED MISSILES
Wang Chuang;Wang Wei
..............page:73-75