1673-4599
2001 Issue 2
THE VULNERABILITY ANALYSIS IN AIRCRAFT SURVIVABILITY RESEARCH
Li Jinrui;Li Tian;Wang Yongqing
Li Jinrui;Li Tian;Wang Yongqing
..............page:1-7
TO RESEARCH AIRCRAFT GLOBAL PARAMETER OPTIMIZATION DESIGN WITH GEOMETRIC PROGRAMMING MENTIONED
Han Ying;Liu Tianfeng
Han Ying;Liu Tianfeng
..............page:8-10
INVESTIGATION OF COMPRESSOR MODEL TEST FOR RCS REDUCTION
Cheng Daguang
Cheng Daguang
..............page:11-13
EFFECT OF AIRFRAME ON SUPERSONIC INLET PERFORMENCE
Zhu Yu;Li Chunxuan;Li Tian
Zhu Yu;Li Chunxuan;Li Tian
..............page:14-17,21
STUDY OF FILGTHER SELF- REPAIRED CONTROL SYSTEM VISUALIZATION BASED ON MATLAB DIGITAL SIMULATION SOFTWARE
Zhang Defa;Hu Shousong;Wang Xingning
Zhang Defa;Hu Shousong;Wang Xingning
..............page:18-21
A VALUE & A CRITERION
Wang Yunhui;Li Luyu
Wang Yunhui;Li Luyu
..............page:22-24,37
SHARED-MEMORY NETWORKING ARCHITECTURE-ORIENTED AIRCRAFT REAL-TIME SIMULATIONS RING NET
Li Yuezhong;Zhang Yong
Li Yuezhong;Zhang Yong
..............page:25-30
THE APPLICATION OF THE DAMPING MATERIAL INREDUCING VIBRATING OF CANNON VIBRATING IN AIRCRAFT
Chen Zhongming;He Lianzhu;Huang Jichi
Chen Zhongming;He Lianzhu;Huang Jichi
..............page:31-33
CONIC METHOD ON SOLVING NONLINEAR EQUATION
Deng Yangchen;Zhang Yining;Li Zhengneng
Deng Yangchen;Zhang Yining;Li Zhengneng
..............page:34-37
..............page:38-43
MATHEMETICAL MODEL RESEARCH ON AIRCRAFT LANDING GEAR DAMPER
Shui Fucheng;Lu Hua
Shui Fucheng;Lu Hua
..............page:44-51
THE STRUCTURRAL VIBRATION BREAKDOWN ANALYSIS RESEARCH ON THE FIGHTER- XX CENTERLINE DROP TANK'S TAIL CONE
Zhu Guangrong
Zhu Guangrong
..............page:52-54
ELECTROSTATIC DISCHARGE AND PROTECTED
Wang Tianshun
Wang Tianshun
..............page:55-59
..............page:60-66
CALIBRATION METHOD FOR ACCELEROMETER
Li Dechun;Meng Xianshu;Zheng Yi;Cui Wei
Li Dechun;Meng Xianshu;Zheng Yi;Cui Wei
..............page:67-74
..............page:75-80