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Aircraft Design
FQ: 双月
AD of Publication: 辽宁省沈阳市
Lanuage: 中文;
ISSN: 1673-4599
CN: 21-1339/V
YP: 1980
Url: 中国航空工业沈阳飞机设计研究所集团公司
Recommended Journals
Aircraft Design
2001 -02
Catalog
THE VULNERABILITY ANALYSIS IN AIRCRAFT SURVIVABILITY RESEARCH Li Jinrui, Li Tian, Wang Yongqing (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
TO RESEARCH AIRCRAFT GLOBAL PARAMETER OPTIMIZATION DESIGN WITH GEOMETRIC PROGRAMMING MENTIONED Han Ying, Liu Tianfeng (Shenyang Institute of Aeronautical Engineering, shenyang 110035, China)
INVESTIGATION OF COMPRESSOR MODEL TEST FOR RCS REDUCTION Cheng Daguang (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
EFFECT OF AIRFRAME ON SUPERSONIC INLET PERFORMENCE Zhu Yu , Li Chunxuan , Li Tian(1. Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)(2. National Laloratory for Computational Fluid Dynamics, Beijng University of Aeronautics and Astronautics, Beijmg 100083, China)
STUDY OF FDLGTHER SELF-REPAIRED CONTROL SYSTEM VISUALIZATION BASED ON MATLAB DIGITAL SIMULATION SOFTWARE Zhang Defa, Hu Shousong , Wang Xingning(1. Shenyang Aircraft Design & Research Institute, shenyang 110035, China)(2. The Automaic Control Department,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
A VALUE & A CRITERION Wang Yunhui , Li Luyu (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
SHARED-MEMORY NETWORKING ARCHITECTURE-ORIENTED AIRCRAFT REAL-TIME SIMULATIONS RING NET Li Yuezhong, Zhang Yong(1. Shenyang Institute of Aeronautical Engineeing, Shenyang 110034, China) (2. Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
THE APPLICATION OF THE DAMPING MATERIAL IN REDUCING VIBRATING OF CANNON VIBRATING IN AIRCRAFT Chen Zhongming, He Lianzhu, Huang Jichi ( Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
CONIC METHOD ON SOLVING NONLINEAR EQUATION Deng Yangchen, Zhang Yining, Li Zhengneng(1. Shenyang Aircraft Design & Research Institute, Shenyang 110035, China) (2. Dept of Flight Vehicle Design and Applied Mechanics, Beijing Univ. of Aero, and Astra ,Beijing 100083, China)
LANDING GEAR ELASTIC DEFORMATION IMPACT ON STRUCTURE STRENGTH Shao Yongqi (Shenyang Aicraft Design & Research Institute, Shenyang 110035, China)
MATHEMETICAL MODEL RESEARCH ON AIRCRAFT LANDING GEAR DAMPER Shui Fucheng, Lu Hua (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
THE STRUCTURRAL VIBRATION BREAKDOWN ANALYSIS RESEARCH ON THE FIGHTER-XX CENTERLINE DROP TANK'S TAIL CONE Zhu Guangrong (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
ELECTROSTATIC DISCHARGE AND PROTECTED Wang Tianshun (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
DESIGN AND REALIZATION OF THE RELAY BOXS COMPUTER AUXILIARY TEST Wu Chao (SAC Airforce Representatives, Shenyang, 110034, China)
CALIBRATION METHOD FOR ACCELEROMETER Li Dechun, Meng Xianshu, Zheng Yi, Cui Wei (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
CONVERTING METHOD RCSEARCH ON AIRCRAFT FIELD-TESTED ENVIRONMENT TEMPERATURE DATE Liu Dongsheng (Shenyang Aircraft Design & Research Institute, Shenyang 110035, China)
2001 Issues:  [02] [03] [04]
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