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Journal of Nanjing University of Aeronautics & Astronautics
FQ: bimonthly
AD of Publication: China
Lanuage: English
ISSN: 1005-2615
CN: 32-1429/V
YP: 1956
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Journal of Nanjing University of Aeronautics & Astronautics
1989 -04
Catalog
Research on Active Dynamic Antiresonant Vibration Isolator——Part 2 Experimental Study Zhou Weiming Gu Zhongquan
Optimal Design of Composite Wing Structures to Satisfy Flutter Speed Constraint Huang Chuanqi Qiao Xin
The Analysis of Dynamic Stiffness of Aircraft Control System and Inherent Vibration Characteristics Coupled with Rudder Lin Xiaofen Ang Haisong Xia Daojia
The Block Chebyshev-Lanczos Method for Solving Large Symmetric Eigenvalue Problems Zhou Shuquan Dai Hua
Aeroassisted Noncoplanar Orbital Transfer of Space shuttle Chen Shi Zhou Donglin
A New Wake Modeling Technology Using Circulation Contours and Its Application to Rotor Rigid Wake Lou Wujiang Wang Shicun
The Influences of Free-Flow Turbulent Intensity and Surface Roughness on Boundary-Layer Transition by Calculation Cheng Guofeng Tang Lei Hou Guohong
A Kind of Semi-Implicit Difference Schemes for Schrdinger Type Equation Zhao Ning Dai Jiazun
Double Exposure Holography with Recorded Beams Modulated by the Plate Motion Cai Yunliang
The Elimination of Force Eccentricity Effect on Optical Fiber Force Sensor Li Weixuan Tao Baoqi
A Petri Net Method for Planed Management System Research Huang Shengguo Lue Bing Yuan Xin
A Mixed Labelling Algorithm for Solving Minimum Cost Flow Problem in the Network Ning Xuanxi
Design of Robust Low-Order Adaptive Controller Zhang Haiqing Lin Daoyuan
Robust Pole Assigment of System by Output Feedback Jiang Changsheng
Optimal Distributed Kalman Filter Using Successive Orthogonalization Procedure Wang Shuhua
Critical Review of classical Model Reductions Hu Shousong Lin Daoyuan
The Study of Distributed Kalman Filter Application to GPS/INS Integrated Navigation System Yuan Xin Liu Jianye
A Fast Algorithm for Multiplicative Inverses Based on the Normal Basis Representation Xu Dazhuan
Proof of Mechanization for Geometry Theorem by Gravity Center coodinate Huang Ming
Improved Finite Element Analysis Model by Modal Test Tang Deman
1989 Issues:  [04] [03] [02] [01]
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