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Acta Aeronautica ET Astronautica Sinica
1000-6893
1998 Issue 5
COMMENT ON TWO-DIMENSIONAL UNSTEADY SEPARATION CRITERIA
Lü Zhiyong;Jia Zhigang
..............page:636-640
GRAPHITIZATION OF PAN-BASED CARBON FIBRE BY AN ELECTRIC CURRENT PULSE
Shen Yifu;Guo Xiaonan;Zhang Kun;Li Shunlin;Zhou Benlian
..............page:628-630
VARIABLE STRUCTURE CONTROLLER DESIGN FOR GUIDED BOMB
Wang Huangang;Shen Yi;Wang Guanzhu
..............page:624-627
SPECTRA ESTIMATION OF THE RANDOM STATOR CURRENT SIGNAL IN THE DIRECT-TORQUE-CONTROL SYSTEM
Zhang Junchang;Li Yanjun;Zhou Ziquan;Lü Jie
..............page:621-623
RESEARCH ON RELIABILITY LIFE FORECASTING BASED ON MODEL-BUILDING OF SUPER-PATH TIME FOR AEROSPACE RELAYS
Zhai Guofu;Zhao Xinmin;Liu Maokai;Zhang Deshuang
..............page:617-620
STUDY FOR THE THEORY OF THE COMBINATIONS OF GPS CARRIER PHASE OBSERVATIONS
Chang Qing;Liu Zhongkan;Zhang Qishan
..............page:612-615
ADAPTIVE OBSERVER BASED ON RADIAL BASIS FUNCTION OF FUZZY SYSTEMS
Wen Xin;Zhang Hongyue;Zhou Lu
..............page:608-611
MODEL VALIDATION WITH STRUCTURED UNCERTAINTY
Shi Feng;Xu Demin;Wu Xuguang
..............page:603-607
MODELING AND COMPENSATION OF A SOFT-SWITCHING-COMBINATION CONVERTER
Xing Yan;Yan Yangguang;Zhao Xiuke
..............page:597-602
ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS
Shen Jinglai;Gao Jinyuan
..............page:592-596
NUMERICAL SIMULATION AND DEFECT PREDICTION OF THE CUP-ROD AXISYMMETRIC COMBINED EXTRUSION
Fan Jianwen;Wu Shidun;Li Miaoquan
..............page:588-591
UNSTEADY CHARACTER OF VORTEX BREAKDOWN FLOW FIELDS
Ge Lixin;Li Chunxuan
..............page:553-555
EROSION WEAR BEHAVIOUR AND MODEL OF ABRADABLE SEAL COATING
Yi Maozhong;Huang Baiyun;He Jiawen;Zhou Huijiu
..............page:546-552
SIZE LIMITATION OF ACTFEL'S CAUSED BY TRANSPARENT ITO CONDUCTOR AND ITS IMPROVEMENT
Liu Jiansheng;Li Zheng;Zhang Qishan
..............page:541-545
TARGET TRACKING BASED ON FUSION OF MULTI-SENSOR
Zhou Rui;Shen Gongxun;Fang Jiancheng;Zhu Shiping
..............page:536-540
ATTITUDE DETERMINATION WITH TWO BASELINES BASED ON GPS
Liao Xiangqian;Huang Shunji;Zhang Xiaoling
..............page:531-535
ON REAL-TIME MODEL AND HYBRID ADAPTIVE VIBRATION CONTROL OF SMART ROTOR BLADES
Ma Kougen;Joerg Melcher
..............page:525-530
NEW METHOD OF DRAWING UP AIRCRAFT LOAD SPECTRUM
Zhang Fuze
..............page:518-524
NUMERICAL STUDY OF THE TURBULENT FLOW IN THE PLANE CASCADE USING A NON-LINEAR k-ε MODEL
Xu Jingle;Xu Zhong;Huang Shujuan
..............page:513-517
ASSESSMENT OF CONCEPTUAL DESIGN FOR AN ADVANCED TRAINING AIRCRAFT USING TRAINING EFFICIENCY
Huang Jun;Cao Huaizhi;Wu Wenzheng;Wang Rongchao
..............page:581-584
EXPERIMENTAL STUDY OF A MULTIPLE SQUEEZE FILMS ELECTRORHEOLOGICAL DAMPER FOR VIBRATION CONTROL OF ROTOR SYSTEM
Yao Guozhi;Qiu Yang;Fang Tong;Meng Guang;Fan Yanbin
..............page:570-574
EFFECT OF HONEYCOMB ON AERODYNAMIC PERFORMANCE AND RADAR CROSS SECTION OF INLET
Liang Dewang;Guo Rongwei;Zhao Minggui
..............page:567-569
IDENTIFICATION OF AERODYNAMIC COEFFICIENTS USING MAXIMUM LIKELIHOOD METHOD
Xia Zhixun;Sheng Xiangrao;Tang Guojing
..............page:564-566
DYNAMIC AIRFLOW TEMPERATURE MEASUREMENT
Cui Jiang;Shou Shengde
..............page:560-563
STUDY OF NUMERICAL SIMULATION WITH UNSTRUCTURED GRID ON TURBULENT FLOW IN ROTATING CENTRIFUGAL IMPELLER
Zhang Chuhua;Liu Zhengxian;Gu Chuangang;Miao Yongmiao
..............page:556-559