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25 December 1998, Volume 19 Issue 6

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25 December 1998, Volume 19 Issue 6

论文

AIRFOIL SHAPE OPTIMIZATION FOR HIGH AERODYNAMIC EFFICIENCY/LOW OBSERVABILITY
Abstract( 2256 )

Zhu Ziqiang;Zhu Yikun;Li Haiming

1998, (6): 2-7.

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STUDY ON NONLINEAR CONTINUOUS DAMAGE CUMULATIVE MODEL FOR UNIAXIAL FATIGUE
Abstract( 3099 )

Shang Deguang;Yao Weixing

1998, (6): 8-17.

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STABILITY MARGIN ANALYSIS OF THE MULTILOOP FLIGHT CONTROL SYSTEMS
Abstract( 2912 )

Wu Bin;Cheng Peng

1998, (6): 18-22.

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FAULT TOLERANT DECENTRALIZED FILTERING METHOD
Abstract( 2059 )

Qiu Hongzhuan;Zhang Hongyue

1998, (6): 23-28.

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NEW PRINCIPLE OF FIBER GYROSCOPE IN NON SAGNAC EFFECT VIEWED PHYSICAL METHODOLOGY
Abstract( 2368 )

Zhang Jiahua;Li Yingzi

1998, (6): 29-34.

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METHODS OF STRUCTURE FAULT DETECTION AND RECONFIGURATION OF SELF REPAIRING CONTROL LAW FOR A FIGHTER
Abstract( 2365 )

Hu Shousong;Guo Wei

1998, (6): 35-38.

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APPLICATION OF ARTIFICIAL NEURAL NETWORKS IN INTELLIGENT CAD OF AIRCRAFT PRELIMINARY CONFIGURATION DESIGN
Abstract( 2224 )

Liu Zhenkai;Gui Zhonghua;Cai Qing

1998, (6): 39-45.

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MACHINING FEATURE RECOGNITION BASED ON SHAPE FEATURE BASED MODEL
Abstract( 1435 )

He Xiaozhao;Shen Mei;Jiang Xieming;Zhang Tiechang

1998, (6): 46-51.

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STUDY AND APPLICATION OF CNC SYSTEM FAULT DIAGNOSIS BASED ARTIFICIAL NEURAL NETWORKS AND EXPERT SYSTEM
Abstract( 2029 )

Wang Runxiao;Qin Xiansheng

1998, (6): 52-56.

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THEORETICAL AND EXPERIMENTAL STUDY ON CONTACT CHARACTERISTICS OF SPIRAL BEVEL GEARS FOR AEROENGINES WITH ELASTIC SUPPORTS
Abstract( 2086 )

Wang Sanmin;Dong Haijun;Li Jiqing

1998, (6): 57-60.

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DEVELOPMENT OF A METHOD AND APPLICATION FOR IMPROVING THE PILOT MODELING ACCURACY
Abstract( 2016 )

Xu Zhongxiang;Qu Xiangju

1998, (6): 61-66.

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SOLUTION OF QPNS EQUATIONS TO SIMULATE AERODYNAMIC FORCES AND HEATING FOR ROTATION BODIES AT HIGH SPEED USING FINITE ELEMENT METHOD
Abstract( 1483 )

Zhang Guofu;Hua Xiqing

1998, (6): 67-70.

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NUMERICAL ANALYSES OF STRESS WAVE PROPAGATION IN A VARIABLE SECTION BAR
Abstract( 1404 )

Cao Zengqiang;She Gongfan;Zhou Tingqing

1998, (6): 71-75.

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EFFECT OF PROOF TESTING ON FATIGUE STRENGTH OF CERAMICS
Abstract( 1679 )

Lü Baotong;Wang Hong

1998, (6): 76-79.

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DESIGN AND SIMULATION OF A NEW KIND OF COMBINATIVE INTELLIGENCE FLIGHT CONTROL SYSTEM AND INTEGRATED FIRE/FLIGHT CONTROL SYSTEM OF ADVANCED ARMED HELICOPTER
Abstract( 1788 )

Jiang Changsheng;Guo Shujun;Wang Pihong;Yang Keming;Sun Longhe

1998, (6): 80-86.

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MULTISENSOR INFORMATION FUSION FOR TARGET IDENTIFICATION USING A RADAR SENSOR AND AN INFRARED SENSOR
Abstract( 1743 )

Hao Chongyang;Tang Wenbin

1998, (6): 87-90.

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EFFECTIVE METHOD FOR 3 D AIRCRAFT TARGET AUTOMATIC RECOGNITION
Abstract( 2172 )

Liao Wenjian;Cheng Yu

1998, (6): 91-96.

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BAYESIAN APPROACH TO HIGH RESOLUTION DIRECTION OF ARRIVAL ESTIMATION
Abstract( 2242 )

Chen Jianfeng;Liu Chunming;Huang Jianguo

1998, (6): 97-100.

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FATIGUE CHARACTERIZATION OF COMPOSITE HONEYCOMB CORE SANDWICH PANELS AFTER LOW VELOCITY IMPACT
Abstract( 2428 )

Cheng Xiaoquan;Kou Changhe;Li Zhengneng

1998, (6): 101-104.

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ESTABLISHING THE KNOWLEDGE BASE OF PARAMETERS FOR SHAPING TUBE AND BAR PRODUCTS ON THE NEURAL NETWORK
Abstract( 2300 )

Qi Lehua;Hou Junjie;Yang Fang;Li Hejun

1998, (6): 105-108.

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TWO DIMENSIONAL UP AND DOWN METHOD
Abstract( 2443 )

Fu Huimin;Yin Gang

1998, (6): 109-114.

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