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AIRFOIL SHAPE OPTIMIZATION FOR HIGH AERODYNAMIC EFFICIENCY/LOW OBSERVABILITY
Zhu Ziqiang;Zhu Yikun;Li Haiming
1998, (6): 2-7.
PDF [ 279 K ]( 772 ) HTML
STUDY ON NONLINEAR CONTINUOUS DAMAGE CUMULATIVE MODEL FOR UNIAXIAL FATIGUE
Shang Deguang;Yao Weixing
1998, (6): 8-17.
PDF [ 494 K ]( 1003 ) HTML
STABILITY MARGIN ANALYSIS OF THE MULTILOOP FLIGHT CONTROL SYSTEMS
Wu Bin;Cheng Peng
1998, (6): 18-22.
PDF [ 301 K ]( 1857 ) HTML
FAULT TOLERANT DECENTRALIZED FILTERING METHOD
Qiu Hongzhuan;Zhang Hongyue
1998, (6): 23-28.
PDF [ 321 K ]( 776 ) HTML
NEW PRINCIPLE OF FIBER GYROSCOPE IN NON SAGNAC EFFECT VIEWED PHYSICAL METHODOLOGY
Zhang Jiahua;Li Yingzi
1998, (6): 29-34.
PDF [ 352 K ]( 1176 ) HTML
METHODS OF STRUCTURE FAULT DETECTION AND RECONFIGURATION OF SELF REPAIRING CONTROL LAW FOR A FIGHTER
Hu Shousong;Guo Wei
1998, (6): 35-38.
PDF [ 257 K ]( 700 ) HTML
APPLICATION OF ARTIFICIAL NEURAL NETWORKS IN INTELLIGENT CAD OF AIRCRAFT PRELIMINARY CONFIGURATION DESIGN
Liu Zhenkai;Gui Zhonghua;Cai Qing
1998, (6): 39-45.
PDF [ 281 K ]( 1051 ) HTML
MACHINING FEATURE RECOGNITION BASED ON SHAPE FEATURE BASED MODEL
He Xiaozhao;Shen Mei;Jiang Xieming;Zhang Tiechang
1998, (6): 46-51.
PDF [ 285 K ]( 638 ) HTML
STUDY AND APPLICATION OF CNC SYSTEM FAULT DIAGNOSIS BASED ARTIFICIAL NEURAL NETWORKS AND EXPERT SYSTEM
Wang Runxiao;Qin Xiansheng
1998, (6): 52-56.
PDF [ 239 K ]( 684 ) HTML
THEORETICAL AND EXPERIMENTAL STUDY ON CONTACT CHARACTERISTICS OF SPIRAL BEVEL GEARS FOR AEROENGINES WITH ELASTIC SUPPORTS
Wang Sanmin;Dong Haijun;Li Jiqing
1998, (6): 57-60.
PDF [ 263 K ]( 747 ) HTML
DEVELOPMENT OF A METHOD AND APPLICATION FOR IMPROVING THE PILOT MODELING ACCURACY
Xu Zhongxiang;Qu Xiangju
1998, (6): 61-66.
PDF [ 312 K ]( 493 ) HTML
SOLUTION OF QPNS EQUATIONS TO SIMULATE AERODYNAMIC FORCES AND HEATING FOR ROTATION BODIES AT HIGH SPEED USING FINITE ELEMENT METHOD
Zhang Guofu;Hua Xiqing
1998, (6): 67-70.
PDF [ 259 K ]( 685 ) HTML
NUMERICAL ANALYSES OF STRESS WAVE PROPAGATION IN A VARIABLE SECTION BAR
Cao Zengqiang;She Gongfan;Zhou Tingqing
1998, (6): 71-75.
PDF [ 367 K ]( 1105 ) HTML
EFFECT OF PROOF TESTING ON FATIGUE STRENGTH OF CERAMICS
Lü Baotong;Wang Hong
1998, (6): 76-79.
PDF [ 250 K ]( 524 ) HTML
DESIGN AND SIMULATION OF A NEW KIND OF COMBINATIVE INTELLIGENCE FLIGHT CONTROL SYSTEM AND INTEGRATED FIRE/FLIGHT CONTROL SYSTEM OF ADVANCED ARMED HELICOPTER
Jiang Changsheng;Guo Shujun;Wang Pihong;Yang Keming;Sun Longhe
1998, (6): 80-86.
PDF [ 375 K ]( 863 ) HTML
MULTISENSOR INFORMATION FUSION FOR TARGET IDENTIFICATION USING A RADAR SENSOR AND AN INFRARED SENSOR
Hao Chongyang;Tang Wenbin
1998, (6): 87-90.
PDF [ 256 K ]( 821 ) HTML
EFFECTIVE METHOD FOR 3 D AIRCRAFT TARGET AUTOMATIC RECOGNITION
Liao Wenjian;Cheng Yu
1998, (6): 91-96.
PDF [ 326 K ]( 527 ) HTML
BAYESIAN APPROACH TO HIGH RESOLUTION DIRECTION OF ARRIVAL ESTIMATION
Chen Jianfeng;Liu Chunming;Huang Jianguo
1998, (6): 97-100.
PDF [ 266 K ]( 757 ) HTML
FATIGUE CHARACTERIZATION OF COMPOSITE HONEYCOMB CORE SANDWICH PANELS AFTER LOW VELOCITY IMPACT
Cheng Xiaoquan;Kou Changhe;Li Zhengneng
1998, (6): 101-104.
PDF [ 144 K ]( 691 ) HTML
ESTABLISHING THE KNOWLEDGE BASE OF PARAMETERS FOR SHAPING TUBE AND BAR PRODUCTS ON THE NEURAL NETWORK
Qi Lehua;Hou Junjie;Yang Fang;Li Hejun
1998, (6): 105-108.
PDF [ 258 K ]( 624 ) HTML
TWO DIMENSIONAL UP AND DOWN METHOD
Fu Huimin;Yin Gang
1998, (6): 109-114.
PDF [ 184 K ]( 927 ) HTML
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