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25 April 1997, Volume 18 Issue 2

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25 April 1997, Volume 18 Issue 2

AERODYNAM IC CHARACTERISTICS OF A HIGHLY SWEPTWING IN STEADY UNSTEADY PITCHING STATES AND EFFECT OF FLAPCONTROL AT LARGE INCIDENCE
Abstract( 2069 )

Xin Dingding;Yu Guangzhi;Yuan Li

1997, (2): 129-134.

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NEW METHOD FOR RELIABILITY ANALYSISOF DISCS'LCF LIFE
Abstract( 2158 )

Lu Shan;Lv Wenlin

1997, (2): 135-138.

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A NEW METHOD FOR PARALLEL BOUNDARY ELEMENT COMPUTATION
Abstract( 2268 )

Wang Renpeng;Zhang Xiaosong;Ye Tianqi

1997, (2): 139-145.

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RESIDUAL STRENGTH ESTIMATION OF COMPOSITE LAM INATES WITH DAMAGE
Abstract( 2298 )

Tang Xiaodong;Shen Zhen;Chen Puhui;Yang Shengchun;Yang Xu;Chen Yebiao

1997, (2): 146-152.

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STUDIES OF EFFECT OF THICKNESS ON FATIGUE CRACK GROWTH UNDER SINGLE-OVERLOADING CONDITIONS
Abstract( 2109 )

Gao Yali;Zhang Shijie;Liu Shaolun

1997, (2): 153-156.

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SEMI-PHYSICAL SIMULATION FOR A PILOTLESS PLANE
Abstract( 2349 )

Dong Juzhong;Kang Fengju

1997, (2): 157-162.

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NEURAL NETWORK BASED ADAPTIVE METHOD FOR MIMO NONLINEAR SYSTEM AND ITS APPLICATION TO FLIGHT CONTROL
Abstract( 1447 )

Zhou Xuan;Shi Zhongke

1997, (2): 163-167.

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DESIGN OF ADAPTIVE SLIDING MODE CONTROLLER FOR MANIPULATORS USING NEURAL NETWORKS
Abstract( 1801 )

Sun Fuchun;Sun Zengqi;Er Lianjie

1997, (2): 168-172.

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EVALUATION AND TEST OF NAVIGATION ACCURACY
Abstract( 1056 )

Jin Hong;Zhang Hongyue;Jin Zhong

1997, (2): 173-177.

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ACTIVE PASSIVE MULTISENSOR MULTITARGET STATE INFORMATION FUSION
Abstract( 1286 )

Li Jianxun;Jing Zhongliang;Yang Yunsheng;Dai Guanzhong;Jin Dekun

1997, (2): 178-182.

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NUMERICAL ANALYSIS OF THE EFFECTS OF MATERIAL PARAMETERS ON SUPERPLASTIC DIE BULGING PROCESS UNDER CONSTANT PRESSURE
Abstract( 1292 )

Li Yuanchun;Li Miaoquan;Wu Shidun

1997, (2): 183-188.

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STRUCTURE AND PROPERTY CONTROL OF THE TC11 ALLOY BLADE DIE FORGINGS
Abstract( 1456 )

Guo Hongzhen;Yao Zekun;Su Hua;Su Zuwu;Shi Xiangsheng;Zhao Buzhang;Sun Xuezheng;Wu Weigan

1997, (2): 189-195.

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MICROSTRUCTURE AND MECHANICAL PROPERTIES OF THREE DIMENSIONAL CARBON/SILICON CARBIDE COMPOSITES
Abstract( 2290 )

Xu Yongdong;Zhang Litong;Cheng Laifei

1997, (2): 196-201.

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TRANSONIC NUMERICAL SIMULATION FORW ING-BODY-PYLON-NACELLE CONF IGURATION
Abstract( 2773 )

Qiao Zhide;Sun Gang;LiDong;Yang Shuchi

1997, (2): 202-206.

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NEW SIMPLIFIED MODEL OF POST STALL TRANSIENTS IN AXIAL COMPRESSION SYSTEMS
Abstract( 2246 )

Hu Jun

1997, (2): 207-209.

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PRELIMINARY RESEARCH ON NUMERICAL SIMULATION OF TRANSONIC WALL INTERFERENCE FOR AIRCRAFT MODEL TESTS
Abstract( 2144 )

Fan Zhaolin;Zhang Yulun;He Zhong

1997, (2): 210-214.

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UNSTEADY WALL CORRECTIONS FOR A DELTA WING OSCILLATING IN PITCH TO VERY HIGH ANGLES OF ATTACK
Abstract( 1971 )

Zhang Wenhua;Li Zhiqiang;Ding Kewen;Huang Da

1997, (2): 215-219.

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TESTING RESEARCH OF LOAD SPECTRA OF AIRCRAFT
Abstract( 2417 )

Zhang Baofa;Fu Xiangjiong;Zhou Yuequan

1997, (2): 220-223.

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NEW METHOD OF SOLVING NONLINEAR EQUATION AND ITS APPLICATION TO FLUTTER ANALYSIS
Abstract( 1969 )

Yang Lifa;Liu Qiangang

1997, (2): 224-227.

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INTERACTION BETWEEN BRAKING AND LANDING GEAR VIBRATION
Abstract( 2140 )

Ku Yuao

1997, (2): 228-230.

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AEROENGINE NEURAL NETWORK CONTROL
Abstract( 1929 )

Tao Tao;Zhang Jiazhen

1997, (2): 231-233.

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STUDY OF IMPROVEMENT ON THE ACCURACY OF STATISTICAL LINEARIZATION AND HIGHER MOMENT PROPAGATION METHOD
Abstract( 1448 )

Lin Xiaohui;Cui Naigang;Liu Yuhua

1997, (2): 234-237.

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STUDY ON PROBLEMS OF NONLINEAR DYNAMIC INVERSION APPLICATION TO FLIGHT CONTROL SYSTEM
Abstract( 1756 )

Xu Jun;Zhang Minglian;Tu Baning

1997, (2): 238-242.

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RESEARCH ON THE MINIATURE MICRO FEED DRIVING MECHANISM AND ITS APPLICATION
Abstract( 1321 )

Yan Guozheng;Zhao Guoguang;Yu Chengye

1997, (2): 243-247.

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EXPERIMENTAL STUDY ON SURFACE STRENGTHENING OF ALUMINUM ALLOY BY LASER SHOCKING
Abstract( 1318 )

Zhang Hong;Tang Yaxin;Yu Chengye;Zhang Yongkang;Guo Dahao;Wu Hongxing

1997, (2): 248-251.

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DAMAGE DETECTION OF THE SMART COMPOSITE STRUCTURE USING WAVELET NEURAL NETWORKS
Abstract( 1373 )

Wu Yaojun;Tao Baoqi

1997, (2): 252-256.

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