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25 April 1998, Volume 19 Issue 2

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25 April 1998, Volume 19 Issue 2

STATUS AND DEVELOPMENT ON EFFECTS OF IMPURITIES AND RARE EARTH ELEMENTS IN Al Li ALLOYS
Abstract( 1609 )

Meng Liang;Zheng Xiulin

1998, (2): 129-136.

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HIGH ANGLE OF ATTACK DYNAMIC DERIVATIVE EXPERIMENT OF STANDARD DYNAMIC MODEL
Abstract( 1707 )

Zhao Zhongliang;Ren Bin;Huang Xuhui

1998, (2): 137-141.

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RESEARCH ON APPLICATION PROBLEMS OF LINEARIZATION VIA FEEDBACK FLIGHT CONTROL TECHNIQUE
Abstract( 1415 )

Zhang Shuguang;Fang Zhenping

1998, (2): 142-146.

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STUDY OF MOTION CHARACTERISTICS OF TARGET SENSITIVITY PROJECTILE DURING THE DECELERATION AND STABLE SCANNING PHASE
Abstract( 1991 )

Sun Le;Han Zipeng;Li Fengchang;Liu Shiping

1998, (2): 147-151.

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GRID GENERATION METHOD IN CFD AND ITS APPLICATION
Abstract( 2977 )

Zhu Ziqiang;Li Jing;Zhang Zhengke;Chen Zemin;Wu Ziniu;Li Haiming

1998, (2): 152-158.

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QUANTITATIVE DETERMINATION OF IMPACT DAMAGE REGION AND DAMAGE EXTENTS IN COMPOSITE MATERIALS BY FIBRE OPTIC IMAGE
Abstract( 1316 )

Xu Ningguang;Sun Liangxin;Huang Hansong

1998, (2): 159-163.

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METHOD OF MEASURING DAMAGE VARIABLE D(E) WITH CHANGING CROSS SECTION SPECIMEN
Abstract( 1422 )

Zhao Yinyan;Zhou Li

1998, (2): 164-168.

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NONLINEAR ROBUST CONTROL FOR FLIGHT CONTROL SYSTEMS
Abstract( 1500 )

Xu Jun;Zhang Minglian;Song Zishan

1998, (2): 169-172.

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NONLINEAR FLIGHT CONTROL USING ADAPTIVE NEURAL NETWORK
Abstract( 1697 )

Cui Hutao;Geng Yunhai;Li Aoshuang;Yang Di

1998, (2): 173-178.

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MOTION TRACKING VARIABLE STRUCTURE GUIDANCE FOR PASSIVE HOMING MISSILE
Abstract( 1823 )

Zhou Di;Mu Chundi

1998, (2): 179-184.

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BOOTSTRAP FILTERING OF SYSTEM WITH RANDOM CHANGING STRUCTURE
Abstract( 1444 )

Wu Sentang;Xu Guangfei;Tang Yong

1998, (2): 185-189.

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SIMULATION OF COVARIANCE ANALYSIS DESCRIBING EQUATION TECHNIQUE FOR TERMINAL WEAPON DELIVERY
Abstract( 1454 )

Jin Huiming;Qu Yepin;Tong Mingan

1998, (2): 190-194.

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NEW MODELLING STRATEGY FOR SEQUENTIAL DISCRETE EVENT SIMULATION——MESSAGE DRIVEN METHOD
Abstract( 1616 )

Lin Jian;Mao Jingying

1998, (2): 195-199.

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BAYESIAN METHOD FOR THE CASE CONTAINMENT ASSESSMENT
Abstract( 1321 )

Wu Xuming;Ning Xuanxi

1998, (2): 200-204.

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COLLABORATIVE GROUP DECISION MODEL AND ITS GRADIENT SOLUTION
Abstract( 1063 )

Chen Yehua;Qiu Wanhua

1998, (2): 205-210.

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RESEARCH ON THE POST STALL PERFORMANCE OF AN AXIAL COMPRESSOR WITH THE TREATED CASING
Abstract( 2321 )

Zhu Junqiang;Du Hui;Li Jun

1998, (2): 211-215.

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RELIABILITY ANALYSIS METHOD OF INCOMPLETE FATIGUE LIFE DATA AND APPLICATION
Abstract( 1546 )

Xiong Junjiang;Wu Zhe;Gao Zhentong

1998, (2): 216-219.

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HYBRID DAMPING WITH LOWER CONTROL VOLTAGE
Abstract( 1199 )

Zhang Xinong;Chen Ling;Zhang Jinghui

1998, (2): 220-223.

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AIRCRAFT ECS RELIABILITY DESIGN AND EVALUATION
Abstract( 1521 )

Wei Hong;Wang Jun

1998, (2): 224-227.

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PROGRESS OF ULTRASONIC FATIGUE
Abstract( 1406 )

Tao Hua

1998, (2): 228-231.

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STRENGTH STUDY OF COMPOSITE STRUCTURE WITH LOW ENERGY IMPACT DAMAGE
Abstract( 1310 )

Tong Mingbo;Chen Puhui;Zeng Jianjiang

1998, (2): 232-235.

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REFINED DELAMINATION MODEL FOR LAMINATED BEAMS
Abstract( 1439 )

Shu Xiaoping

1998, (2): 236-239.

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DESIGN OF THE COMMAND AND STABILITY AUGMENTATION SYSTEMS OF ARMED HELICOPTERS
Abstract( 1541 )

Tang Yongzhe

1998, (2): 240-242.

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COMPUTING HIGH FREQUENCY RCS OF COMPLEX TARGETS IN REAL TIME
Abstract( 1518 )

Yu Yang;Zeng Zhiyong;Zhu Jinsong;Wang Baofa;Zhou Yinqing

1998, (2): 243-246.

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SYNTHESIS OF COMBINATORY CAM TO GENERATE A PERIODIC SPHERICAL MOTION OF SMALL TRAVEL SPACE
Abstract( 1320 )

Li Lixin;Shi Yonggang;Tan Jianrong

1998, (2): 247-249.

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STUDY ON SELF DIAGNOSIS AND SELF REPAIR FUNCTION OF SHAPE MEMORY ALLOY ENHANCED COMPOSITE STRUCTURE
Abstract( 1375 )

Tao Baoqi;Liang Dakai;Xiong Ke;Yuan Shenfang

1998, (2): 250-252.

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STUDY ON SMOOTH SURFACE IN ULTRAPRECISION GRINDING HARD BRITTLE MATERIALS
Abstract( 1981 )

Shi Xingkuan;Yuan Jingting;Xia Linong;Ren Jingxin;Peng Yanwu

1998, (2): 253-256.

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