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25 February 1999, Volume 20 Issue 1

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25 February 1999, Volume 20 Issue 1

FORCE SENSING & CONTROL FOR INTELLIGENT MACHINE:AN OVERVIEW
Abstract( 2226 )

Yin Yuehong;Zhu Jianying

1999, (1): 1-7.

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DYNAMIC RESPONSE OF FLEXIBLE APPENDAGES TO THE HARMONIC EXCITATION DURING EXTENSION
Abstract( 1523 )

Song Yu;Wang Benli;Ma Xingrui

1999, (1): 8-10.

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UPDATING DESIGN PARAMETERS OF FINITE ELEMENT MODEL BY USING TEST COMPLEX MODAL DATA
Abstract( 1416 )

Feng Wenxian;Chen Xin

1999, (1): 11-16.

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RESEARCH ON PASSIVE VIBRATION CONTROL OF TRUSS STRUCTURES BY DISPLACEMENT DEPENDENT DRY FRICTIONAL JOINTS
Abstract( 1603 )

Yan Tianhong;Zheng Gangtie;Huang Wenhu

1999, (1): 17-21.

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STUDY OF RELIABILITY DEGREE OF GPS POSITIONING SOLUTION
Abstract( 1695 )

Chang Qing;Liu Zhongkan;Zhang Qishan

1999, (1): 22-26.

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D TYPE ON LINE LEARNING CONTROL FOR A CLASS OF NONLINEAR SYSTEMS
Abstract( 1436 )

Yan Xinggang;Lin Hui;Dai Guanzhong

1999, (1): 27-29.

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MICROSTRUCTURE AND PHASE TRANSFORMATION OF THE Ni 30Al 1Hf ALLOY
Abstract( 1501 )

Xing Zhanping;Han Yafang;Yan Minggao

1999, (1): 30-33.

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STATISTICAL STUDY OF CORROSION KINETICS LAW FOR LY12CZ AND 7075T7351 ALUMINUM ALLOY IN EXCO SOLUTION
Abstract( 1675 )

Xie Weijie;Li di;Hu Yanling;Guo Baolan

1999, (1): 34-38.

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MODELING THE AERODYNAMIC FORCES OF A MANEUVERING HELICOPTER ROTOR
Abstract( 1350 )

Cao Yihua

1999, (1): 39-42.

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TECHNOLOGY RESEARCHES ABOUT MODIFYING AERONAUTICAL WIND TUNNEL FOR AERODYNAMIC TESTS OF AUTOMOBILE MODELS
Abstract( 1312 )

Cai Guohua;Fu Limin

1999, (1): 43-46.

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OPTIMIZATION OF THE BLADES FOR TURBOMACHINE BY GENETIC ALGORITHM
Abstract( 1351 )

Fan Huiyuan;Wang Shangjin;Xi Guang

1999, (1): 47-51.

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USING FREQUENCY DOMAIN LIKELIHOOD METHOD TO IDENTIFY PARAMETERS OF AIRCRAFT EQUIVALENT SYSTEM
Abstract( 1336 )

Cheng Shaojun;Deng Jianhua

1999, (1): 52-54.

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SEPARATED FLOWS OVER MAIN ELEMENT AND FLAP OF MULTIELEMENT AIRFOIL AT HIGH ANGLES OF ATTACK
Abstract( 1642 )

Li Xiaowei;Qiao Zhide

1999, (1): 55-57.

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NON LINEAR MODEL OF CYCLIC 2 DOF SUBSTRUCTURE OF SHROUDED BLISK
Abstract( 1351 )

Li lin

1999, (1): 58-61.

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EFFECTS OF LASER SHOCK PROCESSING ON THE FATIGUE CRACK GROWTH RATES OF ALUMINIUM ALLOY
Abstract( 1332 )

Zhang Hong;Yu Chengye

1999, (1): 62-64.

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COMMENTS ON RELIABILITY GROWTH MODEL IN GJB/Z77 FOR MULTI SYSTEMS DEVELOPMENT
Abstract( 1640 )

Mei Wenhua;Yang Yixian

1999, (1): 65-68.

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ASSESSMENTS OF AIR TO SURFACE TARGET ATTACKING EFFECTIVENESS FOR A COMBAT AIRCRAFT
Abstract( 1516 )

Huang Jun;Wu Zhe

1999, (1): 69-71.

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STUDY ON MECHANISM OF RESISTANCE CHANGE OF FATIGUE LIFE GAGE
Abstract( 1730 )

Hu Mingmin;Zhou Keyin

1999, (1): 72-74.

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CALCULATION MODEL AND DETERMINATION METHOD OF CORROSION DAMAGE CALENDAR LIFE OF METAL PARTS
Abstract( 1416 )

Zhang Fuze

1999, (1): 75-79.

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