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25 June 1995, Volume 16 Issue 3

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25 June 1995, Volume 16 Issue 3

论文

A FOURIER SERIES EXPANSION METHOD FOR CALCULATING THE UNSTEADY AERODYNAMIC LOADS ON OSCILLATING WINGS
Abstract( 1505 )

Liu Qiangang;Liu Qun;Wu Kai

1995, (3): 2-7.

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NUMERICAL STUDY OF COMBUSTOR TURBULENT SWIRLING FLOW
Abstract( 1447 )

Fu Song

1995, (3): 8-13.

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VARIABLE STRUCTURE CONTROL OF AIRCRAFT FOR ATMOSPHERIC DISTURBANCE
Abstract( 1388 )

Zhu Xiaoping;Zhou Zhou

1995, (3): 14-21.

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OPERATION REQUIREMENTS OF TURRETED GUN IN HELICOPTER AIR COMBAT AND MATHEMATIC INVERSE SOLUTION
Abstract( 1898 )

Cao Yihua

1995, (3): 22-29.

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PILOT-VEHICLE SEMI-PHYSICAL SIMULATION STUDY OF DECOUPLING CONTROL FOR AIRCRAFT TF/TA PENETRATION
Abstract( 1166 )

Sun Baoting;Chen Yanyang

1995, (3): 30-35.

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ESTIMATION OF THE RANGE BETWEEN THE INTERCEPTER AND THE TARGET DURING INFRARED TERMINAL GUIDANCE OF SPACE INTERCEPTION
Abstract( 1652 )

Shi Xiaoping;Wang Zicai;Ke Qihong

1995, (3): 36-43.

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EXPERIMENT RESEARCH ON THE PROPERTIES OF PIEZOELECTRIC CERAMIC MICROACTUATORS
Abstract( 1444 )

Rui Xiaojian Zhang Youzhen

1995, (3): 44-48.

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THE MEASUREMENT OF THE EXFOLIATION RATE OF ALUMINIUM ALLOYS
Abstract( 1217 )

Li Di;Guo Baolan;Zhang Yumei

1995, (3): 49-53.

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THE CAVITY DURING SUPERPLASTIC DEFORMATION AND ITS INFLUENCE ON MECHANICAL PROPERTIES OF SUPERPLASTICALLY-DEFORMED MATERIALS AT ROOM TEMPERATURE
Abstract( 1632 )

Du Zhixiao;Wu Shidun;He Yongmei

1995, (3): 54-59.

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GRAIN STRUCTURES CONTROL OF NICKEL-BASE SUPERALLOYS IN CASTING PROCESS: EFFECT OF MELT ADDITIONS
Abstract( 1464 )

Liu Lin;Zhang Rong

1995, (3): 60-63.

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at% AMORPHOUS ALLOYS
Abstract( 1313 )

Meng Yan;Yang Gencang

1995, (3): 64-70.

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THE STUDY OF TRANSFORMATION KINETICS OF BAINITE IN GD STEEL
Abstract( 1512 )

Wen Cuie

1995, (3): 71-75.

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THE INFLUENCE OF THE CRYSTAL GROWTH ORIENTATION ON THE MICROSTRUCTURE IN HYPORAPID SOLIDIFICATION
Abstract( 1296 )

Jiang Chengbao;Hu Hanqi;Wang Peijun

1995, (3): 76-79.

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EFFECT OF SOLIDIFICATION RATE ON MICROSTRUCTURES OF DIRECTIONALLY SOLIDIFIED SUPERALLOY DZ22
Abstract( 1282 )

Liu Zhongyuan;Shi Zhengxing;She Li;Chen Rongzhang;Wang Luobao;Gu Linyu

1995, (3): 80-84.

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NUMERICAL ANALYSIS ON TURBULENT FLOW IN A DIFFUSER BY TIME MARCHING METHOD
Abstract( 1264 )

Weng Peifen;He Yousheng

1995, (3): 85-88.

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THE FLUCTUATING WALL-PRESSURE MEASUREMENT IN SWEPT SHOCK WAVE/BOUNDARY LAYER INTERACTIONS
Abstract( 1192 )

Zhang Hua;Deng Xueying

1995, (3): 89-92.

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A NUMERICAL ANALYSIS FOR THE GROUND RESONANCE OF A TWO-BLADE HELICOPTER ROTOR ON ANISOTROPIC FLEXIBLE SUPPORTS
Abstract( 1313 )

Lu Meng;Fei Binjun;Ren Zhiyong;Li Xiaolan

1995, (3): 93-99.

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DIRECT FREQUENCY-DOMAIN MODAL IDENTIFICATION BASED ON STRUCTURAL FREE VIBRATIONS
Abstract( 3310 )

Li Yuefeng

1995, (3): 100-104.

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AN INCREMENTAL METHOD FOR ELASTIC CONTACT PROBLEMS WITH FRICTION
Abstract( 1263 )

Yu Hailing;Zhu Depei

1995, (3): 105-109.

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A MATHEMATICAL DESCRIPTION OF FATIGUE TOUGHNESS
Abstract( 1327 )

Wang Yonglian

1995, (3): 110-114.

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STRESS CONCENTRATION OF FINITE ANISOTROPIC PLATE WITH ELLIPTICAL HOLE
Abstract( 1230 )

Xu Xiwu;Zhang Yining;Yang Xu

1995, (3): 115-120.

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THREE-MOMENT METHOD FOR RELIABILITY ANALYSIS
Abstract( 1512 )

Wu Liyan;Liu Geng;Wang Buying

1995, (3): 121-125.

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