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A FOURIER SERIES EXPANSION METHOD FOR CALCULATING THE UNSTEADY AERODYNAMIC LOADS ON OSCILLATING WINGS
Liu Qiangang;Liu Qun;Wu Kai
1995, (3): 2-7.
PDF [ 313 K ]( 748 ) HTML
NUMERICAL STUDY OF COMBUSTOR TURBULENT SWIRLING FLOW
Fu Song
1995, (3): 8-13.
PDF [ 240 K ]( 807 ) HTML
VARIABLE STRUCTURE CONTROL OF AIRCRAFT FOR ATMOSPHERIC DISTURBANCE
Zhu Xiaoping;Zhou Zhou
1995, (3): 14-21.
PDF [ 342 K ]( 551 ) HTML
OPERATION REQUIREMENTS OF TURRETED GUN IN HELICOPTER AIR COMBAT AND MATHEMATIC INVERSE SOLUTION
Cao Yihua
1995, (3): 22-29.
PDF [ 363 K ]( 565 ) HTML
PILOT-VEHICLE SEMI-PHYSICAL SIMULATION STUDY OF DECOUPLING CONTROL FOR AIRCRAFT TF/TA PENETRATION
Sun Baoting;Chen Yanyang
1995, (3): 30-35.
PDF [ 177 K ]( 571 ) HTML
ESTIMATION OF THE RANGE BETWEEN THE INTERCEPTER AND THE TARGET DURING INFRARED TERMINAL GUIDANCE OF SPACE INTERCEPTION
Shi Xiaoping;Wang Zicai;Ke Qihong
1995, (3): 36-43.
PDF [ 329 K ]( 442 ) HTML
EXPERIMENT RESEARCH ON THE PROPERTIES OF PIEZOELECTRIC CERAMIC MICROACTUATORS
Rui Xiaojian Zhang Youzhen
1995, (3): 44-48.
PDF [ 206 K ]( 1819 ) HTML
THE MEASUREMENT OF THE EXFOLIATION RATE OF ALUMINIUM ALLOYS
Li Di;Guo Baolan;Zhang Yumei
1995, (3): 49-53.
PDF [ 204 K ]( 820 ) HTML
THE CAVITY DURING SUPERPLASTIC DEFORMATION AND ITS INFLUENCE ON MECHANICAL PROPERTIES OF SUPERPLASTICALLY-DEFORMED MATERIALS AT ROOM TEMPERATURE
Du Zhixiao;Wu Shidun;He Yongmei
1995, (3): 54-59.
PDF [ 325 K ]( 646 ) HTML
GRAIN STRUCTURES CONTROL OF NICKEL-BASE SUPERALLOYS IN CASTING PROCESS: EFFECT OF MELT ADDITIONS
Liu Lin;Zhang Rong
1995, (3): 60-63.
PDF [ 224 K ]( 512 ) HTML
at% AMORPHOUS ALLOYS
Meng Yan;Yang Gencang
1995, (3): 64-70.
PDF [ 357 K ]( 629 ) HTML
THE STUDY OF TRANSFORMATION KINETICS OF BAINITE IN GD STEEL
Wen Cuie
1995, (3): 71-75.
PDF [ 278 K ]( 806 ) HTML
THE INFLUENCE OF THE CRYSTAL GROWTH ORIENTATION ON THE MICROSTRUCTURE IN HYPORAPID SOLIDIFICATION
Jiang Chengbao;Hu Hanqi;Wang Peijun
1995, (3): 76-79.
PDF [ 189 K ]( 1510 ) HTML
EFFECT OF SOLIDIFICATION RATE ON MICROSTRUCTURES OF DIRECTIONALLY SOLIDIFIED SUPERALLOY DZ22
Liu Zhongyuan;Shi Zhengxing;She Li;Chen Rongzhang;Wang Luobao;Gu Linyu
1995, (3): 80-84.
PDF [ 365 K ]( 689 ) HTML
NUMERICAL ANALYSIS ON TURBULENT FLOW IN A DIFFUSER BY TIME MARCHING METHOD
Weng Peifen;He Yousheng
1995, (3): 85-88.
PDF [ 278 K ]( 554 ) HTML
THE FLUCTUATING WALL-PRESSURE MEASUREMENT IN SWEPT SHOCK WAVE/BOUNDARY LAYER INTERACTIONS
Zhang Hua;Deng Xueying
1995, (3): 89-92.
PDF [ 266 K ]( 493 ) HTML
A NUMERICAL ANALYSIS FOR THE GROUND RESONANCE OF A TWO-BLADE HELICOPTER ROTOR ON ANISOTROPIC FLEXIBLE SUPPORTS
Lu Meng;Fei Binjun;Ren Zhiyong;Li Xiaolan
1995, (3): 93-99.
PDF [ 197 K ]( 985 ) HTML
DIRECT FREQUENCY-DOMAIN MODAL IDENTIFICATION BASED ON STRUCTURAL FREE VIBRATIONS
Li Yuefeng
1995, (3): 100-104.
PDF [ 282 K ]( 809 ) HTML
AN INCREMENTAL METHOD FOR ELASTIC CONTACT PROBLEMS WITH FRICTION
Yu Hailing;Zhu Depei
1995, (3): 105-109.
PDF [ 206 K ]( 720 ) HTML
A MATHEMATICAL DESCRIPTION OF FATIGUE TOUGHNESS
Wang Yonglian
1995, (3): 110-114.
PDF [ 202 K ]( 1478 ) HTML
STRESS CONCENTRATION OF FINITE ANISOTROPIC PLATE WITH ELLIPTICAL HOLE
Xu Xiwu;Zhang Yining;Yang Xu
1995, (3): 115-120.
PDF [ 262 K ]( 632 ) HTML
THREE-MOMENT METHOD FOR RELIABILITY ANALYSIS
Wu Liyan;Liu Geng;Wang Buying
1995, (3): 121-125.
PDF [ 285 K ]( 1936 ) HTML
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