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CONTROL OF SEPARATED FLOW OVER A STRAKE WING BY MOVING SURFACE
Lü Zhiyong;Ma Shuwei
1996, (5): 2-6.
PDF [ 153 K ]( 919 ) HTML
EXPERIMENTAL RESEARCH OF 2 D LOBED EXHAUST EJECTOR SYSTEMS
Hu Hui;Liu Huoxing;Wu Shousheng;Li Li
1996, (5): 7-12.
PDF [ 222 K ]( 735 ) HTML
EXPERIMENT INVESTIGATION ABOUT THE UNSTEADY AERODYNAMIC CHARACTERISTICS OF WINGS
Yu Xinzhi;Yang Yongnian;Wu Ze
1996, (5): 13-17.
PDF [ 199 K ]( 705 ) HTML
DESIGNING ELASTIC CONSTRAINTS IN A VIBRATION ISOLATION SYSTEM FROM THE VIEWPOINT OF NONLINEAR DYNAMICS
Hu Haiyan
1996, (5): 18-22.
PDF [ 264 K ]( 764 ) HTML
THE INTERPOLATION OF RATIONAL BICIRCULAR ARCS AND THE BICIRCULAR SPLINE SURFACES
Sun Jianquan
1996, (5): 23-27.
PDF [ 197 K ]( 773 ) HTML
COMPARATIVE TEST STUDY FOR THE MAXIMUM LIKELIHOOD PRINCIPLE AND THE TREATMENT OF ITS FATIGUE TEST DATA
Xiong Junjiang;Huang Xinyu;Gao Zhentong Xia Qianyou;Gan Weimin;Zeng Benyin;Sun Rulin
1996, (5): 28-31.
PDF [ 228 K ]( 726 ) HTML
APPROXIMATE LIMITS OF THE ENTROPY(METHOD) FOR RELIABILITY ASSESSMENT OF A SYSTEM
Shi Jun
1996, (5): 32-37.
PDF [ 203 K ]( 543 ) HTML
NONLINEAR ANALYSIS OF TWO ACTUATORS FOR ACTIVE CONTROL ON SURGE PHENOMENON
Nie Chaoqun Chen Jingyi
1996, (5): 38-43.
PDF [ 279 K ]( 536 ) HTML
CALCULATION OF AXIAL RELAXED/PRESSED FORCES OF ROTORS WITH CURVIC COUPLINGS
Yin Zeyong;Hu Baian;Wu Jianguo;Xu Youliang Zhen Qixuan
1996, (5): 44-49.
PDF [ 235 K ]( 920 ) HTML
GPS RAIM AVAILABILITY WITH A BAROMETRIC ALTIMETER AIDING
Chen Jiabin Yuan Xin
1996, (5): 50-54.
PDF [ 191 K ]( 630 ) HTML
HELICOPTER VIBRATION REDUCTION TECHNIQUE WITH HARMONIC ACTIVE CONTROL
Yang Yidong;Yuan Weidong
1996, (5): 55-60.
PDF [ 311 K ]( 727 ) HTML
STUDY OF CURRENT EQUALIZATION IN REDUNDANT ACTUATION SYSTEM WITH MAGNETIC FLUX SUM
Cheng Tao;Wang Zhanlin
1996, (5): 61-65.
PDF [ 208 K ]( 711 ) HTML
OXIDATION BEHAVIOUR OF 3D FINE WEAVE PIERCED CARBON CARBON COMPOSITES AT ULTRA HIGH TEMPERATURES
Han Jiecai;Zhang Jie;Du Shanyi
1996, (5): 66-70.
PDF [ 167 K ]( 680 ) HTML
NUMERICAL SIMULATION OF 3 D UNSTEADY TRANSONIC FLOWS OVER ROTARY WINGS
Liu Qiusheng;Shen Mengyu;Wang Baoguo Pu Cunbin
1996, (5): 71-74.
PDF [ 130 K ]( 580 ) HTML
NUMERICAL AND EXPERIMENTAL STUDIES OF JET FLOW EXHAUSTING FROM ROCKET
Le Guigao;Ma Dawei;Zhang Fuxiang
1996, (5): 75-78.
PDF [ 260 K ]( 562 ) HTML
COMPUTATION OF TRANSONIC VISCOUS FLOW AROUND A PITCHING AIRFOIL
Dai Jie;Liu Qiangang
1996, (5): 79-82.
PDF [ 182 K ]( 616 ) HTML
ADAPTIVE GRID SOLUTION OF N S EQUATION FOR COMPRESSIBLE VISCOUS FLOW AROUND AIRFOILS
Guo Dahai;Wen Gongbi
1996, (5): 83-86.
PDF [ 206 K ]( 633 ) HTML
PREDICTION OF ROTOR BLADE VORTEX INTERACTION NOISE FROM MEASURED UNSTEADY SURFACE PRESSURE OF BLADE
Yin Jianping;Hu Zhangwei
1996, (5): 87-89.
PDF [ 222 K ]( 611 ) HTML
TYPES OF FLOW OVER LEESIDE OF A CLIPPED DELTA WING AT SUPERSONIC SPEEDS
Hong Jinsen
1996, (5): 90-95.
PDF [ 288 K ]( 763 ) HTML
DYNAMIC CHARACTERISTICS ANALYSIS BASED ON THE SECTIONAL WARPING CORRECTIVE THEORY FOR COMPOSITE LAMINATED BEAMS
Huang Chuanyue;Zhu Dechao
1996, (5): 96-101.
PDF [ 371 K ]( 454 ) HTML
EQUITY ENVIRONMENTAL SPECTRUM AND SPEED TEST SPECTRUM FOR AIRCRAFT STRUCTURE
Zhou Xiyuan
1996, (5): 102-105.
PDF [ 370 K ]( 1274 ) HTML
VIBRATION ANALYSIS OF THE BEAM WITH AN ATTACHED CONSTRAINED DAMPING LAYER
Chen Guoping;Qian Zhendong
1996, (5): 106-109.
PDF [ 261 K ]( 640 ) HTML
VARIABLE STRUCTURAL CONTROL OF BRAKING MOMENT
Zhang Ling;Zhu Depei;Zhang Yu
1996, (5): 110-113.
PDF [ 182 K ]( 619 ) HTML
BP NEURAL NETWORKS BASED ON ON LINE MODELLING AND FAULT DETECTION IN NONLINEAR SYSTEMS
Dong Xuanming;Qiu Lihua;Wang Zhanlin
1996, (5): 114-118.
PDF [ 281 K ]( 542 ) HTML
METHOD OF INFORMATION DESCRIPITION FOR DETAILS AND AUTOMATIC PLOTTING OF OPERATION SKETCH BASED ON CLASSIFIED FEATURE
Deng Xiujin;Wang Yanwei
1996, (5): 119-123.
PDF [ 229 K ]( 540 ) HTML
STUDY ON ALLOCATION METHOD OF RELIABILITY FOR A LANDING GEAR SYSTEM
Xu Zhong
1996, (5): 124-126.
PDF [ 143 K ]( 476 ) HTML
STUDY OF THE NONUNIFORMITY OF MECHANICAL PROPERTIES IN WELDED JOINTS
Fan Yinhe;Ruan Miqing
1996, (5): 127-129.
PDF [ 173 K ]( 852 ) HTML
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