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25 October 1996, Volume 17 Issue 5

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25 October 1996, Volume 17 Issue 5

论文

CONTROL OF SEPARATED FLOW OVER A STRAKE WING BY MOVING SURFACE
Abstract( 1453 )

Lü Zhiyong;Ma Shuwei

1996, (5): 2-6.

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EXPERIMENTAL RESEARCH OF 2 D LOBED EXHAUST EJECTOR SYSTEMS
Abstract( 1422 )

Hu Hui;Liu Huoxing;Wu Shousheng;Li Li

1996, (5): 7-12.

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EXPERIMENT INVESTIGATION ABOUT THE UNSTEADY AERODYNAMIC CHARACTERISTICS OF WINGS
Abstract( 1535 )

Yu Xinzhi;Yang Yongnian;Wu Ze

1996, (5): 13-17.

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DESIGNING ELASTIC CONSTRAINTS IN A VIBRATION ISOLATION SYSTEM FROM THE VIEWPOINT OF NONLINEAR DYNAMICS
Abstract( 1348 )

Hu Haiyan

1996, (5): 18-22.

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THE INTERPOLATION OF RATIONAL BICIRCULAR ARCS AND THE BICIRCULAR SPLINE SURFACES
Abstract( 2211 )

Sun Jianquan

1996, (5): 23-27.

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COMPARATIVE TEST STUDY FOR THE MAXIMUM LIKELIHOOD PRINCIPLE AND THE TREATMENT OF ITS FATIGUE TEST DATA
Abstract( 6660 )

Xiong Junjiang;Huang Xinyu;Gao Zhentong Xia Qianyou;Gan Weimin;Zeng Benyin;Sun Rulin

1996, (5): 28-31.

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APPROXIMATE LIMITS OF THE ENTROPY(METHOD) FOR RELIABILITY ASSESSMENT OF A SYSTEM
Abstract( 1893 )

Shi Jun

1996, (5): 32-37.

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NONLINEAR ANALYSIS OF TWO ACTUATORS FOR ACTIVE CONTROL ON SURGE PHENOMENON
Abstract( 1230 )

Nie Chaoqun Chen Jingyi

1996, (5): 38-43.

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CALCULATION OF AXIAL RELAXED/PRESSED FORCES OF ROTORS WITH CURVIC COUPLINGS
Abstract( 1509 )

Yin Zeyong;Hu Baian;Wu Jianguo;Xu Youliang Zhen Qixuan

1996, (5): 44-49.

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GPS RAIM AVAILABILITY WITH A BAROMETRIC ALTIMETER AIDING
Abstract( 1367 )

Chen Jiabin Yuan Xin

1996, (5): 50-54.

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HELICOPTER VIBRATION REDUCTION TECHNIQUE WITH HARMONIC ACTIVE CONTROL
Abstract( 1366 )

Yang Yidong;Yuan Weidong

1996, (5): 55-60.

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STUDY OF CURRENT EQUALIZATION IN REDUNDANT ACTUATION SYSTEM WITH MAGNETIC FLUX SUM
Abstract( 1310 )

Cheng Tao;Wang Zhanlin

1996, (5): 61-65.

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OXIDATION BEHAVIOUR OF 3D FINE WEAVE PIERCED CARBON CARBON COMPOSITES AT ULTRA HIGH TEMPERATURES
Abstract( 1441 )

Han Jiecai;Zhang Jie;Du Shanyi

1996, (5): 66-70.

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NUMERICAL SIMULATION OF 3 D UNSTEADY TRANSONIC FLOWS OVER ROTARY WINGS
Abstract( 1586 )

Liu Qiusheng;Shen Mengyu;Wang Baoguo Pu Cunbin

1996, (5): 71-74.

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NUMERICAL AND EXPERIMENTAL STUDIES OF JET FLOW EXHAUSTING FROM ROCKET
Abstract( 1499 )

Le Guigao;Ma Dawei;Zhang Fuxiang

1996, (5): 75-78.

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COMPUTATION OF TRANSONIC VISCOUS FLOW AROUND A PITCHING AIRFOIL
Abstract( 1290 )

Dai Jie;Liu Qiangang

1996, (5): 79-82.

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ADAPTIVE GRID SOLUTION OF N S EQUATION FOR COMPRESSIBLE VISCOUS FLOW AROUND AIRFOILS
Abstract( 1456 )

Guo Dahai;Wen Gongbi

1996, (5): 83-86.

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PREDICTION OF ROTOR BLADE VORTEX INTERACTION NOISE FROM MEASURED UNSTEADY SURFACE PRESSURE OF BLADE
Abstract( 1853 )

Yin Jianping;Hu Zhangwei

1996, (5): 87-89.

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TYPES OF FLOW OVER LEESIDE OF A CLIPPED DELTA WING AT SUPERSONIC SPEEDS
Abstract( 7246 )

Hong Jinsen

1996, (5): 90-95.

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DYNAMIC CHARACTERISTICS ANALYSIS BASED ON THE SECTIONAL WARPING CORRECTIVE THEORY FOR COMPOSITE LAMINATED BEAMS
Abstract( 1142 )

Huang Chuanyue;Zhu Dechao

1996, (5): 96-101.

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EQUITY ENVIRONMENTAL SPECTRUM AND SPEED TEST SPECTRUM FOR AIRCRAFT STRUCTURE
Abstract( 1148 )

Zhou Xiyuan

1996, (5): 102-105.

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VIBRATION ANALYSIS OF THE BEAM WITH AN ATTACHED CONSTRAINED DAMPING LAYER
Abstract( 1302 )

Chen Guoping;Qian Zhendong

1996, (5): 106-109.

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VARIABLE STRUCTURAL CONTROL OF BRAKING MOMENT
Abstract( 1613 )

Zhang Ling;Zhu Depei;Zhang Yu

1996, (5): 110-113.

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BP NEURAL NETWORKS BASED ON ON LINE MODELLING AND FAULT DETECTION IN NONLINEAR SYSTEMS
Abstract( 1096 )

Dong Xuanming;Qiu Lihua;Wang Zhanlin

1996, (5): 114-118.

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METHOD OF INFORMATION DESCRIPITION FOR DETAILS AND AUTOMATIC PLOTTING OF OPERATION SKETCH BASED ON CLASSIFIED FEATURE
Abstract( 1397 )

Deng Xiujin;Wang Yanwei

1996, (5): 119-123.

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STUDY ON ALLOCATION METHOD OF RELIABILITY FOR A LANDING GEAR SYSTEM
Abstract( 1285 )

Xu Zhong

1996, (5): 124-126.

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STUDY OF THE NONUNIFORMITY OF MECHANICAL PROPERTIES IN WELDED JOINTS
Abstract( 1643 )

Fan Yinhe;Ruan Miqing

1996, (5): 127-129.

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