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AN OPTIMAL TRAJECTORY ESTIMATE OF ATTACKING MOVING TARGET
Zeng Yingchao
1990, (9): 417-423.
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A CLOSED FORM SOLUTION OF STRESS INTENSITY FACTORS FOR THE SHAFT OF AEROPLANE ALL-MOVING STABILIZER WITH CORNER CRACKS EMANATING FROM A HOLE
Wang Qizhi;Zhang Xing;He Qingzhi;Ren Bingyi
1990, (9): 424-432.
AN INVESTIGATION ON VIBRATION METHODS FOR THE DETERMINATION OF DYNAMIC MODULI OF COMPOSITE MATERIALS
Li Dazhi;Ding Xihong;Gu Huizhi
1990, (9): 433-439.
NUMERICAL ANALYSES OF STRESS NEAR THE HOLE OF COMPRESSOR DISK BY BOUNDARY ELEMENT METHOD
Wen Weidong;Gao Deping
1990, (9): 440-448.
TRANSONIC FLOW CALCULATION OF EULER EQUATIONS BY IMPLICIT ITERATING SCHEME WITH FLUX SPLITTING
Liu Daozhi;Zha Gecheng
1990, (9): 449-455.
A ADAPTIVE FILTER FOR TRACKING THE MANEUVERING TARGET Institute of Systems Science. Academia Sinica
Jia Peizhang
1990, (9): 456-464.
THE COMPATIBILITY CHECK OF THE FLIGHT TEST DATA OF THE DO 28 RESEARCH AIRCRAFT
Wang Wei;Xiao Shunda;Chen Xinhai;R. Brockhaus
1990, (9): 465-473.
AN IDENTIFICATION METHOD OF FAST TIME VARYING PARAMETERS ADAPTED TO AIRCRAFT CONTROL SYSTEMS
Chen Xinhai;Yan Xiaoming;Li Yanjun
1990, (9): 474-479.
THE PREDICTION OF ELECTROMAGNETIC CHARACTERISTICS OF STRUCTURE ABSORBENT MATERIALS
Jia Baofu;Liu Shuzhang;Lin Weigan
1990, (9): 480-486.
MICROSTRUCTURE AND MECHANICAL PROPERTIES OF HIP AND AGED ZrO_2-Y_2O_3 CERAMICS
Zhou Yu;Lei Tingquan;Sakuma
1990, (9): 487-495.
ANALYTICAL-VARIATIONAL METHOD OF SOLUTION FOR FINITE PLATES WITH SINGLE HOLE-EDGE CRACK
Lai Junbiao Zhang Xing;He Qingzhi
1990, (9): 496-504.
THE INFLUENCES OF FORCED OSCILLATIONS TOWARD VORTEX-BREAKDOWN
Chen Yanqiu Lu Zhiyong;Lee Chun-Hian
1990, (9): 505-509.
AF 2 ITERATION AND ITS PARALLEL ALGORITHM FOR TRANSONIC FLOW WITH LARGE DISTURBANCES IN FREESTREAM-DIRECTION AROUND AXISYMMETRIC BODIES AT ZERO ANGLE OF ATTACK
Min Saijin;Li Xiuying;Luo Shijun
1990, (9): 510-514.
CALCULATION OF UNSTEADY AERODYNAMIC LOADS ON WINGS WITH AN OSCILLATORY LEADING EDGE FLAP
Yuan Li;Lu Zhiyong;Wu Jianmin
1990, (9): 515-520.
GEOMETRICALLY NONLINEAR SPLINE ELEMENT
Fan Zhong;Long Yuqiu
1990, (9): 521-525.
A TIME-DOMAIN AVERAGE METHOD TREATING THE CASE OF LOWER SIGNAL TO NOISE RATIO FOR MODAL PARAMETER IDENTIFICATION
Zheng Gangtie;Huang Wenhu;Shao Chengxun;Zou Jingxiang
1990, (9): 526-531.
The Behavior of Creep Crack Growth in Ni-Base Superalloy GH33A
Jiang Bo;Zhang Xingan;He Jinrui
1990, (9): 532-536.
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