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EXPERIMkNTAL RESEARCH OF THE CONFIGURATION OF WING-TIP DRAG REDUCING FOR LIOHT AIRCRAFT
Deng Yanmin;Hu Jizhong
1994, (8): 897-903.
PDF [ 512 K ]( 636 ) HTML
ITERATIVE COMPUTATION METHOD FOR NONLINEAR FORCED VIBRATION EQUATION ON HELICOPTER MAIN ROTORLOAD
Liu Xiangjian;Shen Xinkang;Xue Zhengzhong
1994, (8): 904-909.
PDF [ 307 K ]( 516 ) HTML
RELIABILITY ANALYSIS METHOD OF STRUCTURAL STIFFNESS
Lu Zhenzhou;Feng Yuansheng
1994, (8): 910-916.
PDF [ 403 K ]( 645 ) HTML
A STUDY OF COMPUTER-AIDED MISSILE PRELIMINARY DESIGN
Wang Jiayun;Chao Jianying
1994, (8): 917-920.
PDF [ 371 K ]( 508 ) HTML
CALCULATED INTERNAL PERFORMANCE OF THE SUPERSONIC THROUGH FLOW INLET
Shan Peng
1994, (8): 921-929.
PDF [ 585 K ]( 541 ) HTML
AN ANALYTIC METHOD FOR NONLINEAR THREE- DIMENSIONAL PROBLEMS OF LAMINATED CIRCULAR PLATES
Jiang Xiaoyu;Zhang Xiangzhou;Chen Baiping
1994, (8): 930-936.
PDF [ 468 K ]( 461 ) HTML
A DYNAMIC STRUCTURE DESIGN OF AN AERONAUTIC GEAR
Li Shuting;Shen Yunwen;Lin Tiancun
1994, (8): 937-941.
PDF [ 268 K ]( 859 ) HTML
STUDY ON FORMING THE CUTTING EDGES AND RAKE FACES OF BALL-END MILLS
ShenQian;Wang Min
1994, (8): 942-949.
PDF [ 498 K ]( 652 ) HTML
INFLUENCE OF CVD Si COATING ON THE SURFACE OF CARBON FIBERS ON THEIR PROPERTIES
Chu Shuangjie;Wang Haowei;He Guiyu
1994, (8): 950-954.
PDF [ 416 K ]( 876 ) HTML
THE TENSILE CREEP BEHAVIOR OF A POLYCRYSTALLINE GRAPHITE MATERIAL
Qiao Shengru;Lou Rong;Zhou Dayu;Yang Zheng
1994, (8): 955-959.
PDF [ 377 K ]( 691 ) HTML
EFFECT OF COLDWORKED HOLES ON THE INIATION LIFE AND PROPAGATION LIFE OF FATIGUE CRACKS IN TWO ULTRA-HIGH STRENGTH STEELS
Ding Chuanfu;Zhao Zhenye;Song Deyu
1994, (8): 960-967.
PDF [ 2753 K ]( 456 ) HTML
CHARACTERISTIC EQUATION NEAR THE SONIC LINE OF AXISYMMETRIC FLOW
Qian Yiji;H. Sobieczky
1994, (8): 968-970.
PDF [ 270 K ]( 483 ) HTML
ON A SEMIEMPIRICAL WALL PRESSURE SIONATURE CORRECTION METHOD FOR HIGH ANGLE OF ATTACK MODEL TESTS
Jiang Guiqing
1994, (8): 971-974.
PDF [ 347 K ]( 514 ) HTML
A PARALLEL ALGORITHM ON THE MIMD FOR THE CALCULATION OF BUCKLING LOADS OF THE PLATE
Lu Quanyi;Ye Tianqi
1994, (8): 975-979.
PDF [ 360 K ]( 373 ) HTML
NON-LINEAR STABILITY OF AN ARCH WITH SYMMETRICLLY VARIALE CURVATURE UNDER UNIFORM LATERAL LOAD
Zhang Zhizhou
1994, (8): 980-984.
PDF [ 267 K ]( 396 ) HTML
FIBRE-OPTIC pH TRANSDUCER
Lu Junfan;Zhou Xiuyin;Yao Yahong;Li Shaomeng
1994, (8): 985-987.
PDF [ 142 K ]( 684 ) HTML
THE APPLICATION OF VARIABLE STRUCTURE MODEL REFERENCE ADAPTIIVE CONTROL FOR BANK-TO-TURN MISSILES
ZhouJun;Chen Xinhai;Fen Wenjian;Zhen Huanmin
1994, (8): 988-992.
PDF [ 262 K ]( 775 ) HTML
THE DESIGN AND SIMULATION OF AN INTELLIGENT FLIGHT CONTROL SYSTEM BASED ON THE INERTIA DESCRIPTION
Jiang Changsheng;Li Wei;Xu Xiaohao
1994, (8): 993-997.
PDF [ 415 K ]( 394 ) HTML
THE INTELLIGENT CONTROL AND SYSTEM SIMULATION OF AN INTEGRATED FIRE/FLIGHT CONTROL SYSTEM
Jiang Changsheng;Xu Xiaohao;Yang Kerning;Lan Weihua
1994, (8): 998-1002.
PDF [ 268 K ]( 754 ) HTML
THE SIMULTANEOUS DATA ACQUISITION SYSTEM WITH MULTI-CHANNEL AND LARGE-CAPACITY
Dai Mingzhen;Tang Mingjie;Yang Zhenqi
1994, (8): 1003-1006.
PDF [ 297 K ]( 626 ) HTML
SUPERRESOLUTION RADAR IMAGING WITH EXTRAPOLATING DATA USING NEURAL NETWORK
Yezhenru;YinJun
1994, (8): 1007-1011.
PDF [ 415 K ]( 512 ) HTML
THE OVERALL ANALYSIS OF RADAR CROSS SECTION FOR A THREE-DIMENSIONAL RADOME AND AN ANTENNA
Deng Shuhui;Ruan Yingzheng
1994, (8): 1012-1016.
PDF [ 344 K ]( 633 ) HTML
THE DESIGNING OF THE SPECIMEN OF DOVETAIL JOINT IN UNIDIRECTIONALLY-LOADED FATIGUE TEST RIG
Huang Zhijian;Zhu Rupeng;Pan Shencai
1994, (8): 1017-1023.
PDF [ 501 K ]( 509 ) HTML
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