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IHE ANALYSIS OF PROPELLELLER LIFTING LINE THEORY BY THE METHOD OF MATCHED ASYMPTOTIC EXPANSIONS
Chenzemin;Pan Jieyuan;Wu Liyi
1994, (5): 513-518.
PDF [ 316 K ]( 790 ) HTML
NUMERICAL SIMULATION OF HYPERSONIC FLOW OVER AXISYMMETRIC SPIKED BODY
Zhang Hanxin;Huang Jie;Gao Shuchun
1994, (5): 519-525.
PDF [ 404 K ]( 664 ) HTML
AN IMPROVEMENT FOR LOWER-ORDER PANEL METHOD BASED ON THE DIRICHLET BOUNDARY CONDITION
Xu Mingchu;Gu Wenying
1994, (5): 526-531.
PDF [ 356 K ]( 809 ) HTML
DEVELOPMENT TOOL OF EXPERT SYSTEM FOR STRUCTURAL OPTIMIZATION
Xia Renwei;Zhang Cailai
1994, (5): 532-538.
PDF [ 397 K ]( 425 ) HTML
SOME CHARACTERISTICS OF BOILING IN NARROW SPACE
Xia Chunlin
1994, (5): 539-544.
PDF [ 453 K ]( 539 ) HTML
VARIABLE STRUCTURE CONTROL FOR SYSTEMS WITH CONSIDERATION OF THE DYNAMICS OF SENSORS
Gao Weibing
1994, (5): 545-551.
PDF [ 419 K ]( 491 ) HTML
LIMIT CYCLE ANALYSIS OF GROUND RESONANCE OF HELICOPTER WITH NONLINEAR DAMPING
Cheng Zhiqing;Zhou Chuanrong;Cheng Jinsong
1994, (5): 552-557.
PDF [ 356 K ]( 472 ) HTML
COMBINATORIAL QUICK JPDA ALGORITHM
Pan Quan;Zhang Hongcai;Xiang Yangzhao;Wang Peide
1994, (5): 558-563.
PDF [ 343 K ]( 446 ) HTML
A SELF-TUNING GUIDED CONTROL METHOD OF ANTI-TANK MISSILE
Liu Min;Kang Jingli
1994, (5): 564-569.
PDF [ 398 K ]( 691 ) HTML
METHODS OF IMAGE PROCESSING BASED ON LOGICAL NEURAL NETWORKS
Yang Guoqing;Ge Hongwei
1994, (5): 570-575.
PDF [ 447 K ]( 376 ) HTML
VIBRATION ANALYSIS IN TRANSMISSION OF SPIRAL BEVEL GEARS
Fang Zongde;Gao Ping;Song Leming
1994, (5): 576-581.
PDF [ 363 K ]( 641 ) HTML
CAD OF THE COMPLICATED OPTICAL SYSTEMS IN AERONAUTICAL ENGINEERING
Wang Yongzhong
1994, (5): 582-587.
PDF [ 390 K ]( 490 ) HTML
INELASTIC BEHAVIOUR OF T300/5222(C/E)LAMINATES WITH CROSS-PLY──NON-LINEAR CREEP
Lu Meng;Kou Changhe
1994, (5): 588-595.
PDF [ 482 K ]( 433 ) HTML
ANALYSIS AND MEASUREMENT ON RESIDUAL STRESS OF ARAMID ALUMINUM LAMINATES
Li Hongyun;Hu Hongjun;Zheng Ruiqi
1994, (5): 596-600.
PDF [ 406 K ]( 445 ) HTML
A NUMERICAL SIMULATION OF NORMAL SHOCK WAVE DIFFRACTION OVER AN OBSTACLE
Cai Hanlong;Li Suxun
1994, (5): 601-603.
PDF [ 116 K ]( 764 ) HTML
THE NUMERICAL SIMULATION OF LIFT-INCREASE EFFECT ON AN AIRFOIL WITH AJET FROM ITS SUREACE
Li Feng;Deng Ningfeng;Zhou Weijiang;Ma Handong
1994, (5): 604-606.
PDF [ 205 K ]( 527 ) HTML
DETERMINING FATIGUE LIFE RELIABILATY MODEL WITH FUZZY JUDGMENT AND BAYES THEORY
Liu Jianzhong;Xie Liyang;Xu Hao
1994, (5): 607-610.
PDF [ 221 K ]( 845 ) HTML
A METHOD FOR THE STRENGTH RELIABILITY CALCULATION OF AXIAL LMACHING PARTS OF AIRLINE ENGINE REDUCER
Yin Mingde;Ouyang Zhuxing
1994, (5): 611-615.
PDF [ 371 K ]( 547 ) HTML
BOUNDARY ELEMENT METHOD FOR 3-D ELASTO-PLASTIC CONTACT PROBLEMS
Wen Weidong;GaO Deping
1994, (5): 616-619.
PDF [ 308 K ]( 486 ) HTML
A NEW NONLINEAR FILTER AND ITS APPLICATION TO FLIGHT STATE AND PAPAMETER ESTIMATION OF AIRCRAFT
Zhang Youmin;Zhang Hongcai;Dai Guanzhong;He Zhibin
1994, (5): 620-626.
PDF [ 441 K ]( 712 ) HTML
MICROPROGRAMMING-CONTROLLED DIRECT MEMORY ACCESS AND ITS APPLICATION IN THE FIELD OF TEST,MEASUREMENT AND CONTROL
Tang Lizheng;Shen Gongxun
1994, (5): 627-631.
PDF [ 314 K ]( 386 ) HTML
ANALYSIS OF MICROCREEP AND ITS AFFECTING FACTORS OF SICP/AI COMPOSITES
Li YiChun;An Xiyun
1994, (5): 632-635.
PDF [ 2243 K ]( 463 ) HTML
AN ANALYSIS OF CUTTER-LOCATION CALCULATING METHOD FOR TWIST TURBINE BLADE SURFACES
Wei Yuanqian
1994, (5): 636-640.
PDF [ 377 K ]( 428 ) HTML
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