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AN EFFICIENT FINITE-DIFFERENCE ALGORITHM FOR COMPUTING AXISYMMETRIC TRANSONIC NACELLE FLOW FIELDS
Huang Mingke
1990, (1): 1-6.
PDF [ 364 K ]( 3879 ) HTML
SOME ASPECTS OF TWO AIRCRAFTS COMBAT IN PLANE-A METHOD OF DEALING WITH TWO-TARGET PROBLEM
Tong Mingan;Zhang Jianhua
1990, (1): 7-15.
PDF [ 611 K ]( 313 ) HTML
STRESS SINGULARITY ANALYSIS FOR A GRACK INITIATING AT A FLAT INCLUSION TIP
Liu Tierang;Liu Xuehui
1990, (1): 16-23.
PDF [ 554 K ]( 473 ) HTML
PROBLEMS ON DYNAMIC RESPONSE IN A QUARTER SPACE UNDER SHEAR LOAD WITH CONSTANT EXTENSION
Zou Zhenzhu;Zhou Zhengong;Ma Xingrui
1990, (1): 24-30.
PDF [ 509 K ]( 385 ) HTML
A NUMERICAL METHOD IN AEROELASTICITY FOR WINGS WITH SEPARATION AT LARGE ANGLE OF ATTACK
Ye Zhengyin;Zhao Lingcheng;Yang Yongnian
1990, (1): 31-36.
PDF [ 504 K ]( 663 ) HTML
MAIN CHARACTERISTIC PARAMETER MODEL FOR JET ENGINE FAULT DIAGNOSIS
Fan Zuomin;Sun Chunlin;Lin Zhaofu
1990, (1): 37-45.
PDF [ 680 K ]( 561 ) HTML
MODIFIED FAULT TOLERANT INERTIAL NAVIGATION SYSTEM
Zhang Hanguo;Zhang Hongyue
1990, (1): 46-52.
PDF [ 435 K ]( 587 ) HTML
ERROR ESTIMATION AND DOUBLE MESH FOR RIGID-VISCOUS-PLASTIC FINITE ELEMENT ANALYSIS OF UNSTEADY EXTRUSION PROCESSES
Guo Yangmine
1990, (1): 53-58.
PDF [ 447 K ]( 378 ) HTML
RECALESCENCE BEHAVIOUR AND SOLIDIFICATION STRUCTURE OF HIGHLY UNDERCOOLED Ni-32.5%Sn EUTECTIC ALLOY
Wei Bingbo;Yang Gencang;Zhou Yaohe
1990, (1): 59-64.
PDF [ 1104 K ]( 541 ) HTML
THE ESTIMATION AND EXPERIMENT OF HYBRID EFFECT OF HYBRID FIBRE-REINFORCED COMPOSITES
Song Huancheng;Deng Hao;Liang Zhiyong
1990, (1): 65-69.
PDF [ 366 K ]( 590 ) HTML
THE EFFECT OF PLATE MANIPULATOR WAKES ON SKIN FRICTION
Shi Shengxi;Dai Changhui;Zhou Mingde
1990, (1): 70-73.
PDF [ 359 K ]( 491 ) HTML
FINITE ELEMENT NUMERICAL ANAIYSIS FOR TRANSONIC FLOWS AROUND LIFTING FUSELAGES
Zhang Guofu;Li Xianpin
1990, (1): 74-77.
PDF [ 329 K ]( 333 ) HTML
AEROELASTIC TAILORING OF COMPOSITE WING STRUCTURES
Huang Chuanqi;Qiao Xin
1990, (1): 78-82.
PDF [ 385 K ]( 352 ) HTML
A COMBINED RICCATI TRANSFER MATRIX-DIRECT INTEGRATION METHOD WITH ITS APPLICATIONS
Wen Weidong;Gu Jialiu
1990, (1): 83-87.
PDF [ 164 K ]( 520 ) HTML
THE STUDY OF TRANSIENT SUPPRESSION TECHNIQUES FOR MULTIMODE FLIGHT CONTROL SYSTEM
Yang Yidong;Niu Peiyi;Jiang Hao
1990, (1): 88-92.
PDF [ 395 K ]( 509 ) HTML
THE METHOD OF RANDOM VARIABLE STRUCTURE OPTIMAL CONTROL FOR AIRCRAFT
Hu Shousong;He Yaqun
1990, (1): 93-97.
PDF [ 392 K ]( 345 ) HTML
UNCERTAINTIES OF OPERATING TIME IN SYSTEM REIIABILITY
Cai kaiyuan;Wen Chuanyuan
1990, (1): 98-105.
PDF [ 447 K ]( 509 ) HTML
ON THE MECHANISM OF FRACTURE OF LC4 ALUMINIUM ALLOY PLATE UNDER COMPLICATED STRESS STATES
Li Huanxi;Chen Changqi
1990, (1): 106-110.
PDF [ 1114 K ]( 446 ) HTML
FURTHER COMMENT ON “BOUNDARY INTEGRAL METHOD FOR TRANSONIC FLOWS”
Pan Jieyuan;Wu Liyi
1990, (1): 111-112.
PDF [ 161 K ]( 473 ) HTML
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