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STATE-OF-ART AND FUTURE OF AIRCRAFT STRUCTURE DESIGN AND STRENGTH ANALYSIS
Huang Yushan;Zhu Depei
1984, (2): 103-111.
PDF [ 642 K ]( 1969 ) HTML
NEW DEVELOPMENTS OF AEROELASTIC RESEARCH
Guan De
1984, (2): 112-117.
PDF [ 394 K ]( 341 ) HTML
SCENE MATCHING AND ITS APPLICATION TO AEROSPACE ELECTRONIC SYSTEMS
Sun Zhongkang
1984, (2): 118-131.
PDF [ 831 K ]( 363 ) HTML
STRENGTHENING THE STUDY ON THE USABILITY OF AIRCRAFT MATERIAIS
Wu Yunshu
1984, (2): 132-139.
PDF [ 602 K ]( 237 ) HTML
A KERNEL FUNCTION METHOD FOR COMPUTING UNSTEADY LOAD ON THREE-DIMENSIONAL WINGS IN TRANSONIC FLOW
Wu Yizhao
1984, (2): 140-148.
PDF [ 494 K ]( 310 ) HTML
ROOT LOCUS METHOD AND AUTOMATIC IDENTIFICATION OF MODES IN FLUTTER ANALYSIS
Yang Xingjian;Li Guangque
1984, (2): 149-156.
PDF [ 406 K ]( 283 ) HTML
DETERMINATION OF THE AXIS AND THE ANGLE OF ROTATION FOR A RETRACTABLE LANDING GEAR
Zhang Qixian
1984, (2): 157-162.
PDF [ 322 K ]( 323 ) HTML
6 FUNCTION AND GENERALIZED TABLES OF THERMODYNAMIC PROPERTIES FOR C_nH_m-AIR SYSTEM COMBUSTION PRODUCTS
Fan Zuomin;Fu Xunquan
1984, (2): 163-167.
PDF [ 290 K ]( 622 ) HTML
NONLINEARITY EFFECT ON THE LOCAL DECENTRALIZED CONTROL OF LARGE-SCALE SYSTEMS
Gao Weibin
1984, (2): 168-177.
PDF [ 474 K ]( 268 ) HTML
MULTI-RATE DIGITAL FLIGHT CONTROL SYSTEMS
Guo Suofeng
1984, (2): 178-185.
PDF [ 427 K ]( 248 ) HTML
A RECONFIGURABLE REDUNDANCY MANAGEMENT STRATEGY FOR A TRIPLEX DFBW SYSTEM
Li Lichun
1984, (2): 186-192.
PDF [ 454 K ]( 348 ) HTML
STATE TRANSITION CHAIN METHOD-RELIABILITY ANALYSES OF IRREPARABLE MARKOVIAN SYSTEMS
Zhang Fuyuang;Li Peiqiong;Han Yugeng
1984, (2): 193-199.
PDF [ 385 K ]( 288 ) HTML
AN EQUIVALENT STRENGTH METHOD FOR OPTIMUM DESIGN OF COMPOSITE LAMINATES
Liu Fanglong
1984, (2): 200-209.
PDF [ 577 K ]( 337 ) HTML
MODAL TEST AND PARAMETER IDENTIFICATION OF A FLUTTER WING MODEL WITH EXTERNAL MISSILES
Zhang Lingmi
1984, (2): 211-218.
PDF [ 446 K ]( 273 ) HTML
AN EXPERIMENTAL STUDY ON EFFECT OF OVERLOAD ON FATIGUE LIFE
Zeng Chunhua;Guo Kangmin
1984, (2): 219-224.
PDF [ 369 K ]( 337 ) HTML
AN EXPERIMENTAL INVESTIGATION ON RESPONSE OF TURBOJET ENGINE TO THE TURBULENCE-TYPE OF DYNAMIC INLET DISTORTION
Chen Fuqun;Li Wenlan;Wang Zongyuan;Cong Mengzi;Lu Baoquan;Zheng Lizhi
1984, (2): 225-232.
PDF [ 499 K ]( 435 ) HTML
APPLICATION OF A TWO-DIMENSIONAL LASER-DOPPLER ANEMOMETER （LDA）TO INVESTIGATION OF A COMPLEX FLOW FIELD IN COMBUSTOR
Lin Qinxun;Ding Yisheng;Du Qinfang;Tang Ming;Xiao Ningfang
1984, (2): 233-240.
PDF [ 468 K ]( 488 ) HTML
FAILURE BEHAVIOUR AND ACOUSTIC EMISSION ANALYSES OF MULTI-PLY CARBON/EPOXY COMPOSITE MATERIALS
Xian Xingjuan;Jiang Conxing
1984, (2): 241-247.
PDF [ 755 K ]( 347 ) HTML
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