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NEW CONTENT OF TACTICAL-TECHNICAL REQUIREMENTS FOR MILITARY AIRCRAFTS IN THE EARLY PART OF THE 21ST CENTARY——THE STEALTH PENETRATION ABILITY
Zhang Kao
1987, (2): 1-10.
PDF [ 755 K ]( 339 ) HTML
A COMPREHENSIVE REVIEW OF THE MODELS FOR PREDICTING FATIGUE CRACK GROWTH UNDER SPECTRUM LOADING
Si Erjian
1987, (2): 11-18.
PDF [ 446 K ]( 388 ) HTML
MEASUREMENTS ON STIFFNESS AND DAMPING COEFFICIENTS OF“O”TYPE RUBBER RING
Yin Peiqi
1987, (2): 19-21.
PDF [ 222 K ]( 538 ) HTML
AN ANALYSIS OF FLIGHT TEST AND DESIGN CONSIDERATION
Ma Yu
1987, (2): 22-31.
PDF [ 716 K ]( 365 ) HTML
PREDICTION OF FATIGUE LIFE FOR TENSION BOLTS AND LUGS
Xue Jingchuan;He Gongtai;Yang Yugong
1987, (2): 33-38.
PDF [ 365 K ]( 359 ) HTML
LOADED CAPABILITY OF AIRFRAME IN THE PROCESS OF DAMAGE——FINITE ELEMENT ANALYSIS FOR STRUCTURAL FAILURE AREA
Huang Jingxian;Huang Yazhang;Liu Xiashi
1987, (2): 39-46.
PDF [ 524 K ]( 408 ) HTML
EXPERIMENTAL STUDY OF A TWO-DIMENSIONAL RANDOM FREQUENCY GENERATOR
Peng Chengyi;Ma Jiaju
1987, (2): 47-54.
PDF [ 621 K ]( 416 ) HTML
THE APPLICATION OF ELECTRO-MAGNETIC EDDY CURRENT TECHNIQUE FOR VIBRATION FATIGUE TESTING
Xu Zhihuai
1987, (2): 55-61.
PDF [ 660 K ]( 498 ) HTML
DESIGN OF SPIRAL ANTENNA BY USE OF COMPUTER DRAWING
Fu Canglin
1987, (2): 63-67.
PDF [ 329 K ]( 300 ) HTML
LBTR Block Diagram Approach to the Digital Simulation of Linear Systems
Gu Qitai
1987, (2): 69-74.
PDF [ 365 K ]( 276 ) HTML
INFLUENCE OF SHOP FLOOR THERMAL EXPANSION ON INTERCHANGEABILITY AND COORDINATION OF AIRCRAFT DURING ASSEMBLY
Liu Zhungliang
1987, (2): 75-82.
PDF [ 470 K ]( 348 ) HTML
TO DETERMINE THE MINIMUM CLEARANCE IN LOCATING WITH TWO PINS BY PROBABILITY METHOD
Cheng Baoqu
1987, (2): 83-86.
PDF [ 236 K ]( 265 ) HTML
ON IMPLEMENTING AN INTERACTIVE ENGINEERING CAD SYSTEM IN A MICROCOMPUTER
He Linshu
1987, (2): 87-91.
PDF [ 310 K ]( 225 ) HTML
EXPERIMENTAL STUDY ON A COMBUSTOR WITH VORTEX-CONTROLLED DUMP DIFFUSER
Cheng Bingtai;Niu Yanyun;Jiang Zhili
1987, (2): 92-96.
PDF [ 323 K ]( 364 ) HTML
ACCELERATION TEST STUDY ON PLUNGER-TYPE FUEL PUMP OF JET ENGINE
Wang Yunpu;Li Lanjiang
1987, (2): 97-100.
PDF [ 252 K ]( 352 ) HTML
APPLICATION OF A LASER-DOPPLER ANEMOMETER（LDA） TO MEASURE THE FLOW FIELD IN FREE JETS
Lin Qixun;Jiang Zhengxing;Du Qinfang;Xiao Ningfang
1987, (2): 101-104.
PDF [ 235 K ]( 643 ) HTML
PARAMETER OPTIMIZATION PROGRAM FOR THE DAMPED （STABILITY AUGMENTED） SYSTEM OF AIRCRAFTS
Feng Yachang;Suo jin
1987, (2): 105-109.
FEASIBILITY STUDY OF TESTING FOR NON-EDSMANTLE TEST TO THE AIRCRAFT ELECTRONIC EQUIPMENT
Kong Derong
1987, (2): 111-114.
PDF [ 276 K ]( 252 ) HTML
IMPROVEMENTS IN TEST METHOD FOR FATIGUE THRESHOLDS AND LOW FATIGUE CRACK GROWTH RATE
Ding Chuanfu;Zhao Wei;Gu Mingda
1987, (2): 115-118.
PDF [ 288 K ]( 358 ) HTML
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