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25 February 1987, Volume 8 Issue 2

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25 February 1987, Volume 8 Issue 2

论文

NEW CONTENT OF TACTICAL-TECHNICAL REQUIREMENTS FOR MILITARY AIRCRAFTS IN THE EARLY PART OF THE 21ST CENTARY——THE STEALTH PENETRATION ABILITY
Abstract( 1112 )

Zhang Kao

1987, (2): 1-10.

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A COMPREHENSIVE REVIEW OF THE MODELS FOR PREDICTING FATIGUE CRACK GROWTH UNDER SPECTRUM LOADING
Abstract( 1378 )

Si Erjian

1987, (2): 11-18.

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MEASUREMENTS ON STIFFNESS AND DAMPING COEFFICIENTS OF“O”TYPE RUBBER RING
Abstract( 1892 )

Yin Peiqi

1987, (2): 19-21.

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AN ANALYSIS OF FLIGHT TEST AND DESIGN CONSIDERATION
Abstract( 1569 )

Ma Yu

1987, (2): 22-31.

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PREDICTION OF FATIGUE LIFE FOR TENSION BOLTS AND LUGS
Abstract( 1369 )

Xue Jingchuan;He Gongtai;Yang Yugong

1987, (2): 33-38.

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LOADED CAPABILITY OF AIRFRAME IN THE PROCESS OF DAMAGE——FINITE ELEMENT ANALYSIS FOR STRUCTURAL FAILURE AREA
Abstract( 2816 )

Huang Jingxian;Huang Yazhang;Liu Xiashi

1987, (2): 39-46.

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EXPERIMENTAL STUDY OF A TWO-DIMENSIONAL RANDOM FREQUENCY GENERATOR
Abstract( 1345 )

Peng Chengyi;Ma Jiaju

1987, (2): 47-54.

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THE APPLICATION OF ELECTRO-MAGNETIC EDDY CURRENT TECHNIQUE FOR VIBRATION FATIGUE TESTING
Abstract( 1212 )

Xu Zhihuai

1987, (2): 55-61.

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DESIGN OF SPIRAL ANTENNA BY USE OF COMPUTER DRAWING
Abstract( 1365 )

Fu Canglin

1987, (2): 63-67.

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LBTR Block Diagram Approach to the Digital Simulation of Linear Systems
Abstract( 1420 )

Gu Qitai

1987, (2): 69-74.

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INFLUENCE OF SHOP FLOOR THERMAL EXPANSION ON INTERCHANGEABILITY AND COORDINATION OF AIRCRAFT DURING ASSEMBLY
Abstract( 1309 )

Liu Zhungliang

1987, (2): 75-82.

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TO DETERMINE THE MINIMUM CLEARANCE IN LOCATING WITH TWO PINS BY PROBABILITY METHOD
Abstract( 1175 )

Cheng Baoqu

1987, (2): 83-86.

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ON IMPLEMENTING AN INTERACTIVE ENGINEERING CAD SYSTEM IN A MICROCOMPUTER
Abstract( 1351 )

He Linshu

1987, (2): 87-91.

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EXPERIMENTAL STUDY ON A COMBUSTOR WITH VORTEX-CONTROLLED DUMP DIFFUSER
Abstract( 1883 )

Cheng Bingtai;Niu Yanyun;Jiang Zhili

1987, (2): 92-96.

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ACCELERATION TEST STUDY ON PLUNGER-TYPE FUEL PUMP OF JET ENGINE
Abstract( 1429 )

Wang Yunpu;Li Lanjiang

1987, (2): 97-100.

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APPLICATION OF A LASER-DOPPLER ANEMOMETER（LDA） TO MEASURE THE FLOW FIELD IN FREE JETS
Abstract( 1340 )

Lin Qixun;Jiang Zhengxing;Du Qinfang;Xiao Ningfang

1987, (2): 101-104.

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PARAMETER OPTIMIZATION PROGRAM FOR THE DAMPED （STABILITY AUGMENTED） SYSTEM OF AIRCRAFTS
Abstract( 1377 )

Feng Yachang;Suo jin

1987, (2): 105-109.

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FEASIBILITY STUDY OF TESTING FOR NON-EDSMANTLE TEST TO THE AIRCRAFT ELECTRONIC EQUIPMENT
Abstract( 1428 )

Kong Derong

1987, (2): 111-114.

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IMPROVEMENTS IN TEST METHOD FOR FATIGUE THRESHOLDS AND LOW FATIGUE CRACK GROWTH RATE
Abstract( 1299 )

Ding Chuanfu;Zhao Wei;Gu Mingda

1987, (2): 115-118.

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