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AN AERODYNAMIC DESIGN CONCEPT FOR A STRAKE-WING AND ASSOCIATED PARAMETER SELECTING RULES—LONGITUDINAL CHARACTERISTIC ANALYSES
Lu Zhiyong
1987, (8): 329-340.
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DEVELOPMENT TRENDS FOR EJECTION SEAT
Shen Erkang
1987, (8): 341-347.
PDF [ 581 K ]( 516 ) HTML
A REVIEW OF THE DEVELOPMENT OF COMPOSITE FAN BLADES
Li Rui;Song Huancheng
1987, (8): 348-354.
PDF [ 510 K ]( 715 ) HTML
A STUDY ON EFFECTS OF AIRCRAFT NOISE ENVIRONMENT ON ITS STRUCTURE
Fu Shijian
1987, (8): 355-361.
PDF [ 488 K ]( 474 ) HTML
THE GENERALIZED J-INTEGRAL METHOD OF SOLUTION ABOUT STRESS INTESITY FACTOR FOR CRACKED ROTATING DISK WITH UARIABLE THICKNESS UNDER NON-UNIFORM TEMPERATURE FIELD
Fan Xiochang;Zhang Xing
1987, (8): 362-369.
PDF [ 407 K ]( 293 ) HTML
USING INTEGRAL TEMPERATURE CRITERION TO PREDICT SCUFFING FAILURE OF BEVEL GEARS FOR AIRCRAFT
Pan Shengcai;Wu Linfeng;Zhong Suixiang;Ouyang Zuxing
1987, (8): 370-376.
PDF [ 427 K ]( 499 ) HTML
AN ANALYTICAL AND EXPERIMENTAL STUDY OF A SUBSONIC DIFFUSER OF A SUPERSONIC INLET
Sun Xiaohua;Huang Xijuh
1987, (8): 377-381.
PDF [ 314 K ]( 378 ) HTML
DIGITAL SIMULATION OF DYNAMIC RESPONSE OF ANALOG AIR DATA COMPUTER
Peng Pusheng
1987, (8): 382-390.
PDF [ 564 K ]( 336 ) HTML
STUDY ON THE PILOT-INDUCED OSCILLATION OF LONGITUDINAL PILOT-AIRPLANE SYNTHESIS SYSTEM
Feng Yachang;Muo Songfen;Yao Tiemei;Xu Xinfu
1987, (8): 391-398.
PDF [ 507 K ]( 448 ) HTML
ON THE STUDY OF ENGINEERING METHOD FOR COMPUTING EFFECTIVE MINIMUM INTERFERENCE
Wu Li
1987, (8): 400-405.
PDF [ 372 K ]( 846 ) HTML
ANALYSES OF METAL FLOW AND STRUCTURE IN BLADE PRECISION FORGING BY RIGID-VISCOPLASTIC FINITE ELEMENT METHOD
Lian Jianmin;Li Xunti;Li Chenggong
1987, (8): 406-415.
PDF [ 1012 K ]( 435 ) HTML
AN OVERVIEW ON THE IMPLEMENTATION OF RELIABILITY-CENTERED MAINTENANCE
Hu Shihua
1987, (8): 416-421.
PDF [ 477 K ]( 376 ) HTML
THE METHOD OF COMPUTER-AIDED CONSTRUCTION AND DRAWING OF A PROJECT NETWORK
Ning Xuanxi;Lei Weizhong
1987, (8): 422-429.
PDF [ 507 K ]( 391 ) HTML
THE APPLICATION OF FUZZY SETS THEORY TO OPTIMAL DESIGN OF PRELIMINARY PARAMETERS OF AIRCRAFT
Zhang Yongshun;Wei Fazie
1987, (8): 430-435.
PDF [ 411 K ]( 370 ) HTML
THE FLIGHT TEST OF TWIN-SPOOL TURBOJET ENGINE SIMULATING THE INGESTION OF MISSILE EXHAUST
Zuo Hanzhong
1987, (8): 436-440.
PDF [ 315 K ]( 437 ) HTML
HIERARCHICAL SELF-TUNING FLIGHT CONTROL
Fu Li
1987, (8): 441-446.
PDF [ 328 K ]( 268 ) HTML
THE PRINCIPLE FOR CALCULATING THE FILAMENT-WOUND NETTING STRUCTURE
Leng Xingwu
1987, (8): 447-450.
PDF [ 362 K ]( 682 ) HTML
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