导航
Archive
BEHAVIOUR ON DAMAGE TOLERANCE OF COMPOSITE AIRCRAFT STRUCTURES
Shen Zhen
1988, (2): 1-10.
PDF [ 799 K ]( 936 ) HTML
THE CHARACTERISTICS OF ASYMMETRIC VORTICES AND SIDE FORCES ON A SHARP-NOSED BODY WITH WING AND VERTICAL TAIL
Chen Nanqian
1988, (2): 11-16.
PDF [ 405 K ]( 325 ) HTML
AN ENGINEERING METHOD OF OPTIMAL LAMINA DESIGN FOR THE COMPOSITE PLATE AND SHELL UNDER POSTBOCKLING
Cheng Wanzhi
1988, (2): 17-24.
PDF [ 462 K ]( 303 ) HTML
THE INTEGRATED DESIGN OF MISSILE WITH SOLID ROCKET -RAMJET COMBINATION
Wang Jiayun;Zhan Zhangpeng and Qu Ziqiang
1988, (2): 25-34.
PDF [ 695 K ]( 357 ) HTML
A STUDY ON SEPARATION FLOW CONTROL OF DIFFUSER
Huang Xijun;Bao Feng;Dong Jinzhong and Xiao Chengshu
1988, (2): 35-40.
PDF [ 453 K ]( 360 ) HTML
A STUDY OF DIGITAL FLY-BY-WIRE CONTROL SYSTEM DESIGN FOR ELASTIC AIRCRAFT
Li Lichun
1988, (2): 41-50.
PDF [ 613 K ]( 315 ) HTML
CONTROL LAW DESIGN OF A CCV AIRPLANE
Feng Gang
1988, (2): 51-57.
PDF [ 392 K ]( 318 ) HTML
THE RESEARCH FOR DIFFERENTIAL CYLINDER SERVO SYSTEM
Wang Zhanlin and Qiu Lihua
1988, (2): 58-67.
PDF [ 624 K ]( 270 ) HTML
A STUDY ON THE LAW OF SHIELDING DURING MICROBEAM ARC WELDING OF TITANIUM ALLOY SHEETS
Zhang Renfu;Tang Nan and Tang Chunlin
1988, (2): 68-76.
PDF [ 1130 K ]( 290 ) HTML
ENGINEERING METHOD FOR PREDICTING PRESSURE AND HEAT RATE OF THE COMPRESSIBLE CORNER REGION
Yang Maozhao
1988, (2): 77-81.
PDF [ 299 K ]( 376 ) HTML
A HIGH ORDER CURVE FITTING FOR ISOLIFE CURVES
Yang Derong
1988, (2): 82-86.
PDF [ 322 K ]( 342 ) HTML
EXPERIMENTAL STUDY ON APPLICABILITY OF DAMAGE FAILURE CRITERION FOR COMPOSITES
Shen Zhen;Liu Junshi;Tang Xiaodong;Huang Qi;Shen Wei
1988, (2): 87-90.
PDF [ 291 K ]( 349 ) HTML
COMPUTER AIDED DETERMINATION OF THE SITE LIMIT OF THERE HOLE GROUP
Chen Bingchen
1988, (2): 91-95.
PDF [ 296 K ]( 424 ) HTML
Academic Quality
Download Ranking