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INFLUENCE OF THE REGULAR WATER WAVE UPON THE AERODYNAMIC CHARACTERISTICS OF A WING DURING THE LOW ALTITUDE FLYING
Lu Chuanjing;He Yousheng
1986, (5): 423-427.
PDF [ 304 K ]( 493 ) HTML
A DIGITAL SIMULATION TECHNIQUE FOR DRYDEN ATMOSPHERIC TURBULENCE MODEL
Zhao Zhenyan;Xiao Yelun;Shi Yijian
1986, (5): 433-443.
PDF [ 552 K ]( 786 ) HTML
SIZE EFFECTS ON FATIQUE CRACK INITIATION LIFE IN HIGH STRAIN AREAS NEAR NOTCHES
Wang Zhizhi;Nie Xuezhou
1986, (5): 444-451.
PDF [ 455 K ]( 360 ) HTML
EFFICIENCY ANALYSIS OF AIRBORNE ELECTRONIC COUNTERMEASURES （ECM） SYSTEMS
Zhang Yiting
1986, (5): 452-460.
PDF [ 551 K ]( 403 ) HTML
THE MODEL OF THE VARIABLE SPEED CONSTANT FREQUENCY CLOSED-LOOP SYSTEM OPERATING IN GENERATING STATE
Ding Daohong
1986, (5): 461-470.
PDF [ 500 K ]( 280 ) HTML
LOW COST DOPPLER AIDED STARPDOWN INERTIAL NAVIGATION SYSTEM
Yuan Xin;Yu Zaixin
1986, (5): 471-481.
PDF [ 566 K ]( 396 ) HTML
INCIPIENT MELTING AND ITS CONTROL IN A blRECTIONALLY SOLIDIFIED NICKEL-BASE SUPERALLOY DZ22
Zheng Yunrong
1986, (5): 482-489.
PDF [ 2361 K ]( 288 ) HTML
SPLIT-COEFFICIENT MATRIX FINIT DIFFERENCE METHOD FOR THE ASYMMETRIC NOSE-CONE
Zhang Lumin;Shan Xiaonan
1986, (5): 490-493.
PDF [ 219 K ]( 303 ) HTML
THE ROTATING NOSE METHOD FOR CONTROLING ASYMMETRIC FORCES AT HIGH ANGLE OF ATTACK
Yu Xinzhi;Yang Yongnian;Wu Ze;WangDaxuan;Wang Zongdong
1986, (5): 494-498.
PDF [ 273 K ]( 419 ) HTML
THE CHARACTERISTIC DEFICIT OF LINEAR VIBRATING SYSTEMS
Chen Zhenfan
1986, (5): 499-503.
PDF [ 270 K ]( 663 ) HTML
AN OPTIMAL DESIGN OF FLIGHT CONTROL SYSTEM BY OUTPUT FEEDBACK
Hu Shousong;Hu Minghua
1986, (5): 504-509.
PDF [ 291 K ]( 353 ) HTML
THE ELIMINATION OF LIMIT CYCLES OF AN AIRCRAFT FLIGHT CONTROL SYSTEM-LINEAR MODEL FOLLOWING APPROACH
Gao Jinyuan;Chen Zongji
1986, (5): 510-514.
PDF [ 311 K ]( 365 ) HTML
RESEARCH ON MICROSTRUCTURE OF GRAPHITEALUMINIUM COMPOSITE
Wu Shengjin;Sui Quanwu Wen Lishi.
1986, (5): 515-518.
PDF [ 1127 K ]( 542 ) HTML
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