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SURVEY ON THE APPLICATIONS OF H~∞ METHOD IN ROBUST FLIGHT CONTROL SYSTEMS DESIGN
Wang Yansheng;Chen Zongji
1996, (2): 129-136.
PDF [ 297 K ]( 866 ) HTML
REVIEW OF THE GREEN'S FUNCTION METHOD FOR STEADY AND UNSTEADY,SUBSONIC, TRANSONIC AND SUPERSONIC AERODYNAMICS AROUND COMPLEX CONFIGURATION
Liu Qiangang
1996, (2): 137-143.
PDF [ 278 K ]( 621 ) HTML
MULTISTAGE GENERALIZED FINITE ELEMENT METHOD FOR TWO DIMENSIONAL VISCOUS TRANSONIC FLOW IN TURBOMACHINERY
Zhu Gang;Shen Mengyu;Liu Qiusheng;Wang Baoguo
1996, (2): 144-148.
PDF [ 284 K ]( 719 ) HTML
EXPERIMENTAL INVESTIGATION ON THE TURBULENT COHERENT STRUCTURES OF LAMINAR SEPARATION FLOW OVER A BACKWARD-FACING STEP
Wang Jinjun;Lian Qixiang;Lan Shilong
1996, (2): 149-154.
PDF [ 193 K ]( 683 ) HTML
VARIABLE STRUCTURE GUIDANCE LAW FOR EXTRA-ATMOSPHERIC INTERCEPTION
Wang Jiayun;Er Lianjie;Wu Wenzheng;Wang Xiaodong
1996, (2): 155-161.
PDF [ 211 K ]( 591 ) HTML
AN EXPERIMENTAL INVESTIGATION OF FUEL DISTRIBUTION OF DOUBLE-SWIRLER AIRBLASTER ATOMIZER FITTED IN A RECTANGULAR TESTING COMBUSTOR
Lin Yuzhen;Xing yumin;Wang Huafang;Liu Gaoen
1996, (2): 162-168.
PDF [ 420 K ]( 658 ) HTML
THE MODEL OF MTT SYSTEM AND COMPENSATION OF VEHICLE MOTION IN AIRBORNE RADAR
Li Shaohong;Mao Shiyi;Hu Xiao
1996, (2): 169-176.
PDF [ 366 K ]( 845 ) HTML
STUDY AND DESIGN OF A FLIGHT NEUROCONTROL SYSTEM
Ruan Xiaogang;Guo Suofeng
1996, (2): 177-184.
PDF [ 366 K ]( 399 ) HTML
ANALYSIS OF MICROSTRUCTURE AND INTERMETALLIC PHASES IN A RAPIDLY SOLIDIFIED AL94Ti4C2 ALLOY
Tong Xingcun;Shen Ningf Liu Beicheng
1996, (2): 185-189.
PDF [ 327 K ]( 467 ) HTML
FORM FEATURE CLASSIFICATION AND REPRESENTATION FOR CAD/CAM INTEGRATION
Wang Cunhe;Zhang Tiechang
1996, (2): 190-195.
PDF [ 219 K ]( 404 ) HTML
EXPERIMENTAL STUDY ON EFFECTS ON DELAMINATION NEAR CRACK OF ARALL BY RESIDUAL STRESS UNDER FATIGUE AND STATIC LOADS
Zhong Weihong;Chen Changqi;Kou Changhe;Zheng Ruiqi
1996, (2): 196-201.
PDF [ 281 K ]( 537 ) HTML
INVESTIGATION ON FRACTURE MECHANISM OF AN AIRCRAFT LANDING GEAR HUB
Su Xijiu;Chen Shenchuan;Chen ying;Wang Shoukai
1996, (2): 202-207.
PDF [ 343 K ]( 507 ) HTML
BOUNDARY LAYER EQUATIONS IN NONINERTIAL CURVILINEAR COORDINATE SYSTEM
Sun Mao
1996, (2): 208-212.
PDF [ 265 K ]( 643 ) HTML
FREE-WAKW CALCULATION OF HELICOPTER ROTOR BLADES
Liu Xiangjian;Shen Xinkang;Xue Zhengzhong
1996, (2): 213-217.
PDF [ 287 K ]( 1085 ) HTML
AN APPROACH OF PREDICTING ROTOR BLADE AIRLOAD BASED ON AERODYNAMIC SCALE
Kang Hao;Liu Shoushen
1996, (2): 218-221.
PDF [ 197 K ]( 551 ) HTML
STUDY OF THE CLOSED-LOOP REAL-TIME ENGINE MODEL USED IN FLIGHT SIMULATOR
Yang Weihua;Sun Jianguo;Xu Weijin;Zhao Bo
1996, (2): 222-226.
PDF [ 273 K ]( 872 ) HTML
ABILITY OF AN ADVANCED HYBRID SQUEEZE FILM DAMPER TO CONTROL ROTOR SYSTEM VIBRATION
Zhu Changsheng
1996, (2): 227-233.
PDF [ 286 K ]( 721 ) HTML
THE VERIFICATION OF Dy AND Yd TYPE TRANSFORMER CONNECTION WITH COMPUTER
Wang Shixu
1996, (2): 234-238.
PDF [ 262 K ]( 1758 ) HTML
NEW FAILURE DETECTION METHOD FOR THE INTEGRATED INS/GPS NAVIGATION SYSTEM
Yan Dong;Zhang Hongyue
1996, (2): 239-242.
PDF [ 187 K ]( 454 ) HTML
STUDY ON DUAL ELECTRO-HYDRAULIC SERVO MOTOR SYNCHRONIZING DRIVE
Fu Yongling;Zhao Keding;Liu Qinghe
1996, (2): 243-247.
PDF [ 299 K ]( 576 ) HTML
A RECURRENCE IDENTIFICATION ALGORITHM FOR MISSILE CONTROL SYSTEM USING CO-VARIANCE MATRIX RESET
Xu Jie;Li Yanjun
1996, (2): 248-250.
PDF [ 161 K ]( 593 ) HTML
OPTIMAL DESIGN OF MECHANICAL CONTROL SYSTEM OF AIRCRAFT
Wang Yibing;Wang Zhanlin;Cui Jinbao;Feng Yachang
1996, (2): 251-255.
PDF [ 366 K ]( 689 ) HTML
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