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25 April 1996, Volume 17 Issue 2

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25 April 1996, Volume 17 Issue 2

论文

SURVEY ON THE APPLICATIONS OF H~∞ METHOD IN ROBUST FLIGHT CONTROL SYSTEMS DESIGN
Abstract( 1437 )

Wang Yansheng;Chen Zongji

1996, (2): 129-136.

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REVIEW OF THE GREEN'S FUNCTION METHOD FOR STEADY AND UNSTEADY,SUBSONIC, TRANSONIC AND SUPERSONIC AERODYNAMICS AROUND COMPLEX CONFIGURATION
Abstract( 1634 )

Liu Qiangang

1996, (2): 137-143.

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MULTISTAGE GENERALIZED FINITE ELEMENT METHOD FOR TWO DIMENSIONAL VISCOUS TRANSONIC FLOW IN TURBOMACHINERY
Abstract( 1318 )

Zhu Gang;Shen Mengyu;Liu Qiusheng;Wang Baoguo

1996, (2): 144-148.

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EXPERIMENTAL INVESTIGATION ON THE TURBULENT COHERENT STRUCTURES OF LAMINAR SEPARATION FLOW OVER A BACKWARD-FACING STEP
Abstract( 1535 )

Wang Jinjun;Lian Qixiang;Lan Shilong

1996, (2): 149-154.

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VARIABLE STRUCTURE GUIDANCE LAW FOR EXTRA-ATMOSPHERIC INTERCEPTION
Abstract( 1278 )

Wang Jiayun;Er Lianjie;Wu Wenzheng;Wang Xiaodong

1996, (2): 155-161.

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AN EXPERIMENTAL INVESTIGATION OF FUEL DISTRIBUTION OF DOUBLE-SWIRLER AIRBLASTER ATOMIZER FITTED IN A RECTANGULAR TESTING COMBUSTOR
Abstract( 1495 )

Lin Yuzhen;Xing yumin;Wang Huafang;Liu Gaoen

1996, (2): 162-168.

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THE MODEL OF MTT SYSTEM AND COMPENSATION OF VEHICLE MOTION IN AIRBORNE RADAR
Abstract( 1485 )

Li Shaohong;Mao Shiyi;Hu Xiao

1996, (2): 169-176.

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STUDY AND DESIGN OF A FLIGHT NEUROCONTROL SYSTEM
Abstract( 1321 )

Ruan Xiaogang;Guo Suofeng

1996, (2): 177-184.

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ANALYSIS OF MICROSTRUCTURE AND INTERMETALLIC PHASES IN A RAPIDLY SOLIDIFIED AL94Ti4C2 ALLOY
Abstract( 1659 )

Tong Xingcun;Shen Ningf Liu Beicheng

1996, (2): 185-189.

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FORM FEATURE CLASSIFICATION AND REPRESENTATION FOR CAD/CAM INTEGRATION
Abstract( 1518 )

Wang Cunhe;Zhang Tiechang

1996, (2): 190-195.

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EXPERIMENTAL STUDY ON EFFECTS ON DELAMINATION NEAR CRACK OF ARALL BY RESIDUAL STRESS UNDER FATIGUE AND STATIC LOADS
Abstract( 1645 )

Zhong Weihong;Chen Changqi;Kou Changhe;Zheng Ruiqi

1996, (2): 196-201.

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INVESTIGATION ON FRACTURE MECHANISM OF AN AIRCRAFT LANDING GEAR HUB
Abstract( 1608 )

Su Xijiu;Chen Shenchuan;Chen ying;Wang Shoukai

1996, (2): 202-207.

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BOUNDARY LAYER EQUATIONS IN NONINERTIAL CURVILINEAR COORDINATE SYSTEM
Abstract( 1290 )

Sun Mao

1996, (2): 208-212.

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FREE-WAKW CALCULATION OF HELICOPTER ROTOR BLADES
Abstract( 1900 )

Liu Xiangjian;Shen Xinkang;Xue Zhengzhong

1996, (2): 213-217.

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AN APPROACH OF PREDICTING ROTOR BLADE AIRLOAD BASED ON AERODYNAMIC SCALE
Abstract( 1146 )

Kang Hao;Liu Shoushen

1996, (2): 218-221.

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STUDY OF THE CLOSED-LOOP REAL-TIME ENGINE MODEL USED IN FLIGHT SIMULATOR
Abstract( 1538 )

Yang Weihua;Sun Jianguo;Xu Weijin;Zhao Bo

1996, (2): 222-226.

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ABILITY OF AN ADVANCED HYBRID SQUEEZE FILM DAMPER TO CONTROL ROTOR SYSTEM VIBRATION
Abstract( 1460 )

Zhu Changsheng

1996, (2): 227-233.

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THE VERIFICATION OF Dy AND Yd TYPE TRANSFORMER CONNECTION WITH COMPUTER
Abstract( 1661 )

Wang Shixu

1996, (2): 234-238.

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NEW FAILURE DETECTION METHOD FOR THE INTEGRATED INS/GPS NAVIGATION SYSTEM
Abstract( 1290 )

Yan Dong;Zhang Hongyue

1996, (2): 239-242.

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STUDY ON DUAL ELECTRO-HYDRAULIC SERVO MOTOR SYNCHRONIZING DRIVE
Abstract( 1241 )

Fu Yongling;Zhao Keding;Liu Qinghe

1996, (2): 243-247.

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A RECURRENCE IDENTIFICATION ALGORITHM FOR MISSILE CONTROL SYSTEM USING CO-VARIANCE MATRIX RESET
Abstract( 1112 )

Xu Jie;Li Yanjun

1996, (2): 248-250.

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OPTIMAL DESIGN OF MECHANICAL CONTROL SYSTEM OF AIRCRAFT
Abstract( 1221 )

Wang Yibing;Wang Zhanlin;Cui Jinbao;Feng Yachang

1996, (2): 251-255.

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