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25 April 1993, Volume 14 Issue 4

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25 April 1993, Volume 14 Issue 4

论文

AERODYNAMIC DESIGN CRITERIA,DESIGN PROCEDURES AND A DESIGN EXAMPLE OF SUPERCRITICAL WING
Abstract( 1710 )

Shen Ke-yang;Zhang Xi-hua

1993, (4): 113-117.

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DESIGN FOR CONTROL LAWS OF MANEUVER FLAPS AND A STUDY OF THE DYNAMIC CHARACTERISTICS OF THE AIRPLANE
Abstract( 1726 )

Zhou Zhou;Liu Qian-gang

1993, (4): 118-125.

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ANALYSIS OF STATISTICAL VIBRATION IN AIRCRAFT DURING TAXIING
Abstract( 1994 )

Liu LiYang;Guo-zhu;He Qing-zhi

1993, (4): 126-132.

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DEVELOPMENT OF STATE ESTIMATION AND PARAMETER IDENTIFICATION SOFTWARE PACKAGE FOR MILITARY AIRCRAFT
Abstract( 1750 )

Deng Jian-hua;Long De-chun;Ai Jian-liang;Zhang Jun-sing

1993, (4): 133-138.

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PSEUDO-ELEMENT METHOD (PEM) FOR SOLVING CYCLIC SYMMETRIC STRUCTURE
Abstract( 1317 )

Shen Yun-wen;Liu Geng;He Da-wei;Yin Ze-yong

1993, (4): 139-144.

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APPLICATION OF FUZZY CONTROL THEORY TO CONTROL SYSTEM OF AERO-TURBOJET ENGINE
Abstract( 1234 )

Fan Ding;Yu Jin-wen;WuChi-hua

1993, (4): 145-152.

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AN ANALYSIS OF DAMAGE FAILURE OF PLUNGER HOLE WALL FOR THE PUMP ZB-16D
Abstract( 1385 )

Zhang Jia-zhen;Lu ShanCui Wei-jun;Shang Quan-li

1993, (4): 153-158.

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STUDY AND SIMULATION OF FIRE CONTROL SYSTEM OF ADVANCED ARMED HELICOPTER
Abstract( 1470 )

Sun Long-he;Cai Ruo-hong

1993, (4): 159-168.

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SCFT:A TMR-BITE FAULT-TOLERANT COMPUTER SYSTEM BASED UPON 16-BIT SINGLE-CHIP MICROCOMPUTERS
Abstract( 2042 )

Huang Feng-ying;Ji Gen-lin;Li Zhen;Zhuang yi

1993, (4): 169-174.

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LONGITUDINAL DFBW CONTROL LAW DESIGN FOR A CERTAIN ACT DEMONSTRATION AIRCRAFT
Abstract( 1155 )

Li Zhi-xin

1993, (4): 175-180.

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THE ELECTRO-CONTACT DISCHARGE DRESSING METAL BONDED DIAMOND GRINDING WHEELS WITH A COUPLE OF ELECTRODES
Abstract( 1637 )

Xu Jia wen;Peng Cun-ping;Tang Ya-xin

1993, (4): 181-186.

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NUMERCAL SIMULATION FOR THREE-DIMENSIONAL CASTINGS IN DIRECTIONAL SOLIDIFICATION PROCESS Ⅱ——The BEM Solution to The DS Process in Transient State
Abstract( 1326 )

Zhang ke-fu;Mao Xie-ming;Fu Heng-zhi

1993, (4): 187-192.

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NUMERICAL SOLUTION TO THE NON-CIRCULAR FACTORS AND THE CORRECTING COEFFICIENTS OF WING-BODY INTERFERENCE FACTORS OF FLIGHT VEHICLE
Abstract( 1334 )

Yang Zhen-sheng

1993, (4): 193-196.

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AERODYNAMIC SHAPE SMOOTHING AND ITS INFLUENCE ON THE EFFECT OF AERODYNAMIC NUMERICAL SIMULATION
Abstract( 1418 )

Zhang Yong;Zhang Zhong-yin

1993, (4): 197-199.

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DESIGN AND APPLICATIONS OF EXPERT SYSTEM ESOPD FOR STRUCTURAL OPTIMIZATION
Abstract( 1438 )

Sun Xia-sheng;Ding Hui-liang;Li Bing-gong

1993, (4): 200-202.

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PARAMETER OPTIMIZATION OF THE ENGINE SPEED CONTROL SYSTEM
Abstract( 1499 )

Xu Yun-hua;Fan Si-qi

1993, (4): 203-206.

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SIMULATION OF DISTORTED FLOW FIELD WITH HIGH TURBULENCE LEVEL
Abstract( 1305 )

Liang De-wang;Zhang Shi-ying

1993, (4): 207-209.

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WHIRL FLUTTER ANALYSIS
Abstract( 1674 )

Jin Yi-chen

1993, (4): 210-213.

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A STUDY ON CARBON FABRIC PPS COMPOSITES
Abstract( 1656 )

Wang Yu-qi

1993, (4): 214-218.

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ANALOGUE SIMULATION OF AIRCRAFT ELECTRONIC ANTISKID BRAKE SYSTEM
Abstract( 1284 )

Xu Xi-ru

1993, (4): 219-222.

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DEVELOPMENT OF HUMAN ERROR DATA BASE IN AERONAUTIC FACILITIES
Abstract( 1365 )

Dai Guang-ya

1993, (4): 222-223.

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