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25 April 2000, Volume 21 Issue 2

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25 April 2000, Volume 21 Issue 2

ANALYSIS ON THE AERODYNAMIC BEHAVIORS OF THE SWEPT LEADING EDGE SHOCKS IN HIGH LOAD AXIAL COMPRESSORS
Abstract( 2233 )

SHAN Peng;LIU Xue-ying

2000, (2): 97-102.

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EFFECTS OF NON-LINEAR FACTORS IN NUMERICAL GRID GENERATION EQUATIONS ON ORTHOGONALITY AND SPACING
Abstract( 1636 )

LI Chun;CHENG Xin-guang

2000, (2): 103-107.

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NUMERICAL SIMULATION TO AIRCRAFT CABIN TEMPERATURE PHYSIOLOGICAL IDENTIFICATION
Abstract( 1476 )

QIU Yi-fen;YUAN Xiu-gan;CAO Zuo;SONG Ji-shen

2000, (2): 108-112.

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USING STRAKE VORTEX TO REDUCE THE DISTORTION OF A Y SHAPED INLET
Abstract( 1546 )

HUANG Guo-ping;YANG De-hua;LIANG De-wang;LI Bo

2000, (2): 113-117.

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COMPILATION THEORY OF MEDIAN STOCHASTIC FATIGUE LOAD SPECTRUM WITH HIGH CONFIDENCE LEVEL FOR AIRPLANE
Abstract( 1532 )

YAN Chu-liang;GAO Zhen-tong

2000, (2): 118-123.

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INFLUENCE OF THE CONSTITUTIVE EQUATIONS ON THE WELL-POSEDNESS OF FUNDAMENTAL EQUATIONS IN CONTINUUM DAMAGE MECHANICS ——THE CASE OF ONE DIMENSION ELASTIC DAMAGE
Abstract( 1759 )

HUANG Zai-xing

2000, (2): 124-127.

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EQUIVALENT ENVIRONMENT SPECTRUM RESEARCH OF DETERMINING CALENDAR LIFE FOR AIRCRAFT
Abstract( 1402 )

ZHANG Dong

2000, (2): 128-133.

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STUDY ON MULTITASK MANAGEMENT UNIT MTU OF EMBEDDED MICROPROCESSOR NCS
Abstract( 1890 )

LI Shu-guo;GAO De-yuan;NIE Pei-qin

2000, (2): 134-137.

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DESIGN AND REALIZATION OF AIRBORNE PD TRACKING RADAR SIGNAL PROCESSOR
Abstract( 2144 )

ZENG Tao;LONG Teng

2000, (2): 138-141.

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ATTITUDE CONTROL SYSTEM DESIGN FOR SMALL SATELLITE EARTH ACQUISITION WITH ACTIVE MAGNETIC CONTROL
Abstract( 2193 )

GENG Yun-hai;CUI Hu-tao;SUN Zhao-wei;YANG Di

2000, (2): 142-145.

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A CENTRALIZED COORDINATED PATH PLANNING METHOD BASED ON GENETIC ALGORITHM FOR MULTIPLE MODILE ROBOTS
Abstract( 2152 )

ZHOU Ming;SUN Shu-dong;PENG Yan-wu

2000, (2): 146-149.

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ADAPTIVE CONTROL OF SPACE-BASED MANIPULATOR WITH UNCERTAIN PARAMETERS
Abstract( 2108 )

CHEN Li;LIU Yan-zhu

2000, (2): 150-154.

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INTEGRAL INFERENCE METHOD FOR THE BINOMIAL DISTRIBUTION PARAMETER
Abstract( 2425 )

FU Hui-min

2000, (2): 155-158.

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MODELING OF PIEZOELECTRIC THIN PLATES AND QUASI INDEPENDENT MODAL CONTROL FOR DAMPING
Abstract( 1897 )

YAO Jun;LI Yue-feng;LIU Juan

2000, (2): 159-163.

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CONVERSION METHOD OF EQUIVALENT LOAD FOR PRE-FATIGUE TEST OF No.58 TITANIUM FRAME
Abstract( 1316 )

WANG Xiang-ming;ZHANG Yi-ning

2000, (2): 164-166.

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ACTIVE CONSTRAINED LAYER DAMPING TREATMENT OF SUPPORTER
Abstract( 1169 )

TIAN Xiao-geng;SHEN Ya-peng;ZHANG Yuan-chong

2000, (2): 167-170.

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STUDY ON CYCLIC STRESS-STRAIN BEHAVIOR AND CYCLIC STRAIN-LIFE RELATION OF MATERIALS
Abstract( 1576 )

WANG Bin-tuan;YANG Qing-xiong

2000, (2): 171-174.

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ROBUST H_∞ CONTROLLER DESIGN FOR AERO ENGINE BASED ON LMI
Abstract( 1458 )

XIE Guang-hua;ZENG Qing-fu

2000, (2): 175-178.

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VISUALIZATION AND ANIMATION OF CFD RESULTS
Abstract( 1512 )

FAN Yan-bin;MENG Guang;SHEN Zi-lin;YANG Peng-ji

2000, (2): 179-182.

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STUDY OF MATHEMATICAL MODELS IN MATERIAL CORROSION PREDICTION
Abstract( 1410 )

CHENG Ji-wei;ZHANG Qi

2000, (2): 183-186.

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FACE CONFIGURATION WITH HIGH PERFORMANCE FOR GAS FILM FACE SEAL
Abstract( 1487 )

LIU Yu-chuan;XU Wan-fu;CHEN Guo-lin;SHEN Xin-min

2000, (2): 187-190.

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