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ANALYSIS ON THE AERODYNAMIC BEHAVIORS OF THE SWEPT LEADING EDGE SHOCKS IN HIGH LOAD AXIAL COMPRESSORS
SHAN Peng;LIU Xue-ying
2000, (2): 97-102.
PDF [ 273 K ]( 586 ) HTML
EFFECTS OF NON-LINEAR FACTORS IN NUMERICAL GRID GENERATION EQUATIONS ON ORTHOGONALITY AND SPACING
LI Chun;CHENG Xin-guang
2000, (2): 103-107.
PDF [ 304 K ]( 775 ) HTML
NUMERICAL SIMULATION TO AIRCRAFT CABIN TEMPERATURE PHYSIOLOGICAL IDENTIFICATION
QIU Yi-fen;YUAN Xiu-gan;CAO Zuo;SONG Ji-shen
2000, (2): 108-112.
PDF [ 301 K ]( 825 ) HTML
USING STRAKE VORTEX TO REDUCE THE DISTORTION OF A Y SHAPED INLET
HUANG Guo-ping;YANG De-hua;LIANG De-wang;LI Bo
2000, (2): 113-117.
PDF [ 312 K ]( 726 ) HTML
COMPILATION THEORY OF MEDIAN STOCHASTIC FATIGUE LOAD SPECTRUM WITH HIGH CONFIDENCE LEVEL FOR AIRPLANE
YAN Chu-liang;GAO Zhen-tong
2000, (2): 118-123.
PDF [ 286 K ]( 1165 ) HTML
INFLUENCE OF THE CONSTITUTIVE EQUATIONS ON THE WELL-POSEDNESS OF FUNDAMENTAL EQUATIONS IN CONTINUUM DAMAGE MECHANICS ——THE CASE OF ONE DIMENSION ELASTIC DAMAGE
HUANG Zai-xing
2000, (2): 124-127.
PDF [ 297 K ]( 1021 ) HTML
EQUIVALENT ENVIRONMENT SPECTRUM RESEARCH OF DETERMINING CALENDAR LIFE FOR AIRCRAFT
ZHANG Dong
2000, (2): 128-133.
PDF [ 349 K ]( 632 ) HTML
STUDY ON MULTITASK MANAGEMENT UNIT MTU OF EMBEDDED MICROPROCESSOR NCS
LI Shu-guo;GAO De-yuan;NIE Pei-qin
2000, (2): 134-137.
PDF [ 259 K ]( 655 ) HTML
DESIGN AND REALIZATION OF AIRBORNE PD TRACKING RADAR SIGNAL PROCESSOR
ZENG Tao;LONG Teng
2000, (2): 138-141.
PDF [ 276 K ]( 684 ) HTML
ATTITUDE CONTROL SYSTEM DESIGN FOR SMALL SATELLITE EARTH ACQUISITION WITH ACTIVE MAGNETIC CONTROL
GENG Yun-hai;CUI Hu-tao;SUN Zhao-wei;YANG Di
2000, (2): 142-145.
PDF [ 301 K ]( 882 ) HTML
A CENTRALIZED COORDINATED PATH PLANNING METHOD BASED ON GENETIC ALGORITHM FOR MULTIPLE MODILE ROBOTS
ZHOU Ming;SUN Shu-dong;PENG Yan-wu
2000, (2): 146-149.
PDF [ 200 K ]( 833 ) HTML
ADAPTIVE CONTROL OF SPACE-BASED MANIPULATOR WITH UNCERTAIN PARAMETERS
CHEN Li;LIU Yan-zhu
2000, (2): 150-154.
PDF [ 311 K ]( 636 ) HTML
INTEGRAL INFERENCE METHOD FOR THE BINOMIAL DISTRIBUTION PARAMETER
FU Hui-min
2000, (2): 155-158.
PDF [ 195 K ]( 872 ) HTML
MODELING OF PIEZOELECTRIC THIN PLATES AND QUASI INDEPENDENT MODAL CONTROL FOR DAMPING
YAO Jun;LI Yue-feng;LIU Juan
2000, (2): 159-163.
PDF [ 170 K ]( 652 ) HTML
CONVERSION METHOD OF EQUIVALENT LOAD FOR PRE-FATIGUE TEST OF No.58 TITANIUM FRAME
WANG Xiang-ming;ZHANG Yi-ning
2000, (2): 164-166.
PDF [ 119 K ]( 512 ) HTML
ACTIVE CONSTRAINED LAYER DAMPING TREATMENT OF SUPPORTER
TIAN Xiao-geng;SHEN Ya-peng;ZHANG Yuan-chong
2000, (2): 167-170.
PDF [ 271 K ]( 486 ) HTML
STUDY ON CYCLIC STRESS-STRAIN BEHAVIOR AND CYCLIC STRAIN-LIFE RELATION OF MATERIALS
WANG Bin-tuan;YANG Qing-xiong
2000, (2): 171-174.
PDF [ 265 K ]( 2778 ) HTML
ROBUST H∞ CONTROLLER DESIGN FOR AERO ENGINE BASED ON LMI
XIE Guang-hua;ZENG Qing-fu
2000, (2): 175-178.
PDF [ 158 K ]( 710 ) HTML
VISUALIZATION AND ANIMATION OF CFD RESULTS
FAN Yan-bin;MENG Guang;SHEN Zi-lin;YANG Peng-ji
2000, (2): 179-182.
PDF [ 280 K ]( 719 ) HTML
STUDY OF MATHEMATICAL MODELS IN MATERIAL CORROSION PREDICTION
CHENG Ji-wei;ZHANG Qi
2000, (2): 183-186.
PDF [ 203 K ]( 893 ) HTML
FACE CONFIGURATION WITH HIGH PERFORMANCE FOR GAS FILM FACE SEAL
LIU Yu-chuan;XU Wan-fu;CHEN Guo-lin;SHEN Xin-min
2000, (2): 187-190.
PDF [ 286 K ]( 875 ) HTML
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