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NUMERICAL SIMULATION OF TWO PHASE FLOW WITHIN PASSIVE EJECTORS
YANG Juan;HE Hong-qing;MAO Gen-wang
2000, (3): 193-195.
PDF [ 253 K ]( 697 ) HTML
ACCELERATED CORROSION TEST OF THE AIRCRAFT STRUCTURE UNDER EQUIVALENT ENVIRONMENT SPECTRUM AND THE COMPUTING METHOD FOR THE CALENDAR LIFE
ZHANG Dong
2000, (3): 196-201.
PDF [ 242 K ]( 661 ) HTML
INFLUENCE ANALYSIS AND CALCULATION OF CHAFF CORRIDOR ON THE STEALTH PERFORMANCE OF AIRCRAFT
ZHANG Yun-fei;ZHANG Kao;HE Qing-zhi
2000, (3): 202-205.
PDF [ 281 K ]( 796 ) HTML
STUDY ON COMPUTER AIDED RELIABILITY DESIGN AND ANALYSIS SYSTEM
ZHAO Ting-di;ZENG Sheng-kui;KANG Rui
2000, (3): 206-209.
PDF [ 257 K ]( 733 ) HTML
EVALUATION OF LINK OPERATION MODES ON AIR GROUND VHF DATA LINK
ZHANG Jun;ZHANG Qi-shan;FANG Xin;ZHU Yan-bo
2000, (3): 210-213.
PDF [ 281 K ]( 863 ) HTML
COMBINED METHOD TO DESIGN BLOCK DIAGONAL CONTROLLER OF MISSILE
HU Yun-an;WU Guang-bin;GU Wen-jin
2000, (3): 214-218.
PDF [ 328 K ]( 721 ) HTML
STUDY ON MECHANISM FOR PMEB TO PRODUCE MAGNETIC SUSPENSION FORCE
ZENG Li;WANG Tong-yue;XU Long-xiang;LIU Zheng-xun
2000, (3): 219-221.
PDF [ 216 K ]( 1454 ) HTML
MODELING FOR EVALUATING THE PROCESS ABILITY OF CASTING STRUCTURE
WANG Gui;YANG Li;ZHOU Tie-tao
2000, (3): 222-225.
PDF [ 218 K ]( 941 ) HTML
FLOW FIELD CONTROL ON THE SUBMERGED INLET
REN San-xing;LI Xue-lai;GUO Rong-wei
2000, (3): 226-229.
PDF [ 341 K ]( 700 ) HTML
APPLICATION OF H_∞ CONTROL THEORY TO FLIGHT DYNAMICS PROBLEMS
FAN Zi-qiang;FANG Zhen-ping
2000, (3): 230-233.
PDF [ 283 K ]( 608 ) HTML
APPLICATION OF FUZZY LOGIC CONTROL IN POST STALL MANEUVERS
YIN Jiang-hui;ZHOU Na;LIU Chang
2000, (3): 234-237.
PDF [ 286 K ]( 574 ) HTML
APPLICATION OF MULTIBLOCK/MULTIGRID METHOD TO INLET PARTICLE SEPARATOR IN HELICOPTER
HOU Ling-yun;YAN Chuan-jun
2000, (3): 238-240.
PDF [ 182 K ]( 726 ) HTML
STUDY ON REDUCTION OF RCS BY COATING RADAR ABSORBING MATERIAL FOR METAL WINGS
MA Dong-li;WU Zhe
2000, (3): 241-243.
PDF [ 252 K ]( 1025 ) HTML
RELIABILITY ANALYSIS METHOD OF STOCHASTIC STRUCTURES
ZHANG Jian-guo
2000, (3): 244-246.
PDF [ 297 K ]( 746 ) HTML
ACTIVE VIBRATION CONTROL OF COMPOSITE PLATE WITH SELF-SENSINGPIEZOELECTRIC ACTUATORS
FANG You-liang;WU Zhe
2000, (3): 247-250.
PDF [ 320 K ]( 455 ) HTML
CONTROLLING METHOD FOR AIRCRAFT FLAW PROBABILITY OF MISSING
LIU Deng-di;FU Hui-min
2000, (3): 251-253.
PDF [ 184 K ]( 737 ) HTML
NEW COUNT METHOD BASED ON UPDATED COEFFICIENT MATRIX OF EFFICIENCY
MA Jun-feng;LÜ Guo-zhi
2000, (3): 254-257.
PDF [ 281 K ]( 467 ) HTML
STATISTICAL ANALYSIS TO RANDOM PROCESS OF FATIGUE CRACK PROPAGATION
ZHANG Jian-yu;ZHAO-Li-bin;FEI Bin-jun
2000, (3): 258-261.
PDF [ 278 K ]( 869 ) HTML
EXPLORATION OF THE FATIGUE REMAINING LIFE BASED ON AN EQUIVALENT AVERAGE DAMAGE MODE
HU Ming-min
2000, (3): 262-266.
PDF [ 232 K ]( 866 ) HTML
APPLICATION OF NORMALIZED LCF H∞ METHOE IN FLIGHT/PROPULSEON CONTROLLER DESIGN
ZHANG Li-jun;XIAO Ying-yue;CHENG Peng
2000, (3): 267-269.
PDF [ 256 K ]( 967 ) HTML
ON THE INTERACTIVE TECHNOLOGY IN AIR COMBAT SIMULATION
JING Tong;KANG Ji-chang;TONG Ming-an
2000, (3): 270-273.
PDF [ 263 K ]( 464 ) HTML
EIGENVALUE DECOMPOSITION BASED ADAPTIVE INFORMATION FUSION FILTER ALGORITHM FOR INTEGRATED NAVIGATION SYSTEMS
WANG Yu-fei;HUANG Xian-lin;HU Heng-zhang
2000, (3): 274-276.
PDF [ 251 K ]( 537 ) HTML
SPEED-SENSORLESS DIRECT TORQUE CONTROL SYSTEM OF AN INDUCTION MOTOR
CHEN Bao-lin;HU Yu-wen
2000, (3): 277-278.
PDF [ 216 K ]( 582 ) HTML
ALGORITHM OF GRAPHIC BASED BEST FIT ANALYSIS BETWEEN TWO COMPLEX SURFACES
CHEN Zhi-yang;LI Jiang-xiong;KE Ying-lin
2000, (3): 279-281.
PDF [ 257 K ]( 681 ) HTML
REPAIRS OF COMPOSITE LAMINATES WITH LOW VELOCITY IMPACT DAMAGE
CHENG Xiao-quan;KOU Chang-he;LI Zheng-neng
2000, (3): 282-285.
PDF [ 284 K ]( 1084 ) HTML
THERMAL STRESSES ANALYSIS AND OPTIMIZATION OF SUBSTRATE/FUNCTIONAL GRADED COATING STRUCTURE
WANG Bao-lin;Han Jie-cai;Du Shan-yi
2000, (3): 286-288.
PDF [ 237 K ]( 709 ) HTML
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