Acta Aeronautica ET Astronautica Sinica 2000 Issue 3 fa dong ji ruan ke xue xue shu tao lun hui wei fa zhan wo guo hang kong dong li shi ye xian ji xian ce

fa dong ji ruan ke xue xue shu tao lun hui wei fa zhan wo guo hang kong dong li shi ye xian ji xian ce

..............page:261

zhong guo hang kong xue hui 2000 nian du xue shu huo dong an pai

..............page:225,229,237,240,269

zhong guo hang kong xue hui tui jian cui er jie tao bao zuo he chen yi jian chen mao zhang zhong qun peng fen bie ru xuan zhong ke yuan he gong cheng yuan yuan shi

..............page:266

dong li zhuan ye fen hui 1999 nian xue shu huo dong

..............page:213

THERMAL STRESSES ANALYSIS AND OPTIMIZATION OF SUBSTRATE/FUNCTIONAL GRADED COATING STRUCTURE
WANG Bao-lin;Han Jie-cai;Du Shan-yi

..............page:286-288

REPAIRS OF COMPOSITE LAMINATES WITH LOW VELOCITY IMPACT DAMAGE
CHENG Xiao-quan;KOU Chang-he;LI Zheng-neng

..............page:282-285

ALGORITHM OF GRAPHIC-BASED BEST FIT ANALYSIS BETWEEN TWO COMPLEX SURFACES
CHEN Zhi-yang;LI Jiang-xiong;KE Ying-lin

..............page:279-281

STUDY ON COMPUTER-AIDED RELIABILITY DESIGN AND ANALYSIS SYSTEM
ZHAO Ting-di;ZENG Sheng-kui;KANG Rui

..............page:206-209

INFLUENCE ANALYSIS AND CALCULATION OF CHAFF CORRIDOR ON THE STEALTH PERFORMANCE OF AIRCRAFT
ZHANG Yun-fei;ZHANG Kao;HE Qing-zhi

..............page:202-205

ACCELERATED CORROSION TEST OF THE AIRCRAFT STRUCTURE UNDER EQUIVALENT ENVIRONMENT SPECTRUM AND THE COMPUTING METHOD FOR THE CALENDAR LIFE
ZHANG Dong

..............page:196-201

NUMERICAL SIMULATION OF TWO PHASE FLOW WITHIN PASSIVE EJECTORS
YANG Juan;HE Hong-qing;MAO Gen-wang

..............page:193-195

SPEED-SENSORLESS DIRECT TORQUE CONTROL SYSTEM OF AN INDUCTION MOTOR
CHEN Bao-lin;HU Yu-wen

..............page:277-278

EIGENVALUE-DECOMPOSITION-BASED ADAPTIVE INFORMATION FUSION FILTER ALGORITHM FOR INTEGRATED NAVIGATION SYSTEMS
WANG Yu-fei;HUANG Xian-lin;HU Heng-zhang

..............page:274-276

ON THE INTERACTIVE TECHNOLOGY IN AIR COMBAT SIMULATION
JING Tong;KANG Ji-chang;TONG Ming-an

..............page:270-273

APPLICATION OF NORMALIZED LCF H∞ METHOE IN FLIGHT/PROPULSEON CONTROLLER DESIGN
ZHANG Li-jun;XIAO Ying-yue;CHENG Peng

..............page:267-269

EXPLORATION OF THE FATIGUE REMAINING LIFE BASED ON AN EQUIVALENT AVERAGE DAMAGE MODE
HU Ming-min

..............page:262-266

STATISTICAL ANALYSIS TO RANDOM PROCESS OF FATIGUE CRACK PROPAGATION
ZHANG Jian-yu;ZHAO Li-bin;FEI Bin-jun

..............page:258-261

NEW COUNT METHOD BASED ON UPDATED COEFFICIENT MATRIX OF EFFICIENCY
MA Jun-feng;Lu Guo-zhi

..............page:254-257

CONTROLLING METHOD FOR AIRCRAFT FLAW PROBABILITY OF MISSING
LIU Deng-di;FU Hui-min

..............page:251-253

ACTIVE VIBRATION CONTROL OF COMPOSITE PLATE WITH SELF-SENSING PIEZOELECTRIC ACTUATORS
FANG You-liang;WU Zhe

..............page:247-250

RELIABILITY NALYSIS ETHOD F TOCHASTIC TRUCTURES
ZHAN Jian-guo

..............page:244-246

STUDY ON REDUCTION OF RCS BY COATING RADAR ABSORBING MATERIAL FOR METAL WINGS
MA Dong-li;WU Zhe

..............page:241-243

APPLICATION OF MULTIBLOCK/MULTIGRID METHOD TO INLET PARTICLE SEPARATOR IN HELICOPTER
HOU Ling-yun;YAN Chuan-jun

..............page:238-240

APPLICATION OF FUZZY LOGIC CONTROL IN POST-STALL MANEUVERS
YIN Jiang-hui;ZHOU Na;LIU Chang

..............page:234-237

APPLICATION OF H∞ CONTROL THEORY TO FLIGHT DYNAMICS PROBLEMS
FAN Zi-qiang;FANG Zhen-ping

..............page:230-233

FLOW FIELD CONTROL ON THE SUBMERGED INLET
REN San-xing;LI Xue-lai;GUO Rong-wei

..............page:226-229

MODELING FOR EVALUATING THE PROCESS ABILITY OF CASTING STRUCTURE
WANG Gui;YANG Li;ZHOU Tie-tao

..............page:222-225

STUDY ON MECHANISM FOR PMEB TO PRODUCE MAGNETIC SUSPENSION FORCE
ZENG Li;WANG Tong-yue;XU Long-xiang;LIU Zheng-xun

..............page:219-221

COMBINED METHOD TO DESIGN BLOCK DIAGONAL CONTROLLER OF MISSILE
HU Yun-an;WU Guang-bin;GU Wen-jin

..............page:214-218

EVALUATION OF LINK OPERATION MODES ON AIR-GROUND VHF DATA LINK
ZHANG Jun;ZHANG Qi-shan;FANG Xin;ZHU Yan-bo

..............page:210-213