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MULTIDISCIPLINARY DESIGN OPTIMIZATION A SURVEY OF ITS ALGORITHMS AND APPLICATIONS TO AIRCRAFT DESIGN
YU Xiongqing;DING Yunliang
2000, (1): 1-6.
PDF [ 209 K ]( 1534 ) HTML
RECENT DEVELOPMENT IN MATERIALS DESIGN OF THERMAL BARRIER COATINGS FOR GAS TURBINE
XU Huibin;GONG Shengkai;LIU Fushun
2000, (1): 7-12.
PDF [ 427 K ]( 3348 ) HTML
NUMERICAL RESEARCH ON COHERENT STRUCTURES IN A MIXING LAYER WITH CROSS-SHEAR
LIN Jianzhong;SHAO Xueming;YU Zhaosheng
2000, (1): 13-20.
PDF [ 543 K ]( 391 ) HTML
INFLUENCE OF NONLINEAR CONTROL SYSTEM ON AIRCRAFT LONGITUDINAL PILOT INDUCED OSCILLATION
GAO Qing yu;FANG Zhen ping
2000, (1): 21-24.
PDF [ 279 K ]( 756 ) HTML
COMPRESSIVE BUCKLING FAILURE OF LAMINATES WITH A SURFACE NOTCH
HU Zili
2000, (1): 25-29.
PDF [ 190 K ]( 619 ) HTML
RESEARCHING AND ACCOMPLISHING FOR HOMING MISSILE ATTACKING MANEUVERING TARGET
WANG Xiao hu;ZHANG Ming lian
2000, (1): 30-33.
PDF [ 283 K ]( 845 ) HTML
APPLICATION OF DYNAMIC FAULT TREE ANALYSIS TO SOFTWARE AND HARDWARE FAULT TOLERANT CONTROL COMPUTER SYSTEMS
CHENG Ming hua;YAO Yi ping
2000, (1): 34-37.
PDF [ 162 K ]( 790 ) HTML
STUDY ON COST CONTROL OF MODERN AIRPLANE MANUFACTURING
WEI Fa jie;ZHANG Ren qian;WANG Dan
2000, (1): 38-42,47.
PDF [ 304 K ]( 1297 ) HTML
REPRESENTATION SCHEME OF PRODUCT MODELS FOR CONCURRENT CAD/CAM INTEGRATION
HE Xiaozhao;SHEN Mei;ZHANG Tiechang
2000, (1): 43-47.
PDF [ 293 K ]( 608 ) HTML
INVESTIGATION OF HELICOPTER ROTOR AEROACOUSTICS FOR DIFFERENT TIP SHAPES
WANG Liqun;SONG Wenping
2000, (1): 48-51.
PDF [ 331 K ]( 811 ) HTML
INVESTIGATION ON MODEL DYNAMIC STABILITY DERIVATIVES TEST TECHNIQUES IN TRANS-, SUPERS-, HYPERSONIC WIND TUNNELS
ZHAO Zhongliang;REN Bin;HUANG Xuhui;YU Li
2000, (1): 52-55.
PDF [ 300 K ]( 581 ) HTML
MECHANICAL MODEL AND DATA PROCESSING OF LOAD MEASUREMENT TEST FOR THE AIRPLANE’S WING STRUCTURE
YAN Chu liang;ZHANG Shu ming;ZHUO Ning sheng;GAO Zhen tong
2000, (1): 56-59.
PDF [ 270 K ]( 776 ) HTML
MIMO REAL-TIME IDENTIFICATION CONTROL AND EXPERIMENT OF VIBRATIONAL STRUCTURES
MA Kougen;GU Zhongquan
2000, (1): 60-63.
PDF [ 282 K ]( 546 ) HTML
RESEARCH ON RAPID REPAIR OF BATTLE\|DAMAGED INTEGRAL PANEL OF AIRCRAFT
JIAO Liang;ZHANG Jianhua
2000, (1): 64-66.
PDF [ 227 K ]( 438 ) HTML
ACCURATE ALGORITHM OF SAMPLING PLAN & ITS APPLICATION IN TESTABILITY DEMONSTRATION
XU Zhongwei;ZHOU Yufen;XU Songtao;GAO Xijun
2000, (1): 67-69.
PDF [ 193 K ]( 749 ) HTML
STUDY ON EVALUATION CRITERIA AND ASSESSMENT METHODOLOGY FOR CONCEPTUAL/PRELIMINARY DESIGN OF COMBAT AIRCRAFT
HUANG Jun;WU Zhe;SUN Huizhong;WU Binglin
2000, (1): 70-73.
PDF [ 290 K ]( 824 ) HTML
RESIDUAL STRENGTH MODEL OF ELEMENTS’ FATIGUE RELIABILITY EVALUATION
LU Haibo;YAO Weixing Haibo;YAO Weixing
2000, (1): 74-77.
PDF [ 277 K ]( 1395 ) HTML
MAGNETIC DEVIATION COMPENSATION FOR UAV’S HEADING MEASUREMENT
LIU Shibin;YAN Jiaming;SUN Xiren
2000, (1): 78-80.
PDF [ 191 K ]( 921 ) HTML
DETECTING DIM POINT TARGETS IN IMAGE WITH GENETIC ALGORITHM
LI Hongyan;WU Chengke
2000, (1): 81-83.
PDF [ 120 K ]( 429 ) HTML
NEURAL NETWORKS BASED ADAPTIVE FEEDBACK LINEARIZATION FOR BANK-TO-TURN MISSILE CONTROL
ZHANG Youan;YANG Xu;CUI Pingyuan;YANG Di
2000, (1): 84-86.
PDF [ 200 K ]( 793 ) HTML
CYCLIC OXIDATION BEHAVIOR OF TiAl AND SURFACE MODIFICATION
ZHOU Chungen;XU Huibin;GONG Shengkai;LIU Fushun
2000, (1): 87-89.
PDF [ 176 K ]( 542 ) HTML
STUDY ON THE POWER SUPPLIES OF FLEXIBLE MICRO ACTUATORS WITH ELECTRO RHEOLOGICAL FLUID
WU Zhong;YUAN Weizheng;PENG Yanwu
2000, (1): 91-93.
PDF [ 198 K ]( 404 ) HTML
ARTIFICIAL NEURAL NETWORKS APPLIED TO THE QUALITY CONTROL IN ALTERNATING CURRENT RESISTANCE SPOT WELDING
FANG Ping;TAN Yiming;WU Lu;ZHANG Yong
2000, (1): 94-95，86.
PDF [ 140 K ]( 772 ) HTML
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