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ADVANCES IN THE DEVELOPMENT OF STRAIN ACTUATORS FOR ADAPTIVE ROTOR
Xiong Ke;Tao Baoqi;Chen Renwen;Liu Guo
1997, (6): 641-647.
PDF [ 376 K ]( 10304 ) HTML
AERODYNAMIC INVERSE DESIGN METHOD OF AIRFOIL VIA CFD
Zhao Xiaohu;Yan Chao
1997, (6): 648-651.
PDF [ 266 K ]( 884 ) HTML
UNSTEADY WIND TUNNEL WALL PRESSURE RESEARCH
Li Zhiqiang;Zhang Wenhua;Huang Da;Ding Kewen
1997, (6): 652-655.
PDF [ 246 K ]( 596 ) HTML
INTEGRATED OPTIMUM DESIGN OF WING STRUCTURES WITH COMPOSITE SKINS
Zhang Yining;Yang Xu
1997, (6): 656-660.
PDF [ 281 K ]( 732 ) HTML
GROUND THERMAL SCALE MODELING OF CONDUCTION CONVECTION RADIATION SYSTEMS IN MICRO GRAVITY ENVIRONMENT
Liu Yunlong;Liang Xingang;Qu Weilin;Ren Jianxun;Guo Zengyuan
1997, (6): 661-665.
PDF [ 177 K ]( 706 ) HTML
EFFECTS OF FABRIC MICRO STRUCTURAL PARAMETERS ON ELASTIC PROPERTIES OF WOVEN FABRIC REINFORCED COMPOSITES
Yan Ying
1997, (6): 666-669.
PDF [ 236 K ]( 704 ) HTML
PASSIVE DAMPING DESIGN FOR FRAME STRUCTURE BASED ON TRAVELLING WAVE MODEL
Zhu Guidong;Zheng Gangtie;Shao Chengxun
1997, (6): 670-675.
PDF [ 334 K ]( 506 ) HTML
PERFORMANCE ANALYSIS AND COMPARISON OF AS4074 AND PAVE PILLAR HSDB
Xiong Huagang;Luo Zhiqiang;Zhang Qishan
1997, (6): 676-680.
PDF [ 215 K ]( 896 ) HTML
TWO TARGET DETECTION AND LOCALIZATION METHODS BASED ON GENETIC ALGORITHMS
Hou Gexian;Wu Chengke
1997, (6): 681-686.
PDF [ 378 K ]( 551 ) HTML
STUDY ON HYBRID KINEMATIC ANALYSES OF FORCE AND POSITION PARALLEL LOOP FOR ROBOT
Yin Yuehong;Zhu Jianying;Wei Zhongxin
1997, (6): 687-692.
PDF [ 360 K ]( 857 ) HTML
DETECTION AND ISOLATION OF CONTROL SURFACE EFFECTIVENESS FAILURES
Li Qing;Shen Chunlin;Guo Suofeng
1997, (6): 693-697.
PDF [ 284 K ]( 715 ) HTML
FUZZY PROCESS IN QUALITY FUNCTION DEPLOYMENT SYSTEM
Ma Jian;Tang Xiaoqing;Li Jun
1997, (6): 698-702.
PDF [ 212 K ]( 402 ) HTML
FEM ANALYSIS OF MANUFACTURING ERROR EFFECTS ON THE STATIC CHARACTERISTICS OF AEROSTATIC JOURNAL BEARING
Wu Qi;Chi Changqing;Wang Zhishan
1997, (6): 703-708.
PDF [ 298 K ]( 842 ) HTML
AERODYNAMIC FORCES AND BLADE FLAPPING MOTION OF A ROTOR IN FORWARD FLIGHT WITH GROUND EFFECTS
Kang Ning;Sun Mao
1997, (6): 709-711.
PDF [ 173 K ]( 854 ) HTML
ATTITUDE IDENTIFICATION OF SPACECRAFT
Yuan Ping;Gou Xingyu;Wu Zhifeng
1997, (6): 712-715.
PDF [ 192 K ]( 680 ) HTML
NEW WAY TO THE STUDY OF HIGH ORDER SCHEMES IN FEM
Duan Zhanyuan;Tong Binggang;Jiang Guiqing
1997, (6): 716-719.
PDF [ 272 K ]( 1066 ) HTML
ACTIVE VIBRATION CONTROL OF FLEXIBLE STRUCTURE USING PIEZOELECTRIC SENSOR/ACTUATOR
Tao Yungang;Zhou Jiemin;Lu Xiaobo;He Yanwei
1997, (6): 720-724.
PDF [ 312 K ]( 973 ) HTML
STUDY OF THE AUTOMATIC CALCULATION METHOD FOR THE WINGLIKE STRUCTURE MASS DISTRIBUTION OF AIRCRAFT
Wang Heping; Song Minxin
1997, (6): 725-727.
PDF [ 190 K ]( 497 ) HTML
ESTIMATION OF FRACTURE TOUGHNESS BY FATIGUE CRACK GROWTH RATE
Wang Yonglian
1997, (6): 728-731.
PDF [ 258 K ]( 854 ) HTML
RELIABILITY MATHEMATICS MODEL OF AEROSPACE ELECTRICAL CONNECTOR
Chen Wenhua;Cheng Yaodong; Li Pingzhen;Lu Xianbiao
1997, (6): 732-734.
PDF [ 217 K ]( 1217 ) HTML
IMPROVEMENT OF LEVY METHOD
Gu Qitai;Liu Xuebin
1997, (6): 735-738.
PDF [ 241 K ]( 706 ) HTML
PERFORMANCE ANALYSIS OF APD OPTICAL RECEIVER FOR AIRBORNE WIDE TEMPERATURE ENVIRONMENT
Yang Wenge;Li Zheng
1997, (6): 739-742.
PDF [ 245 K ]( 534 ) HTML
STUDIES ON THE ALGORITHM FOR 5 AXIS MILLING OF INTERSECTION CURVE OF SCULPTURED SURFACES
Wang Qinghui;Liao Wenhe;Zhou Rurong
1997, (6): 743-746.
PDF [ 259 K ]( 570 ) HTML
STUDY ON REACTIVE MECHANISM OF XD METHOD FOR SYNTHESIZING NiAl MATRIX IN SITU COMPOSITES
Lu Yuxiang;Yang Dezhuang;Tao Chunhu;Chen Lin;Xie Mingli
1997, (6): 747-751.
PDF [ 236 K ]( 526 ) HTML
ANALYSES OF FACTORS AFFECTING EKMAN FLOW DURING ACRT PROCESS
Liu Juncheng;Guo Xiping;Liu Xiaohua;Jie Wanqi;Zhou Yaohe
1997, (6): 752-754.
PDF [ 220 K ]( 548 ) HTML
GRINDING CHARACTERISTIC OF NICKEL BASED SUPERALLOY
Ren Jingxin;Yang Maokui;Li Yaqing;Wu Xiaoling
1997, (6): 755-758.
PDF [ 178 K ]( 700 ) HTML
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