Acta Aeronautica ET Astronautica Sinica 1998 Issue 4 hang kong xue bao jia ru zhong guo ke ji qi kan ( guang pan ban ) shen ming

hang kong xue bao jia ru zhong guo ke ji qi kan ( guang pan ban ) shen ming

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guan yu chu ban hang kong ji chu ke xue ji jin lun wen zhuan ji de shen ming

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di si jie xian jin cai liao ji shu yan tao hui zai jiu jiang zhao kai
li tie bai

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'97 gu ti huo jian tui jin xue shu yan tao hui zai kun ming zhao kai
li tie bai

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zhong guo hang kong xue hui zong ti zhuan ye fen hui di si ci xue shu jiao liu hui zuo huan jie hui yi zai cheng du zhao kai
li tie bai

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di jiu jie quan guo duan lie pi lao xue shu hui yi zheng wen
li tie bai

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DESIGN-ORIENTED FINITE ELEMENT MODELLING TO AERONAUTICAL STRUCTURES
Sun Xiasheng;ChenWenpu;Chen Huanxing

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MEASUREMENT AND ANALYSIS OF THE FREQUENCY RESPONSE CHARACTERISTICS OF A SONIC TRAVELLING WAVE SYSTEM
Dong Xiaowei;Ding Aixiang

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FLUTTER RELIABILITY ANALYSIS OF WING STRUCTURE
Liu Yingwei;Chen Kuilin;Zheng Dongqing

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RESEARCH ON MULTIPLE-BOLTED COMPOSITE JOINT BY FINITE ELEMENT ANALYSIS
Chi Jian;Xie Mingjiu

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VIBRATION ISOLATOR WITH HIGH DAMPING USED IN AIRCRAFT
Yao Qihang;Ge Zude;Pan Shuxiang

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INVESTIGATION AND DEVELOPMENT OF MAIN LOAD-BEARING JOINTS IN COMPOSITES FOR AIRCRAFT STRUCTURES
Shi Jianzhong;Huang Weiyang

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STUDY ON CRACK INSPECTION PROBABILITY BY USING EDDY CURRENT UNDER DIFFERENT THICKNESS COVER LAYERS
Liu Xiuli;Huang Huabin

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IN-FLIGHT MEASUREMENT OF STATIC PRESSURE ON A SUBSONIC TRANSPORT AIRCRAFT
Yuan Zhengting

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SOME EFFECTS ON FATIGUE PROPERTIES UNDER PROTECTION/UNPROTECTION COATING SYSTEMS
Liu Yiming;Jiang Junliang;Shan Yongshou

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FIGHTER LOAD SPECTRA DERIVATION USING EVALUATION AND VALIDATION FLIGHT TEST DATA
Sun Shutian;Yang Jianzhong

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EVALUATION APPROACH TO INITIAL FATIGUE QUALITY OF FASTENER HOLE
Wang Zhizhi;Wang Puxuan;Nie Xuezhou

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FINITE ELEMENT ANALYSES (FEA) OF CRITICAL SITES AND SIF OF SYMMETRIC AND NON-SYMMETRIC TAPERED LUGS
Huang Qiqing

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EFFECTS OF WET/HOT SPECTRUM AGING ON STRENGTH OF COMPOSITE LAMINATES
Zheng Xitao;Li Ye;Liu Haiyan;Guo Wenxue

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EXPERIMENT STUDY ON THE DYNAMIC CHARACTERS AND VIBRATION CONTROL OF A SANDWICH PLATE WITH ELECTRORHEOLOGICAL FLUID
Meng Guang;Lu Hongquan;Ren Xingming

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EQUIVALENT ENVIRONMENT SPECTRUM RESEARCH ON SERVICE CALENDAR TIME FOR FIGHTER AIRCRAFT
Dong Dengke;Wang Junyang

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FINITE ELEMENT METHOD NUMERICAL SIMULATION OF BIRD STRIKING MULTILAYER WINDSHIELD
Wang Aijun;Qiao Xin;Li Lei

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MODAL TRANSFORMATION OF A STRUCTURE
Gu Songnian;Jiang Jiesheng;Yao Qihang

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STUDY ON ACCELERATED CORROSION TEST ENVIRONMENT SPECTRUMFOR CRITICAL AREA
Jiang Dongbin

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CONSISTENCY EVALUATION OF THE STRUCTURAL TEST AND ANALYSIS
Duan Shihui;Hao Fengqin;Huang Jiahuang

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CALCULATION OF DYNAMIC LOADS FOR RIPPLE EJECTION AND UNSYMMETRICAL EJECTION OF EXTERNAL STORE
Zheng Chengxing;Wei Lixin;Xiao Xiaoling

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TEST BASED FEM MODELING AND MODIFICATION
Cai Yanzhong;Duan Shihui

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INVESTIGATION OF CORROSION EQUIVALENT RELATIONSHIPS BETWEEN THE ACCELERATED ENVIRONMENT AND THE TYPICAL SERVICE ENVIRONMENTS OF AIRCRAFT STRUCTURES
Chen Qunzhi;Li Ximing;Zhou Xiyuan;Wang Yingli;Wu Zhen;Liu Wenting;Xu Xiaofei

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RESEARCH ON CCD IMAGE PROCESSING TECHNOLOGY OF FATIGUE SECTION FOR STRUCTURE DURABILITY ANALYSIS
Wu Dafang;Tao Tao;He Xiaofan

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RESEARCH ON VIBRATION ENVIRONMENT TEST TECHNOLOGY OF AIRCRAFT STRUCTURE COMBINED WITH FATIGUE OR STATIC LOAD
Cao Qi;Shao Chuang;Yao Qihang

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PROMOTION OF ELECTRONIC DAMPING BY MEANS OF LOCAL STRAIN COMPENSATION
Yao Jun;Li Yuefeng;Zhu Demao;Yao Qihang;Liu Juan

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DESIGN ALLOWABLES OF COMPOSITE AIRCRAFT STRUCTURES AND THEIR DETERMINATION PRINCIPLES
Shen Zhen

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COMPARISON OF RESULTS OBTAINED BY THREE KINDS OF IMPLICIT TIME INTEGRATION METHODS FOR ELASTIC STRUCTURAL IMPACT
Zhu Dechao;Li Ming

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