1000-6893
1988 Issue S1
THE APPLICATION AND DEVELOPMENT OF FRACTURE MECHANICS IN CHINESE AEROSPACE INDUSTRY
Ministry of Aeronautics and Astronautics Gu WeihaoBeijing Institute of Aeronautic Materials Liu Caimu
Ministry of Aeronautics and Astronautics Gu WeihaoBeijing Institute of Aeronautic Materials Liu Caimu
..............page:1-4
A GENERALIZED VARIATIONAL METHOD FOR SOLVING STRESS INTENSITY FACTORS AT CRACKS ON THE EDGE OF HOLES IN ORTHOTROPIC PLATES
Beijing University of Aeronautics and AstronauticsCui Deyu Gu Pei Zhang Xing Imperial College;London;U.K. Davies.G.A.O.
Beijing University of Aeronautics and AstronauticsCui Deyu Gu Pei Zhang Xing Imperial College;London;U.K. Davies.G.A.O.
..............page:5-16
RESIDUAL LIFE ANALYSIS OF THE SKIM PANEL OF AH-24 WING INTEGRAL TANK WITH CRACKS
Civil Aeronautical Institute of China Du Hongzeng Tian Xinyun Yu Huaidong
Civil Aeronautical Institute of China Du Hongzeng Tian Xinyun Yu Huaidong
..............page:17-22
NUMERICAL AND EXPERIMENTAL STUDIES ON THE STRESS CONCENTRATION OF COMPOSITE LAMINATES WITH A HOLE
Beijing University of Aeronautics and Astronautics Yang Bingxiaa
Beijing University of Aeronautics and Astronautics Yang Bingxiaa
..............page:23-28
THE CONFIDENCE LEVEL OF FATIGUE STRENGTH
Beijing University of Aeronautics and Astronautics Fu Huimin Gao Zhentong
Beijing University of Aeronautics and Astronautics Fu Huimin Gao Zhentong
..............page:29-35
ELASTO-PLASTIC STRESS-STRAIN ANALYSIS OF HOLED PLATE UNDER CYCLIC LOADINGS
Northwestern Poly technical University Jiang Jinqing Yang Qingxiong
Northwestern Poly technical University Jiang Jinqing Yang Qingxiong
..............page:36-42
THE EFFECT OF FRETTING ON FATIGUE STRENGTH FOR TYPICAL JOINTS OF ALUMINUM ALLOY SHEETS
Institute of Metal Research;Academia Sinica Dong Xianglin Shenyang Aircraft Company Tian Tiezhong
Institute of Metal Research;Academia Sinica Dong Xianglin Shenyang Aircraft Company Tian Tiezhong
..............page:43-48
THE ANALYSIS OF ACCURACY OF BOUNDARY ELEMENT TECHNIQUE IN SURFACE CRACK PROBLEMS
Northwest Telecommunication Engineering Institute Xie Huicai Yang Qi Wang Deman
Northwest Telecommunication Engineering Institute Xie Huicai Yang Qi Wang Deman
..............page:49-53
A MODIFICATION TO THE FMDF MODEL
Nanjing Electric Power College Wang Yonglian
Nanjing Electric Power College Wang Yonglian
..............page:54-57
STRESS-STRAIN ANALYSIS AND FATIGUE LIFE PREDICTION OF INTERFERENCE JOINTS
Shanghai Aircraft Design and Research Institute Xie Weidong Northwestern Polytcchnical University Wu Fumin Xiao Shouting
Shanghai Aircraft Design and Research Institute Xie Weidong Northwestern Polytcchnical University Wu Fumin Xiao Shouting
..............page:58-64
THE RELIABILITY ANALYSIS FOR THE CRACK GROWTH RESISTANCE CURVE OF THIN PLATES
Beijing University of.Aeronautics and Astronautacs;Liu Wenting Civil Aeronautic Institute of China Gao Jinhua
Beijing University of.Aeronautics and Astronautacs;Liu Wenting Civil Aeronautic Institute of China Gao Jinhua
..............page:65-71
DISTRIBUTION FUNCTION OF TWO-DIMENSIONAL FATIGUE STRENGTH
Beijing University of Aeronautics and Astronautics Fu Huimin Gao Zhentong
Beijing University of Aeronautics and Astronautics Fu Huimin Gao Zhentong
..............page:72-77
SHORT FATIGUE CRACK GROWTH AND PREDICTION OF ENGINEERING CRACK INITIATION LIFE
Beijing University of Aeronautics and Astronautics Jiang Weizni Xu Boqing Shao Aimin Jin Chengmin
Beijing University of Aeronautics and Astronautics Jiang Weizni Xu Boqing Shao Aimin Jin Chengmin
..............page:78-83
APPLICATION OF LOCAL STRAIN METHOD IN FATIGUE LIFE ESTIMATION OF WING JOINT LUGS
Shenyang Aircraft Manufacture Company Liu Shuyuan Jia Guorong
Shenyang Aircraft Manufacture Company Liu Shuyuan Jia Guorong
..............page:84-87
THE PRIMARY STUDlES FOR RANDOM FATIGUE LIFE PREDICTIONS
Tong Ji University Hit Yuren
Tong Ji University Hit Yuren
..............page:88-91
THE EFFECTS OF THE STRESS RATIO AND THE LOADING SEQUENCE ON THE LOCAL STRAIN RANGE
Northwestern Polytechnicai University Zheng Sitao Zheng Xiulin
Northwestern Polytechnicai University Zheng Sitao Zheng Xiulin
..............page:92-94
A METHOD FOR STATISTICALLY PREDICATING CRACK PROPAGATION LIFE
The air force college of engineering Zhang Hengxi
The air force college of engineering Zhang Hengxi
..............page:95-98
FATIGUE ANALYSIS OF STRUCTURAL MEMBERS WITH ELLIPTIC CROSS SECTION
Nanchang Aircraft Manufacture Company Yang Derong
Nanchang Aircraft Manufacture Company Yang Derong
..............page:99-102
AN ENGINEERING APPROACH CALCULATING STRESS INTENSITY FACTOR FOR A SURFACE CRACK
Beijing University of Aeronautics and Astronautics Shen Tao He Qingzhi
Beijing University of Aeronautics and Astronautics Shen Tao He Qingzhi
..............page:103-107
EFFECTS OF OVERLOADING AND OVERLOADING RATIO ON FATIGUE CRACK INITIATION LIFE OF LY12CZ ALLOY
Northwestern poly technical University Lin Chao Zheng Xiulin Zhang Rong
Northwestern poly technical University Lin Chao Zheng Xiulin Zhang Rong
..............page:108-110
ENGINEERING METHOD FOR PREDICTING RESIDUAL STRENGTH OF NOTCHED LAMlNATES UNDER TENSION
Aircraft Structural Strength Research Institute Shen Zhen Liu Junshi
Aircraft Structural Strength Research Institute Shen Zhen Liu Junshi
..............page:111-115
STRUCTURAL SYSTEM RELIABILITY COMBINED WITH THE CONSTRAINT OF DAMAGE TOLERANCE DESIGN
Northwestern polytechnical University Feng Yuansheng
Northwestern polytechnical University Feng Yuansheng
..............page:116-119
AN ESTIMATE OF FATIGUE LIFE OF A STRUCTURE ELEMENT WITH CONSIDERATION OF THE INFLUENCE OF WELDING
Tianjin University Wang Liduan Zhu Lizhang
Tianjin University Wang Liduan Zhu Lizhang
..............page:120-123
..............page:123
THE FATIGUE BEHAVIOUR OF FASTENER HOLES WITHOUT LOAD TRANSFER
Nanjing Aeronautical Institute Wu Shen Wang YongXian Aireraft Aircraft Research Institute Zhang Jianrong
Nanjing Aeronautical Institute Wu Shen Wang YongXian Aireraft Aircraft Research Institute Zhang Jianrong
..............page:124-127
A 2-DIMENSIONAL FINITE ELEMENT STIFFENER MODEL FOR CRACKED SIFFENERS IN A STIFFENED PANEL STRUCTURE
The First Air Force Aeronautical Engineering College Jiao Liang
The First Air Force Aeronautical Engineering College Jiao Liang
..............page:128-130
THE PROCESS AND MECHANISM OF MICRODAMAGE IN FINE GRINDING
Beijing Institute of Aeronautical Materials Ouyang Jie Hou Shue
Beijing Institute of Aeronautical Materials Ouyang Jie Hou Shue
..............page:131-134
FATIGUE LIFE ESTIMATION AND ENERGY CRITERION
Northwestern Polytechnical University Xiao Shouting
Northwestern Polytechnical University Xiao Shouting
..............page:135-139
THE CALIBRATION OF ELECTRICAL POTENTIAL OF STANDARD CT AND TPB SPECIMENS USING BOUNDARY ELEMENT METHOD
Northwestern Poly technica! University Wang Jianjun Liu Xiaokun Lu Minxu
Northwestern Poly technica! University Wang Jianjun Liu Xiaokun Lu Minxu
..............page:140-143
Absolute Size Effect on Fatigue
Tsinghua University Zeng Pan Yu Xinlu Yan Yongnian zheng Chuhong
Tsinghua University Zeng Pan Yu Xinlu Yan Yongnian zheng Chuhong
..............page:144-147