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25 April 1995, Volume 16 Issue 2

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25 April 1995, Volume 16 Issue 2

论文

THREE DIMENSIONAL PROBLEM IN DAMAGE TOLERANCE DESIGN OF AIRCRAFT STRUCTURES
Abstract( 1737 )

Guo Wanlin

1995, (2): 2-9.

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PROBABILITY DAMAGE TOLERANCE EVALUATION METHOD FOR MULTI-CRACKED STRUCTURE
Abstract( 1450 )

Fei Binjun;Tong Mingbo;Liu Wenting

1995, (2): 10-15.

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NUMERICAL SIMULATION AND EXPERIMENTAL VERIFICATION OF FAILURE PROCESS AND LOAD-CARRYING CAPACITY FOR MECHANICALLY FASTENED JOINTS IN COMPOSITE MATERIALS AND STRUCTURES
Abstract( 1547 )

Guan Changwen;Chen Haoran;Zheng Changlian

1995, (2): 16-20.

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DISTRIBUTION MODEL OF FATIGUE LIFE AND ITS GOODNESS-OF-FIT TEST
Abstract( 1481 )

Dong Cong;Rong Haiwu;Xia Renwei

1995, (2): 21-25.

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PROGRESSIVE DAMAGE SINULATION FOR SIMGLE FASTENER COMPOSITE JOINTS
Abstract( 1363 )

Hua Yu;Li Zhengneng;Kou Changhe;Luo Xiaodong;He Qingzhi

1995, (2): 26-32.

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A CYCLIC VISCOPLASTIC DESCRIPTION FOR THE EFFECT OF MEAN STRAIN
Abstract( 1436 )

Yang Xianjie

1995, (2): 33-38.

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ANALYTICAL VARIATIONAL METHOD OF SOLUTION FOR STRESS CONCENTRATION FACTORS OF FINITE PLATES WITH A PIN HOLE
Abstract( 1304 )

Xi YuanShan;Zhang Xing

1995, (2): 39-45.

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ON THE NONLOCAL THEORY MEASUREMENT OF STRESS CONCENTRATION NEAR THE EDGE OF A CIRCULAR HOLE
Abstract( 1547 )

Liu Zhenguo Zhu Depei

1995, (2): 46-50.

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A VARIABLE OPTIMIZATION METHOD A NEW TECHNIQUE FOR MULTICRACK GROWTH ANALYSIS IN STRUCTURE DETAILS
Abstract( 1034 )

Zhou Yuequan;Wang sunna

1995, (2): 51-54.

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A PARAMETER STUDY OF FATIGUE CRACK PROPAGATION
Abstract( 1269 )

Ni Huiling;Fu Xiangjiong

1995, (2): 55-60.

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THE MATHEMATICAL MODEL da/dN-(ΔK,f)OF CORROSION FATIGUE CRACK GROWTH
Abstract( 1347 )

Jiang Jianhua;Fan Weiwun;Huang Weiyang

1995, (2): 61-65.

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THE RELATION BETWEEN A STRUCTURAL RISK OF FAILURE AND SERVICE LIFE
Abstract( 1183 )

Qiu Jin;Xue Jingchuan

1995, (2): 66-69.

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EFFECTS OF PERIODIC OVERLOADS ON CORROSION FATIGUE CRACK PROPAGATION IN LY12CZ ALUMINUM ALLOY
Abstract( 1224 )

Wang Rong;heng Xiulin

1995, (2): 70-74.

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AN OPTIMUM METHOD FOR ESTIMATING PARAMETERS OF CRACK GROWTH MODEL UNDER LOAD SPECTRUM IN AIRCRAFT STURCTURE DESIGN
Abstract( 1061 )

Yan Hongjia;Liu Wenting

1995, (2): 75-77.

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EFFECT OF AIRCRAFT STRUCTURE FLEXIBILITY ON THE SHOCK-ABSORBER BEHAVIOR OF LANDING GEARS
Abstract( 1956 )

Mu Rangke Luo;Junjie

1995, (2): 78-81.

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AN EXPERIMENTAL STUDY OF STRENGTHENING TECHNOLOGY BY LASER CLADDING
Abstract( 1817 )

Guo Zhide

1995, (2): 82-84.

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THE RESEARCH OF STRUCTURAL DURABILITY ANALYSIS MTHOD BASED ON PROBABILISTIC FATIGUE
Abstract( 1110 )

Dong Dengke;Sue Jingchuan;Yang Yugong

1995, (2): 85-90.

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A SIMPLIFIED IFQ MODEL FOR DURABILITY ANALYSIS OF STRUCTURES
Abstract( 1201 )

Chen Chuanyao;Gao Daxing

1995, (2): 91-94.

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A STDUY ON EXPRESSIONS OF FATIGUE CRACK PROPAGATION IN ALL AREA
Abstract( 1265 )

Liu Wenting;Hu Renwei

1995, (2): 95-98.

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CHARACTERISTIC STRESS APPROACH FOR DURABILITY ANALYSIS
Abstract( 1168 )

Wang Zhizhi;Nie Xuezhou;Zheng Minzhong

1995, (2): 99-103.

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STRESS ANALYSIS OF COLDWORKED HOLES USING A COMBINED HARDENING MODEL
Abstract( 1211 )

Li Yazhi;Zhou Jinxing;Xing Wenzhen

1995, (2): 104-107.

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RESIDUAL STRENGTH TESTS AND STATISTICAL ANALYSIS FOR THIN WALLED STIFFENED STRUCTURE WITH MULTI CRACKS
Abstract( 1049 )

Yan Wensheng;Lu Fumei

1995, (2): 108-112.

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DAMAGE EQUIVALENT RECURRENCE METHOD OF FATIGUE RELIABILITY ANALYSIS UNDER PROGRAM LOADING
Abstract( 1095 )

Xie Liyang;Hu Qiao;Lin Wenqiang

1995, (2): 113-115.

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RELIABILITY ANALYSIS OF MULTI-SUPPORT AXIS DEFORMATION SEIZURE
Abstract( 1166 )

He Dongbin;Feng Yuansheng;Shi Tianlu

1995, (2): 116-118.

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A FINITE ELEMENT SIMULATION OF STABLE CRACK PROPAGATION IN POWER LAW HARDENING MATERIALS UNDER PLANE STRESS
Abstract( 1205 )

Zhu Wenhao

1995, (2): 120-125.

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CORROSION FATIGUE L IFE EVALUATION METHOD RESEARCHES FOR THE BOL TED JOINTS
Abstract( 977 )

Han Jinling

1995, (2): 126-127.

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THE TWO APPROACHES FOR CALCULATING FAILURE PROBABILITY OF STRUCTURES
Abstract( 1255 )

Wang Zhizhi;Wang Bin

1995, (2): 128-129.

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