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THREE DIMENSIONAL PROBLEM IN DAMAGE TOLERANCE DESIGN OF AIRCRAFT STRUCTURES
Guo Wanlin
1995, (2): 2-9.
PDF [ 390 K ]( 652 ) HTML
PROBABILITY DAMAGE TOLERANCE EVALUATION METHOD FOR MULTI-CRACKED STRUCTURE
Fei Binjun;Tong Mingbo;Liu Wenting
1995, (2): 10-15.
PDF [ 297 K ]( 549 ) HTML
NUMERICAL SIMULATION AND EXPERIMENTAL VERIFICATION OF FAILURE PROCESS AND LOAD-CARRYING CAPACITY FOR MECHANICALLY FASTENED JOINTS IN COMPOSITE MATERIALS AND STRUCTURES
Guan Changwen;Chen Haoran;Zheng Changlian
1995, (2): 16-20.
PDF [ 222 K ]( 657 ) HTML
DISTRIBUTION MODEL OF FATIGUE LIFE AND ITS GOODNESS-OF-FIT TEST
Dong Cong;Rong Haiwu;Xia Renwei
1995, (2): 21-25.
PDF [ 291 K ]( 1185 ) HTML
PROGRESSIVE DAMAGE SINULATION FOR SIMGLE FASTENER COMPOSITE JOINTS
Hua Yu;Li Zhengneng;Kou Changhe;Luo Xiaodong;He Qingzhi
1995, (2): 26-32.
PDF [ 398 K ]( 761 ) HTML
A CYCLIC VISCOPLASTIC DESCRIPTION FOR THE EFFECT OF MEAN STRAIN
Yang Xianjie
1995, (2): 33-38.
PDF [ 306 K ]( 710 ) HTML
ANALYTICAL VARIATIONAL METHOD OF SOLUTION FOR STRESS CONCENTRATION FACTORS OF FINITE PLATES WITH A PIN HOLE
Xi YuanShan;Zhang Xing
1995, (2): 39-45.
PDF [ 323 K ]( 454 ) HTML
ON THE NONLOCAL THEORY MEASUREMENT OF STRESS CONCENTRATION NEAR THE EDGE OF A CIRCULAR HOLE
Liu Zhenguo Zhu Depei
1995, (2): 46-50.
PDF [ 287 K ]( 784 ) HTML
A VARIABLE OPTIMIZATION METHOD A NEW TECHNIQUE FOR MULTICRACK GROWTH ANALYSIS IN STRUCTURE DETAILS
Zhou Yuequan;Wang sunna
1995, (2): 51-54.
PDF [ 146 K ]( 433 ) HTML
A PARAMETER STUDY OF FATIGUE CRACK PROPAGATION
Ni Huiling;Fu Xiangjiong
1995, (2): 55-60.
PDF [ 324 K ]( 672 ) HTML
THE MATHEMATICAL MODEL da/dN-(ΔK,f)OF CORROSION FATIGUE CRACK GROWTH
Jiang Jianhua;Fan Weiwun;Huang Weiyang
1995, (2): 61-65.
PDF [ 295 K ]( 706 ) HTML
THE RELATION BETWEEN A STRUCTURAL RISK OF FAILURE AND SERVICE LIFE
Qiu Jin;Xue Jingchuan
1995, (2): 66-69.
PDF [ 189 K ]( 449 ) HTML
EFFECTS OF PERIODIC OVERLOADS ON CORROSION FATIGUE CRACK PROPAGATION IN LY12CZ ALUMINUM ALLOY
Wang Rong;heng Xiulin
1995, (2): 70-74.
PDF [ 224 K ]( 626 ) HTML
AN OPTIMUM METHOD FOR ESTIMATING PARAMETERS OF CRACK GROWTH MODEL UNDER LOAD SPECTRUM IN AIRCRAFT STURCTURE DESIGN
Yan Hongjia;Liu Wenting
1995, (2): 75-77.
PDF [ 210 K ]( 418 ) HTML
EFFECT OF AIRCRAFT STRUCTURE FLEXIBILITY ON THE SHOCK-ABSORBER BEHAVIOR OF LANDING GEARS
Mu Rangke Luo;Junjie
1995, (2): 78-81.
PDF [ 143 K ]( 786 ) HTML
AN EXPERIMENTAL STUDY OF STRENGTHENING TECHNOLOGY BY LASER CLADDING
Guo Zhide
1995, (2): 82-84.
PDF [ 213 K ]( 483 ) HTML
THE RESEARCH OF STRUCTURAL DURABILITY ANALYSIS MTHOD BASED ON PROBABILISTIC FATIGUE
Dong Dengke;Sue Jingchuan;Yang Yugong
1995, (2): 85-90.
PDF [ 290 K ]( 476 ) HTML
A SIMPLIFIED IFQ MODEL FOR DURABILITY ANALYSIS OF STRUCTURES
Chen Chuanyao;Gao Daxing
1995, (2): 91-94.
PDF [ 228 K ]( 447 ) HTML
A STDUY ON EXPRESSIONS OF FATIGUE CRACK PROPAGATION IN ALL AREA
Liu Wenting;Hu Renwei
1995, (2): 95-98.
PDF [ 241 K ]( 654 ) HTML
CHARACTERISTIC STRESS APPROACH FOR DURABILITY ANALYSIS
Wang Zhizhi;Nie Xuezhou;Zheng Minzhong
1995, (2): 99-103.
PDF [ 264 K ]( 429 ) HTML
STRESS ANALYSIS OF COLDWORKED HOLES USING A COMBINED HARDENING MODEL
Li Yazhi;Zhou Jinxing;Xing Wenzhen
1995, (2): 104-107.
PDF [ 252 K ]( 580 ) HTML
RESIDUAL STRENGTH TESTS AND STATISTICAL ANALYSIS FOR THIN WALLED STIFFENED STRUCTURE WITH MULTI CRACKS
Yan Wensheng;Lu Fumei
1995, (2): 108-112.
PDF [ 285 K ]( 363 ) HTML
DAMAGE EQUIVALENT RECURRENCE METHOD OF FATIGUE RELIABILITY ANALYSIS UNDER PROGRAM LOADING
Xie Liyang;Hu Qiao;Lin Wenqiang
1995, (2): 113-115.
PDF [ 207 K ]( 715 ) HTML
RELIABILITY ANALYSIS OF MULTI-SUPPORT AXIS DEFORMATION SEIZURE
He Dongbin;Feng Yuansheng;Shi Tianlu
1995, (2): 116-118.
PDF [ 218 K ]( 529 ) HTML
A FINITE ELEMENT SIMULATION OF STABLE CRACK PROPAGATION IN POWER LAW HARDENING MATERIALS UNDER PLANE STRESS
Zhu Wenhao
1995, (2): 120-125.
PDF [ 342 K ]( 588 ) HTML
CORROSION FATIGUE L IFE EVALUATION METHOD RESEARCHES FOR THE BOL TED JOINTS
Han Jinling
1995, (2): 126-127.
PDF [ 63 K ]( 500 ) HTML
THE TWO APPROACHES FOR CALCULATING FAILURE PROBABILITY OF STRUCTURES
Wang Zhizhi;Wang Bin
1995, (2): 128-129.
PDF [ 151 K ]( 551 ) HTML
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