Probabilistic simulation of progressive fracture in bolted joint composite laminates

被引：0
|
作者：
Chamis, C.C.
Singhal, S.N.
Minnetyan, L.
机构：
来源：
NASA Technical Memorandum | 1996年 / 107107期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [41] PROGRESSIVE TRANSVERSE CRACKING IN COMPOSITE LAMINATES
    LAWS, N
    DVORAK, GJ
    JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (10) : 900 - 916
  • [42] Influence of Shim Layers on Progressive Failure of a Composite Component in Composite-Aluminum Bolted Joint in Aerospace Structural Assembly
    Cephas Yaw Attahu
    An Luling
    Li Zhaoqing
    Gao Guoqiang
    Transactions of Nanjing University of Aeronautics and Astronautics, 2018, 35 (01) : 188 - 202
  • [43] Global/Local analysis for progressive fracture of bolted structure
    Jiang, Jinfeng
    Zhang, Ying
    Sun, Qin
    Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 2010, 42 (03): : 318 - 321
  • [44] Subcritical damage mechanisms of bolted joints in CFRP composite laminates
    Atas, A.
    Soutis, C.
    COMPOSITES PART B-ENGINEERING, 2013, 54 : 20 - 27
  • [45] Strength prediction of bolted joints in graphite/epoxy composite laminates
    Tserpes, KI
    Labeas, G
    Papanikos, P
    Kermanidis, T
    COMPOSITES PART B-ENGINEERING, 2002, 33 (07) : 521 - 529
  • [46] FAILURE RESPONSE OF TWO SERIAL BOLTED JOINTS IN COMPOSITE LAMINATES
    Sen, F.
    Sayman, O.
    JOURNAL OF MECHANICS, 2011, 27 (03) : 293 - 307
  • [47] Failure Analysis of Single and Double Bolted Joints for Composite Laminates
    Mehmood, Saqib
    Zhao Libin
    Huang Hai
    2015 12TH INTERNATIONAL BHURBAN CONFERENCE ON APPLIED SCIENCES AND TECHNOLOGY (IBCAST), 2015, : 49 - 54
  • [48] A finite element simulation and experimental validation of a composite bolted joint loaded in bending and torsion
    Cavatorta, M. P.
    Paolino, D. S.
    Peroni, L.
    Rodino, M.
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2007, 38 (04) : 1251 - 1261
  • [49] Parameterized simulation for composite laminates with single mechanically fastened joint based on ANSYS
    Zhang, Shuang
    Wang, Dong
    Li, Zheng-Neng
    Kou, Chang-He
    Zhang, Yi-Ning
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2006, 27 (06): : 1088 - 1091
  • [50] Progressive Failure Simulation for Damaged Composite Laminates Using Nonlinear Finite Element Method
    许承东
    张慧
    孙家广
    郦正能
    TsinghuaScienceandTechnology, 1999, (04) : 1628 - 1631
12345