Delamination Under Fatigue Loads in Composite Laminates: A Review on the Observed Phenomenology and Computational Methods

被引:145
作者
Bak, Brian L. V. [1 ,2 ]
Sarrado, Carlos [3 ]
Turon, Albert [3 ]
Costa, Josep [3 ]
机构
[1] Aalborg Univ, Dept Mech & Mfg Engn, Fibigerstraede 16, DK-9220 Aalborg, Denmark
[2] Siemens Wind Power, DK-9220 Aalborg, Denmark
[3] Univ Girona, Polytech Sch, AMADE, Girona 17071, Spain
关键词
delamination; fatigue; composites; computational methods; experimental observations; phenomenological models; COHESIVE ZONE MODEL; HIGH-CYCLE FATIGUE; CRACK-GROWTH; BONDED JOINTS; STRESS-RATIO; CARBON/EPOXY COMPOSITE; GLASS/EPOXY COMPOSITES; FRACTURE-TOUGHNESS; ELEMENT-ANALYSIS; EPOXY COMPOSITE;
D O I
10.1115/1.4027647
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Advanced design methodologies enable lighter and more reliable composite structures or components. However, efforts to include fatigue delamination in the simulation of composites have not yet been consolidated. Besides that, there is a lack of a proper categorization of the published methods in terms of their predictive capabilities and the principles they are based on. This paper reviews the available experimental observations, the phenomenological models, and the computational simulation methods for the three phases of delamination (initiation, onset, and propagation). It compiles a synthesis of the current state-of-the-art while identifying the unsolved problems and the areas where research is missing. It is concluded that there is a lack of knowledge, or there are unsolved problems, in all categories in the field, but particularly in the category of computational methods, which in turn prevents its inclusion in the structural design process. Suggested areas where short-term and midterm research should be focused to overcome the current situation are identified.
引用
收藏
页数:24
相关论文
共 142 条
  • [1] Fatigue damage modeling in solder interconnects using a cohesive zone approach
    Abdul-Baqi, A
    Schreurs, PJG
    Geers, MGD
    [J]. INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2005, 42 (3-4) : 927 - 942
  • [2] Adams D. F., 1987, TOUGHENED COMPOSITES, P242
  • [3] A new semi-empirical law for variable stress-ratio and mixed-mode fatigue delamination growth
    Allegri, G.
    Wisnom, M. R.
    Hallett, S. R.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2013, 48 : 192 - 200
  • [4] A new semi-empirical model for stress ratio effect on mode II fatigue delamination growth
    Allegri, G.
    Jones, M. I.
    Wisnom, M. R.
    Hallett, S. R.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2011, 42 (07) : 733 - 740
  • [5] Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates
    Andersons, J
    Hojo, M
    Ochiai, S
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2004, 26 (06) : 597 - 604
  • [6] [Anonymous], [No title captured]
  • [7] [Anonymous], APPL MATH MECH
  • [8] [Anonymous], P 10 INT C COMP MAT
  • [9] [Anonymous], D611597 ASTM
  • [10] [Anonymous], COMPOSITE MAT FATIGU