A multi-area fatigue damage model of composite honeycomb sandwich panels under three-point bending load

被引：13
|
作者：
Ma, Mingze [1 ]
Yao, Weixing [2 ]
Jiang, Wen [1 ]
Jin, Wei [3 ]
Chen, Yan [3 ]
Li, Piao [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Key Lab Fundamental Sci Natl Def Adv Design Techn, Nanjing 210016, Peoples R China
[3] Chengdu Aircraft Design Inst, Struct Strength Dept, Chengdu 610092, Peoples R China
来源：
COMPOSITE STRUCTURES | 2021年 / 261卷
关键词：
Composite sandwich panels; Fatigue damage; Three-point bending test; IMPACT RESPONSE; BEAMS; BEHAVIOR; CORE; FOAM;
D O I：
10.1016/j.compstruct.2021.113603
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The fatigue damage of composite sandwich panels is divided into two parts: the face sheet damage and the core damage. Both the two kinds of damage cause the performance degradation of panels, however only the core damage results in the ultimate failure. In this paper, a fatigue damage model of the face sheet and the core is proposed and three-point bending tests are carried out to obtain the deflection evolution curves. With the proposed model, the fatigue damage can be predicted accurately, which proves the validity of the fatigue damage model proposed in this paper.
引用
收藏
页数：8
相关论文
共 50 条
  • [41] On the feasibility of a three-point bending setup for the validation of (fatigue) damage models for thin composite laminates
    De Baere, I.
    Van Paepegem, W.
    Degrieck, J.
    POLYMER COMPOSITES, 2008, 29 (10) : 1067 - 1076
  • [42] Deformation and Failure Behavior of Wooden Sandwich Composites with Taiji Honeycomb Core under a Three-Point Bending Test
    Hao, Jingxin
    Wu, Xinfeng
    Oporto, Gloria
    Wang, Jingxin
    Dahle, Gregory
    Nan, Nan
    MATERIALS, 2018, 11 (11):
  • [43] Damage Development in Hybrid Composite Laminates under Three-point Bending at Cryogenic Temperatures
    Miura, Masaya
    Shindo, Yasuhide
    Takeda, Tomo
    Narita, Fumio
    ADVANCES IN FRACTURE AND DAMAGE MECHANICS IX, 2011, 452-453 : 565 - 568
  • [44] Experimental three-point bending test of glass fibre aluminium honeycomb sandwich panel with acoustic emission damage assessment
    Abdulaziz, A. H.
    McCrory, J.
    Holford, K.
    Elsabbagh, A.
    Hedaya, M.
    INSIGHT, 2021, 63 (12) : 727 - 733
  • [45] Experimental analysis of behavior and damage of sandwich composite materials in three-point bending. Part 2. Fatigue test results and damage mechanisms
    A. Bezazi
    A. El Mahi
    J.-M. Berthelot
    B. Bezzazi
    Strength of Materials, 2009, 41 : 257 - 267
  • [46] Experimental analysis of behavior and damage of sandwich composite materials in three-point bending. Part 2. Fatigue test results and damage mechanisms
    Bezazi, A.
    El Mahi, A.
    Berthelot, J. -M.
    Bezzazi, B.
    STRENGTH OF MATERIALS, 2009, 41 (03) : 257 - 267
  • [47] Effect of Core Density on the Three-Point Bending Performance of Aluminum Foam Sandwich Panels
    Huang, Peng
    Gao, Qiang
    Su, Xixi
    Feng, Zhanhao
    Sun, Xi
    Zu, Guoyin
    MATERIALS, 2023, 16 (22)
  • [48] Unsymmetrical sandwich beams under three-point bending - Analytical studies
    Magnucka-Blandzi, Ewa
    Kedzia, Piotr
    Smyczynski, Mikolaj Jan
    COMPOSITE STRUCTURES, 2018, 202 : 539 - 544
  • [49] Numerical analysis of singly curved shallow composite panels under three-point bend load
    Guedes, R. M.
    Sa, Alcides
    COMPOSITE STRUCTURES, 2008, 83 (02) : 212 - 220
  • [50] Damage sequence of honeycomb sandwich panels under bending loading: Experimental and numerical investigation
    Medina, S. A.
    Meza, J. M.
    Kawashita, Luiz F.
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2020, 39 (5-6) : 175 - 192
12345