Vibro-impact response of FRP sandwich plates with a foam core reinforced by chopped fiber rods

被引:56
作者
Li, Hui [1 ,2 ,3 ]
Li, Zelin [1 ]
Xiao, Zhengyang [1 ]
Xiong, Jian [4 ]
Wang, Xiangping [2 ]
Han, Qingkai [1 ]
Zhou, Jin [5 ]
Guan, Zhongwei [3 ,6 ]
机构
[1] Northeastern Univ, Sch Mech Engn & Automat, Shenyang 110819, Peoples R China
[2] Key Lab Impact Dynam Aero Engine, Shenyang 110015, Peoples R China
[3] Univ Liverpool, Sch Engn, Brownlow St, Liverpool L69 3GQ, England
[4] Harbin Inst Technol, Natl Key Lab Sci & Technol Adv Composites Special, Harbin 150001, Peoples R China
[5] Xi An Jiao Tong Univ, Sch Mech Engn, Xi'an 710054, Peoples R China
[6] Technol Innovat Inst, Masdar City, Abu Dhabi, U Arab Emirates
基金
中国博士后科学基金;
关键词
Vibro-impact response; FRP sandwich Plate; Reinforced foam core; Chopped fiber rods; FREE-VIBRATION; COMPOSITE; PANELS;
D O I
10.1016/j.compositesb.2022.110077
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In the present study, both the impact and vibration response characteristics of fiber reinforced polymer (FRP) sandwich plates (FRPSPs) with a foam core (FC) reinforced by chopped fiber rods (CFRs) are investigated. Initially, a dynamic model is proposed to predict the vibro-impact characteristics of the FC-CFRs-FRPSP structures. Here, by considering the influence of the dispersion pattern of chopped fiber rods, the equivalent material parameters of this complex core are redefined. Also, by employing the modified mid-plane displacement equation based on the principle of virtual work at the impact point, together with the progressive quasi-static approach and Reddy's high-order shear deformation principle, the key parameters such as impact contact force and displacement related to each failure event are obtained. In addition, with consideration of the impact damage, the natural frequencies and vibration responses are solved by using the energy principle, the proportional damping method, and the Duhamel integral technique. Finally, a number of the FC-FRPSP specimens with and without reinforcement of CFRs are fabricated and tested under different impact energies for verifying the present model. Also, the influences of critical geometric and material parameters on the vibro-impact response of the FC-CFRs-FRPSP structures are discussed. It has been found that the FC-CFRs-FRPSP specimens have a smaller vibro-impact response compared to the specimens without CFRs. For example, when impact energy of 10 J is applied, the impact peak force increases by 19.1%, the impact displacement reduces by 26.6%, and the maximum time-domain vibration response reduces by 5.8%. To reduce the vibro-impact response of such structures, it is recommended to adopt a large thickness ratio of the CFR reinforced foam core to the overall sandwich plate as well as volume fraction of CFRs to the foam core with a uniform dispersion pattern.
引用
收藏
页数:14
相关论文
共 65 条
  • [1] Snap-buckling and failure studies on CFRP laminate with an embedded circular delamination under flexural loading
    Andraju, Lala Bahadur
    Ramji, M.
    Raju, Gangadharan
    [J]. COMPOSITES PART B-ENGINEERING, 2021, 214
  • [2] [Anonymous], 2010, E7562005 ASTM
  • [3] [Anonymous], 2005, D7136 ASTM
  • [4] Bending and free vibration analysis of foam-filled truss core sandwich panel
    Arunkumar, M. P.
    Pitchaimani, Jeyaraj
    Gangadharan, K. V.
    [J]. JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2018, 20 (05) : 617 - 638
  • [5] Experiments and nonlinear analysis of the impact behaviour of sandwich panels constructed with flax fibre-reinforced polymer faces and foam cores
    Betts, Dillon
    Sadeghian, Pedram
    Fam, Amir
    [J]. JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2021, 23 (07) : 3139 - 3163
  • [6] Effect of boundary support conditions on impact behavior of silicone pin-reinforced polymer sandwich composite structure
    Chauhan, Shivanku
    Sahu, Sonika
    Ansari, Mohd. Z.
    [J]. POLYMER COMPOSITES, 2020, 41 (12) : 5104 - 5115
  • [7] Geometrically nonlinear transient analysis of composite laminated plate and shells subjected to low-velocity impact
    Choi, I. H.
    [J]. COMPOSITE STRUCTURES, 2016, 142 : 7 - 14
  • [8] Assessment of the apparent bending stiffness and damping of multilayer plates; modelling and experiment
    Ege, Kerem
    Roozen, N. B.
    Leclere, Quentin
    Rinaldi, Renaud G.
    [J]. JOURNAL OF SOUND AND VIBRATION, 2018, 426 : 129 - 149
  • [9] Quasi-static and low-velocity impact responses of polypropylene random copolymer composites with adjustable crystalline structures
    Fang, Wenjun
    Yang, Xujing
    Xu, Xinxin
    Li, Weiwei
    Li, Qing
    [J]. COMPOSITES PART B-ENGINEERING, 2021, 224
  • [10] Influence of interfacial adhesive on impact and post-impact behaviors of CFRP/end-grain balsawood sandwich composites
    Fatima, Narin Sara
    Dhaliwal, Gurpinder Singh
    Newaz, Golam
    [J]. COMPOSITES PART B-ENGINEERING, 2021, 212