Vibration characteristic of delaminated plain woven fabric glass fiber/epoxy composite laminate under hygrothermal environment

被引：0
|
作者：
Jia B. [1 ]
Zhang G. [1 ]
Lin Y. [1 ]
Lu X. [1 ]
机构：
[1] Aeronautical Engineering, Civil Aviation University of China, Tianjin
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2019年 / 36卷 / 04期
关键词：
Delaminated plain woven fabric glass fiber/epoxy composite laminate; Delamination angle; Delamination location; Hygrothermal environment; Vibration characteristic;
D O I：
10.13801/j.cnki.fhclxb.20180703.001
中图分类号：
学科分类号：
摘要：
Through theoretical derived and finite element simulation, the vibration characteristic of delaminated plain woven fabric glass fiber/epoxy composite laminate with four sides clamped and one side clamped under hygrothermal environment were studied. This paper studies the relationship between delamination angle, delamination location and vibration characteristic. Based on the first order shearing deformation theory of Mindlin and Hamilton principle, the formula of hygrothermal constitutive equation and the natural frequency of laminated plates was derived, considering the hygrothermal stress, mass effect and the equivalence between moisture and temperature. Using user material subroutine (UMAT) interface with the finite element software ABAQUS, the corresponding interface program was compiled and a series of delaminated model under hygrothermal environment were established. It is found that the simulation results are in good agreement with literature experimental value. Results show that delamination makes vibration frequency decrease intensify under hygrothermal environment. Increasing delamination angle can cause the decline of frequency value, and the larger delamination angle, the larger decline frequency. The influence of moisture is more serious than that of temperature on vibration characteristic. The hygrothermal effect can cause the order of the base frequency decline and intensify the local resonance phenomenon. Surface delamination and middle delamination can cause modal change, but there is little difference. © 2019, Editorial Office of Acta Materiae Compositae Sinica. All right reserved.
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页码：892 / 904
页数：12
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共 24 条
  • [1] Ma L., Zhang J., Yue G., Application of composite materials in new generation of large civil aircraft, Acta Materiae Compositae Sinica, 32, 2, pp. 317-322, (2015)
  • [2] Tong G., Zhao L., Based on ABAQU-S woven fiber laminate structure analysis, In-Dustrial Technology, 24, 12, pp. 87-89, (2014)
  • [3] Jin P., Research on hygro-thermo-stress coupling response and damage of composites, (2011)
  • [4] Mei L., Vibration characteristic and optimiza-tion of the composite plate in thermal environm-ent, (2016)
  • [5] Feng Q., Li M., Gu Y., Experimental study on thermal properties of carbon fiber/epoxy composite materials under different hot and humid conditions, Acta Materiae Compositae Sinica, 27, 6, pp. 16-20, (2010)
  • [6] Tenek L.T., Some explicit beam, plate and s-hell finite elements, International Review of Civil Engineering, 5, 3, pp. 326-342, (2014)
  • [7] Bhattacharyya K., Sinha P.K., Finite element dynamic analysis of laminated composite plates with delaminations, Journal of Reinforced Plastics and Composites, 19, 11, pp. 863-882, (2000)
  • [8] Sarangan S., Singh B.N., Evaluation of free vibration and bending analysis of laminated com-posite and sandwich plates using non-polynomialzigzag models: C<sup>0</sup> Finite element formulation, Aerospace Science and Technology, 68, 7, pp. 496-508, (2017)
  • [9] Feng Z., Li D., Xu J., Study on the self-vibration characteristic of composite laminated composite laminated composites with multiple layers of damage, Acta Materiae Compositae Sinica, 26, 4, pp. 186-190, (2009)
  • [10] Feng G., Wang J., Cheng X., Effects of perforation damage size and direction on vibration characteristic of composite blades, Acta Materiae Compositae Sinica, 28, 1, pp. 151-155, (2011)
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