The dynamic response of composite sandwich beams to transverse impact

被引:73
作者
Tagarielli, V. L. [1 ]
Deshpande, V. S. [1 ]
Fleck, N. A. [1 ]
机构
[1] Univ Cambridge, Dept Engn, Cambridge CB2 1PZ, England
关键词
composite sandwich panels; dynamic testing; PVC foam; balsa wood;
D O I
10.1016/j.ijsolstr.2006.07.015
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The dynamic response of glass fibre-vinylester composite beams is measured by impacting the beams at mid-span with metal foam projectiles. The beams exist in composite monolithic form, and in sandwich configuration with composite face-sheets and a core made from PVC foam or end-grain balsa wood. High-speed photography is used to measure the transient transverse deflection of the beams and to record the dynamic modes of deformation and failure. For both monolithic and sandwich configurations, a flexural wave travels from the impact site towards the supports. Ultimate failure of the monolithic and sandwich beams is by tensile tearing of the faces. The sandwich beams also exhibit cracking of the core, and face-sheet delamination. The dynamic strength of the beams is quantified by the maximum transient transverse deflection at mid-span of the beams as a function of projectile momentum. It is demonstrated that sandwich beams can outperform monolithic beams of equal mass. The trade-off between core strength and core thickness is such that a low density PVC foam core outperforms a higher density PVC foam core. End-grain balsa wood has a superior stiffness and strength to that of PVC foam in compression and in shear. Consequently, sandwich beams with a balsa core outperform beams with a PVC foam core for projectiles of low momentum. The order reverses at high values of projectile momentum: the sandwich beams with a balsa wood core fail prematurely in longitudinal shear by splitting along the grain. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2442 / 2457
页数:16
相关论文
共 24 条
  • [1] Abrate S., 1997, APPL MECH REV, V50, P69, DOI DOI 10.1115/1.3101689
  • [2] Abrate Serge., 1998, IMPACT COMPOSITE STR, DOI [10.1017/CBO9780511574504, DOI 10.1017/CBO9780511574504]
  • [3] Ashby MF, 2000, METAL FOAM DESIGN GU
  • [4] Multi-axial yield behaviour of polymer foams
    Deshpande, VS
    Fleck, NA
    [J]. ACTA MATERIALIA, 2001, 49 (10) : 1859 - 1866
  • [5] The resistance of clamped sandwich beams to shock loading
    Fleck, NA
    Deshpande, VS
    [J]. JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2004, 71 (03): : 386 - 401
  • [6] Gibson L J., 1997, CELLULAR SOLIDS STRU, DOI [10.1017/CBO9781139878326, DOI 10.1017/CBO9781139878326]
  • [7] A TENSILE TESTING TECHNIQUE FOR FIBER-REINFORCED COMPOSITES AT IMPACT RATES OF STRAIN
    HARDING, J
    WELSH, LM
    [J]. JOURNAL OF MATERIALS SCIENCE, 1983, 18 (06) : 1810 - 1826
  • [8] MAKINEN K, 2001, THESIS ROYAL I TECHN
  • [9] MCSHANE GJ, IN PRESS EUROPEAN A
  • [10] MOYER ET, 1991, SANDWICH CONSTRUCTIO, V2