Modelling of perforation failure in fibre metal laminates subjected to high impulsive blast loading
作者： E. Sitnikova , Z.W. Guan , G.K. Schleyer , W.J. Cantwell
DOI: 10.1016/J.IJSOLSTR.2014.05.010
关键词: Aluminium 、 Materials science 、 Perforation (oil well) 、 Composite material 、 Aluminium alloy 、 Tearing 、 Composite number 、 Glass fiber 、 Deformation (engineering) 、 Ultimate tensile strength
摘要: Abstract Perforation failure of fibre metal laminate (FML) panels subjected to the localized high intensity blast loading is studied. The FMLs are based on various stacking configurations aluminium alloy sheets and layers woven glass in a polypropylene matrix (GFPP) composite. Finite element models were created using commercial software package Abaqus/Explicit, where constitutive relationships damage composite material described through user-defined subroutine. was modelled as an orthotropically elastic prior initiation growth subsequent instant rate-dependent model. simulated deformation modes found be good agreement with published experimental data. For thin GFPP layers, number dynamic scenarios captured, such petalling, large tensile tearing multiple debonding between layers. A degree correlation back face underlying revealed. Finally, transient behaviour FML during studied discussed.
core.ac.uk
sci-hub.se 参考文章(20)
N.M. Hassan, R.C. Batra, Modeling damage in polymeric composites Composites Part B-engineering. ,vol. 39, pp. 66- 82 ,(2008) , 10.1016/J.COMPOSITESB.2007.02.001
A. Vlot, Impact loading on fibre metal laminates International Journal of Impact Engineering. ,vol. 18, pp. 291- 307 ,(1996) , 10.1016/0734-743X(96)89050-6
Thuc P. Vo, Z.W. Guan, W.J. Cantwell, G.K. Schleyer, Modelling of the low-impulse blast behaviour of fibre–metal laminates based on different aluminium alloys Composites Part B-engineering. ,vol. 44, pp. 141- 151 ,(2013) , 10.1016/J.COMPOSITESB.2012.06.013
J. Fan, Z.W. Guan, W.J. Cantwell, Numerical modelling of perforation failure in fibre metal laminates subjected to low velocity impact loading Composite Structures. ,vol. 93, pp. 2430- 2436 ,(2011) , 10.1016/J.COMPSTRUCT.2011.04.008
G LANGDON, G NURICK, S LEMANSKI, M SIMMONS, W CANTWELL, G SCHLEYER, Failure characterisation of blast-loaded fibre–metal laminate panels based on aluminium and glass–fibre reinforced polypropylene Composites Science and Technology. ,vol. 67, pp. 1385- 1405 ,(2007) , 10.1016/J.COMPSCITECH.2006.09.010
M. A. McCarthy, J. R. Xiao, N. Petrinic, A. Kamoulakos, V. Melito, Modelling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates – Part 1: Material Modelling Applied Composite Materials. ,vol. 11, pp. 295- 315 ,(2004) , 10.1023/B:ACMA.0000037133.64496.13
A. Seyed Yaghoubi, B. Liaw, Effect of lay-up orientation on ballistic impact behaviors of GLARE 5 FML beams International Journal of Impact Engineering. ,vol. 54, pp. 138- 148 ,(2013) , 10.1016/J.IJIMPENG.2012.10.007
Y. Shi, T. Swait, C. Soutis, Modelling damage evolution in composite laminates subjected to low velocity impact Composite Structures. ,vol. 94, pp. 2902- 2913 ,(2012) , 10.1016/J.COMPSTRUCT.2012.03.039
L. Iannucci, Progressive failure modelling of woven carbon composite under impact International Journal of Impact Engineering. ,vol. 32, pp. 1013- 1043 ,(2006) , 10.1016/J.IJIMPENG.2004.08.006
A. Matzenmiller, J. Lubliner, R.L. Taylor, A constitutive model for anisotropic damage in fiber-composites Mechanics of Materials. ,vol. 20, pp. 125- 152 ,(1995) , 10.1016/0167-6636(94)00053-0