Analytical evaluation on uniaxial tensile deformation behavior of fiber metal laminate based on SRPP and its experimental confirmation
作者： Byoung-Eon Lee , Eu-Ttem Park , Jeong Kim , Beom-Soo Kang , Woo-Jin Song
DOI: 10.1016/J.COMPOSITESB.2014.06.031
关键词: Deformation (engineering) 、 Finite element method 、 Fiber metal laminate 、 Fracture (geology) 、 Computer simulation 、 Composite material 、 Materials science 、 Ultimate tensile strength 、 Constitutive equation 、 Volume fraction
摘要: Abstract Uniaxial tensile tests have been carried out to accurately evaluate the in-plain mechanical properties of fiber metal laminates (FMLs). The FMLs in this paper comprised a layer self-reinforced polypropylene (SRPP) sandwiched between two layers aluminum alloy 5052-H34. In study, nonlinear and fracture behavior under in-plane loading conditions has investigated with numerical simulations theoretical analysis. simulation based on finite element modeling using ABAQUS/Explicit constitutive model volume fraction approach rule mixture modified classical lamination theory, which incorporates elastic–plastic SRPP, are used predict such as stress–strain response deformation FMLs. addition, pre-stretching process is reduce thermal residual stresses before uniaxial Through comparing analysis experimental results, it concluded that adopted can describe sufficient accuracy actual curve.
sci-hub.se 参考文章(16)
C. Soutis, Fibre reinforced composites in aircraft construction Progress in Aerospace Sciences. ,vol. 41, pp. 143- 151 ,(2005) , 10.1016/J.PAEROSCI.2005.02.004
S.U. Khan, R.C. Alderliesten, R. Benedictus, Post-stretching induced stress redistribution in Fibre Metal Laminates for increased fatigue crack growth resistance Composites Science and Technology. ,vol. 69, pp. 396- 405 ,(2009) , 10.1016/J.COMPSCITECH.2008.11.006
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
L.B Vogelesang, A Vlot, Development of fibre metal laminates for advanced aerospace structures Journal of Materials Processing Technology. ,vol. 103, pp. 1- 5 ,(2000) , 10.1016/S0924-0136(00)00411-8
Luke Mosse, Paul Compston, Wesley J. Cantwell, Michael Cardew-Hall, Shankar Kalyanasundaram, The development of a finite element model for simulating the stamp forming of fibre-metal laminates Composite Structures. ,vol. 75, pp. 298- 304 ,(2006) , 10.1016/J.COMPSTRUCT.2006.04.009
J. Gresham, W. Cantwell, M.J. Cardew-Hall, P. Compston, S. Kalyanasundaram, Drawing behaviour of metal-composite sandwich structures Composite Structures. ,vol. 75, pp. 305- 312 ,(2006) , 10.1016/J.COMPSTRUCT.2006.04.010
G. Caprino, G. Spataro, S. Del Luongo, Low-velocity impact behaviour of fibreglass-aluminium laminates Composites Part A-applied Science and Manufacturing. ,vol. 35, pp. 605- 616 ,(2004) , 10.1016/J.COMPOSITESA.2003.11.003
J.G. Carrillo, W.J. Cantwell, Mechanical properties of a novel fiber–metal laminate based on a polypropylene composite Mechanics of Materials. ,vol. 41, pp. 828- 838 ,(2009) , 10.1016/J.MECHMAT.2009.03.002
J.H. Ku, I.H. Jung, K.Y. Rhee, S.J. Park, Atmospheric pressure plasma treatment of polypropylene to improve the bonding strength of polypropylene/aluminum composites Composites Part B-engineering. ,vol. 45, pp. 1282- 1287 ,(2013) , 10.1016/J.COMPOSITESB.2012.06.016
Luke Mosse, Paul Compston, Wesley J. Cantwell, Michael Cardew-Hall, Shankar Kalyanasundaram, Stamp forming of polypropylene based fibre–metal laminates: The effect of process variables on formability Journal of Materials Processing Technology. ,vol. 172, pp. 163- 168 ,(2006) , 10.1016/J.JMATPROTEC.2005.09.002