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Modelling of stresses and strains in two-layer combined materials at their formation

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Języki publikacji
EN
Abstrakty
EN
Purpose: The aim of the represented study was to model the behaviour of two-layer combined material during its manufacturing. Design/methodology/approach: The model of material layers joining by means of calender method is built in LS-DYNA software on the basis of finite element method. Using the developed model the study of stress and strain condition changes is carried out. Numerical modelling was carried out for two types of two-layer combined materials in similar conditions. First combination was of high-density polyethylene top layer and aluminium foil bottom layer. Second combination was of high-density polyethylene top layer and low- density polyethylene bottom layer. Joining materials had equal thicknesses. Findings: During formation of two-layer combined materials the primary strain always occurs at the bottom plate of the bottom layer. However, the maximum plastic strain will be represented for the layer with lower elastic modulus value. At the point of the highest loading applied to the two-layer combined material the elasticity condition is changed to the plasticity one and the yield process is registered. Practical implications: Multi-layer combined materials are some of the most advanced types of materials. The quality of the joining of the layers, the strains and the stresses arising in their manufacturing process are the main causes of low interlayer strength. It leads to easy exfoliation and destruction of the material. The results of the study may be used to improve the quality of multi-layer combined materials. Originality/value: For the first time the model was developed for the determination of strains and stresses arising during the formation of multi-layer combined materials by means of calendering method. The calculations of the stresses and strains distribution dynamics for two-layer combined materials are represented for polymer-metal and polymer-polymer layers combinations. The results of the study may be of interest to specialists in the field of multi-layer combined materials designing and manufacturing.
Rocznik
Strony
12--19
Opis fizyczny
Bibliogr. 21 poz.
Twórcy
  • Department of Theoretical Mechanics, Engineering Science and Robotics Systems, N. E. Zhukovsky National Aerospace University Kharkiv Aviation Institute, 17 Chkalova str., Kharkiv, 61070, Ukraine
Bibliografia
  • [1] G.M. Koloskova, Classifier of multi-layer combined packaging materials, Bulletin of NTU “KhPI”, Series: Mechanical-technological Systems and Complexes 16/1238 (2014) 7-11 (in Russian).
  • [2] E. Sina (Ed.), Plastic films in food packaging. Materials, technology, and applications, William Andrew, 2012.
  • [3] M.I. Syomin, Calculations of compounds of structural elements of polymeric materials for strength and durability: a monograph, MADI, Moscow, 2016 (in Russian).
  • [4] L.B. Freund, S. Suresh, Thin Film Materials, Cambridge University Press, Cambridge, 2003.
  • [5] M.R. Begley, J.W. Hutchinson, The Mechanics and Reliability of Films, Multilayers and Coatings, Cambridge University Press, Cambridge, 2017.
  • [6] J.W. Hutchinson, Stresses and failure modes in thin films and multilayers, Technical University of Denmark, 1996.
  • [7] H.-H. Yu, M.-Y. He, J.W. Hutchinson, Edge effects in thin film delamination, Acta Materialia 49/1 (2001) 93-107, DOI: https://doi.org/10.1016/S1359-6454(00) 00293-7.
  • [8] A.G. Evans, J.W. Hutchinson, The thermomechanical integrity of thin films and multilayers, Acta Metallurgica et Materialia 43/7 (1995) 2507-2530, DOI:https://doi.org/10.1016/0956-7151(94)00444-M.
  • [9] M.D. Thouless, Z. Li, N.J. Douville, S. Takayama, Periodic cracking of films supported on compliant substrates, Journal of the Mechanics and Physics of Solids 59/9 (2011) 1927-1937, DOI: https://doi.org/ 10.1016/j.jmps.2011.04.009.
  • [10] H.-H. Yu, J.W. Hutchinson, Influence of substrate compliance on buckling delamination of thin films, International Journal of Fracture 113/1 (2002) 39-55, DOI: https://doi.Org/10.1023/A:1013790232359.
  • [11] B. Cotterell, Z. Chen, Buckling and cracking of thin films on compliant substrates under compression, International Journal of Fracture 104/2 (2000) 169-179, DOI: https://doi.org/10.1023/A:1007628800620.
  • [12] V. Rizov, Non-linear study of delamination cracks in multilayered beams, Multidiscipline Modeling in Materials and Structures 12/4 (2016) 678-692, DOI: https://doi.org/10.1108/MMMS-01 -2016-0003.
  • [13] M. Hajikazemi, M.H. Sadr, J. Varna, Analysis of cracked general cross-ply laminates under general bending loads: A variational approach, Journal of Composite Materials 51/22 (2017) 3089-3109, DOI: https://doi.org/10.1177/0021998316682364.
  • [14] F. Masoumi, A. Ghasemi-Ghalebahman, M.-J. Kokabi, Identification of mechanical and damage parameters of composite laminates based on a CPAM method, Journal of Reinforced Plastics and Composites 37/17 (2018) 1114-1128, DOI: https://doi.org/10.1177/0731684418793207.
  • [15] T. Liu, X. Ma, P.K. Wong, J. Zhao, Z Xie, V.A. Melo Cristino, A Simplified Finite Element Approach for Modeling of Multilayer Plates, Shock and Vibration 2019 (2019) Article ID 7295615, DOI: https://doi.org/ 10.1155/2019/7295615.
  • [16] A.K. Onkar, Nonlinear buckling analysis of damaged laminated composite plates, Journal of Composite Materials (2019), DOI: 10.1177/0021998319833446.
  • [17] J. Useche, H. Alvarez, Elastodynamic Analysis of Thick Multilayer Composite Plates by The Boundary Element Method, Computer Modeling in Engineering and Sciences 107/4 (2015) 277-296, DOI: 10.3970/ cmes.2015.107.277 .
  • [18] G.M. Koloskova, Experimental investigation of T-shaped welded joint of polymeric films, Issues of Design and Production of Aircraft Structures 3/83 (2015) 65-68 (in Russian).
  • [19] S.V. Kotomin, K.P. Sollogoub, Adhesion strength in multilayer polymer films, Engineering Journal: Science and Innovation 5 (2014) 1-9 (in Russian).
  • [20] LS-DYNA theoretical manual, Livermore Software Technology Corporation, Livermore, California, 1998.
  • [21] LS-DYNA keyword user’s manual, Livermore Software Technology Corporation, Livermore, California, 2006
Uwagi
PL
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-3f6fb8e5-42e1-4490-b310-62e1a33a6dca
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