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Assessment methods of mechanical properties of composite materials

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper deals with a specific kind of imperfection in multilayered composite structures as thickness deviation. During manufacturing process the layers are laminated together with resin. Lack of accuracy or some errors during autoclaving process could contribute to thickness deviation when thin layer of resin remains between plies. This is particularly important in the case of hybrid laminates as Fibre Metal Laminates (FML). Therefore, the aim of this work is to determine the impact of thickness imperfection on the variation of effective mechanical properties of FML thin-walled panels. Two methods have been considered in the study: assumption of additional resin/matrix layer in a stacking sequence and a correction of fibre volume fraction in composite layers. A full 3-2 FML lay-up has been analyzed using Classical Lamination Plate Theory with connection to two micromechanical approaches: analytical (Rule of Mixture) and numerical (Finite Element Method). Results of calculations were verified by conducted experimental tests.
Rocznik
Strony
1005--1018
Opis fizyczny
Bibliogr. 13 poz., il. kolor., rys., wykr.
Twórcy
autor
  • Department of Strength of Materials, Lodz University of Technology, Stefanowskiego 1/15, Łódź, Poland
autor
  • Department of Strength of Materials, Lodz University of Technology, Stefanowskiego 1/15, Łódź, Poland
Bibliografia
  • [1] Sinmazçelik, T., Avcu, E., Bora, M. Ö., Çoban, O.: A review: Fibre metal laminates. background, bonding types and applied test methods, Materials and Design, 32, 3671-3685, 2011.
  • [2] Vlot A., Gunnik, J. W.: Fiber Metal Laminates, An Introduction, Springer Science and Business Media B.V., 2001.
  • [3] Bienias, J.: Fibre Metal Laminates-some aspects of manufacturing process, structure and selected properties, Compos., Theory Pract., 11, 39-43, 2011.
  • [4] Bienias, J., Gliszczynski, A., Jakubczak, P., Kubiak, T., Majerski, K.: Influence of autoclaving process parameters on the buckling and postbuckling behaviour of thin-walled channel section beams, Thin-Walled Struct., 85, 262-270, http://dx.doi.org/10.1016/j.tws.2014.09.007, 2014.
  • [5] Czapski, P., Kubiak, T.: Influence of fibre arrangement on the buckling load of composite plates - analytical solution, Fibres Text East Eur., 5, 92, http://dx.doi.org/10.5604/12303666.1161764, 2015.
  • [6] Kamocka, M., Zglinicki, M., Mania, R. J.: Multi-method approach for FML mechanical properties prediction, Compos., Part B, 91, 135-143, http://dx.doi.org/10.1016/j.compositesb, 2016.
  • [7] Bieniaś, J., Mania, R. J., Jakubczak, P., Majerski, K.: The Issues of manufacturing of geometrically Complicated Elements by using FML Laminates, Compos, Theory Pract., 15, 4, 243-249, 2015.
  • [8] Jones, R. M.: Mechanics of composite materials, Taylor & Francis, 1999.
  • [9] Barbero, E.: Finite element analysis of composite materials using ANSYS, CRC Press, 2014.
  • [10] User's Guide ANSYS 14.5, Houston, USA, Ansys Inc.
  • [11] Bieniaś, A., Majerski, K., Surowska, B., Jakubczak, P.: The mechanical properties and failure analysis of selected fiber metal laminates, Lublin University of Technology, 2013.
  • [12] Moussavi-Torshizi, S. E., Dariushi, S., Sadighi, M., Safarpour, P.: A study on tensile, novel fiber/metal laminates, Materials Science and Engineering, A, 527, 4920-4925, 2010.
  • [13] Soltani, P., Keikhosravy, M., Oskouei, R. H., Soutis, C.: Studying the Tensile Behaviour of GLARE Laminates: A Finite Element Modelling Approach, Applied Composite Materials, 18, 271-282, 2011.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a23b444b-b336-4b67-aad7-ef41ec990a09
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