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Tytuł artykułu

The analysis of buckling and post buckling in the compressed composite columns

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Języki publikacji
EN
Abstrakty
EN
Purpose: The aim of the study was to analyse the work of a thin-walled C-shaped profile, made of a carbon-epoxy composite, which was subjected to unified axial compression. Design/methodology/approach: The scope of the study included the analysis of the critical and low post-critical state by the use of numerical and experimental methods. As a result of the experimental test, performed on the physical specimen, post-critical equilibrium path had been determined, on the basis of which, with use of the adequate approximation method critical load value was defined. The next stage of the research was devoted to numerical analysis based on the finite element method. The studies were carried out on a scope of the linear analysis of the eigenvalue problem, on the basis of witch the critical value of load for mathematical model was found. The next step of the numerical tests was covering the nonlinear analysis of the low post-critical state for the model with geometrical imperfection, corresponding to the lowest form of buckling. Findings: The result of the study was to determine the value of the critical load, on the basis of the experimentally obtained post-critical equilibrium paths of the structure, with use of two independent methods of Approximation: Koiter's method and the method of the vertical tangent. The results of the analysis were compared with the value of the critical load determined by using finite element method. Research limitations/implications: The obtained results of study provide the important information concerning the modelling techniques of the thin-walled structures made of composite materials, while confirming the adequacy of the numerical models developed both in the calculation of eigenvalue problem, as well as non-linear static analysis in the post-critical range. Originality/value: The research provided the necessary knowledge of the behaviour of the critical and low post-critical of the thin-walled structure made of modern orthotropic material (CFRP).
Rocznik
Strony
35--41
Opis fizyczny
Bibliogr. 16 poz.
Twórcy
autor
  • Department of Machine Design and Mechatronics, Faculty of Mechanical Engineering, Lublin University of Technology, ul. Nadbystrzycka 36, 20-618 Lublin, Polska
Bibliografia
  • [1] H. Debski, A. Teter, T. Kubiak, Numerical and experimental studies of compressed composite columns, Composite Structures 118 (2014) 28-36.
  • [2] K. Falkowicz, P. Mazurek, P. Różyło, P. Wysmulski, W. Smagowski, Experimental and numerical analysis of the compression thin-walled composite plate, Advances in Science and Technology Research Journal 10/31 (2016) 177-184.
  • [3] T. Kopecki, J. Bakunowicz, T. Lis, Post-critical deformation states of composite thin-walled aircraft load-bearing structures, Journal of Theoretical and Applied Mechanics 54/1 (2016) 195-204.
  • [4] T. Kopecki, P. Mazurek, T. Lis, D. Chodorowska, Post-buckling deformation states of semi-monocoque cylindrical structures with large cut-outs under operating load conditions. Numerical analysis and experimental tests, Maintenance and Reliability 18/1 (2016) 16-24.
  • [5] P. Różyło, K. Wrzesinska, Numerical analysis of the behavior of compressed thin-walled elements with holes, Advances in Science and Technology Research Journal 10/31 (2016) 199-206.
  • [6] P. Wysmulski, H. Dębski, P. Różyło, K. Falkowicz, A study of stability and post-critical behaviour of thinwalled composite profiles under compression, Maintenance and Reliability 18/4 (2016) 632-637.
  • [7] J. Singer, J. Arbocz, T. Weller, Buckling experiments. Experimental methods in buckling of thin-walled structure, Vol. 1: Basic concepts, columns, beams, and plates, John Wiley & Sons Inc., New York, 2002.
  • [8] H. Debski, T. Sadowski, Modelling of microcracks initiation and evolution along interfaces of the WC/Co composite by the finite element method, Computational Materials Science 83 (2014) 403-411.
  • [9] Z. Kolakowski, R.J. Mania, Semi-analytical method versus the FEM for analyzing of the local postbuckling of thin-walled composite structures, Composite Structures 97 (2013) 99-106.
  • [10] E. Stanova, G. Fedorko, S. Kmet, V. Molnar, M. Fabian, Finite element analysis of spiral strands with different shapes subjected to axial loads, Advances in Engineering Software 83 (2015) 45-58.
  • [11] F. Bloom, D. Coffin, Handbook of thin plate buckling and postbuckling, Chapman & Hall/CRC, Boca Raton, London, New York, Washington D.C., 2001.
  • [12] K. Falkowicz, M. Ferdynus, H. Debski Numerical analysis of compressed plates with a cut-out operating in the geometrically nonlinear range, Maintenance and Reliability 17/12 (2015) 222-227.
  • [13] A. Teter, H. Debski, S. Samborski, On buckling collapse and failure analysis of thin-walled composite lippedchannel columns subjected to uniaxial compression, Thin-Walled Structures 85 (2014) 324-331.
  • [14] Z. Kolakowski, Static and dynamic interactive buckling of composite columns, Journal of Theoretical and Applied Mechanics 47 (2009) 177-192.
  • [15] G.J. Turvey, Y. Zhang, A computational and experimental analysis of the buckling, postbuckling and initial failure of pultruded GFRP columns, Computers & Structures 84 (2006) 1527-1537.
  • [16] O.C. Zienkiewicz, R.L. Taylor, Finite Element Method, Vol. 2: Solid Mechanics, 5th Edition, Elsevier, 2000.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-990f6db7-a288-4f60-99e9-bc76ee1cc147
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