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Abstrakty
A buckling and post{buckling behavior analysis of thin-walled composite plate under a compressive force is presented. The plate with central notch was made of a carbonepoxy composite - a laminate consisting of eight symmetrically oriented plies. The one layer arrangement was taken into consideration. The main objective of the study was to investigate the behavior of the considered plate under quasi-static compression. A numerical analysis was conducted with the Abaqus commercial FEM software package. The experimental test was performed under standard conditions on a universal Zwick/Roell Z050 testing machine. The results obtained in the numerical methods are compared to these obtained experimentally. The experimental results were then used to develop new FEM models that allowed one to describe the post{buckling behavior and to estimate the ultimate load-carrying capacity of the composite plates under investigation.
Czasopismo
Rocznik
Tom
Strony
167--175
Opis fizyczny
Bibliogr. 25 poz.
Twórcy
autor
- Faculty of Mechanical Engineering Department of Machine Design and Mechatronics Lublin University of Technology Nadbystrzycka 36, 20-618 Lublin, Poland
autor
- Faculty of Mechanical Engineering Department of Machine Design and Mechatronics Lublin University of Technology Nadbystrzycka 36, 20-618 Lublin, Poland
Bibliografia
- [1] Bazant, Z. P. and Cedolin, L.: Stability of structures. Elastic, inelastic, fracture and damage theories, Oxford University Press, 1991.
- [2] Koiter, W. T.: Elastic stability and post–buckling behavior, In Proceedings of the Symposium on Non–linear Problems, Wisconsin: Univ. of Wisconsin Press, 257–275, 1963.
- [3] Krolak, M. and Mania, R.: Statics, dynamics and stability of structures, Stability of thin–walled plate structures, Series of monographs, odz: Technical University of Lodz, 2011.
- [4] Singer, J., Arbocz, J. andWeller, T.: Buckling experiments. Experimental methods in buckling of thin-walled structure. Basic concepts, columns, beams, and plates. New York: John Wiley & Sons inc., 1998.
- [5] Singer, J., Arbocz, J. and Weller, T.: Buckling experiments. Experimental methods in buckling of thin–walled structure. Shells built–up structures, composites and additional topics, New York: John Wiley & Sons inc., 2002.
- [6] Spencer, H. and Walker, A.: Techniques for Measuring The critical Loads of column and Plates, SeSa Spring Meeting, 25, 1974.
- [7] Tereszkowski, Z.: An experimental method for determining critical loads of plates, Archive of mechanical engineering, 3, 485–493, 1970.
- [8] Kopecki, T. and Mazurek, P.: Problems of numerical bifurcation reproducing in postcritical deformation states of aircraft structures, Journal of Theoretical and applied Mechanics, 51(4), 969-977, 2013.
- [9] Kopecki, T.: Numerical and experimental analysis of post-critical deformation states in a tensioned plate weakned by a crack. Journal of Theoretical and Applied Mechanics, 48(1), 45–70, 2010.
- [10] Kubiak, T.: Static and Dynamic Buckling of Thin–Walled Plate Structures, Springer, 1-25, http://dx.doi.org/10.1007/978-3-319-006543 1, http://dx.doi.org/10.1007/978-3-31900654-3, 2013.
- [11] Simitses, G. and Hodges, D.: Fundamentals of structural stability, Elsvier/Butterworth{heinemann, Amsterdam, 2006.
- [12] Thompson, J. M. T. and Hunt, G. W.: General theory of elastic stability, New York: Wiley, 1973.
- [13] Narayanan, R., Chow, F. Y.: Ultimate capacity of uniaxially compressed perforated plates, Thin-Walled Structures, 2(2), 241–264, 1984.
- [14] Prabhakara, D. L. and Datta, P. K.: Vibration, Buckling and Parametric Instability Behaviour of Plates with Centrally Located Cutouts Subjected to In–Plane Edge Loading (Tension or Compression), Thin-Walled Structures, 27(4), 287–310, 1997.
- [15] Ritchie, D. and Rhodes, J.: Buckling and post–buckling behaviour of plates with holes, The Aeronautical Quarterly, 26(4), 281–296, 1975.
- [16] Shanmugam, N. E.: Openings in Thin–walled Steel Structures, Thin-Walled Structures, 28(3/4), 355–372, 1997.
- [17] Kumar, D. and Singh, S. B.: Effects of boundary conditions on buckling and postbuckling responses of composite laminate with various shaped cutouts, Composites Structures, 92, 769–779, 2010.
- [18] Jain, P., Kumar, A.: Postbuckling response of square laminates with a central circular cutout, Composite Structures, 65, 179–185, 2004.
- [19] Falkowicz, K., Ferdynus, M., Dębski, H.: Numerical analysis of compressed plates with a cut-out operating in the geometrically nonlinear range, Maintenance and Reliability, 17(12), 222–235, 2015.
- [20] Swanson, S. R.: Introduction to design and analysis with advanced composite materials, Prentice-Hall, Inc., 1997.
- [21] Czapski, P. and Kubiak, T.: Influence of fibre arrangement on the buckling load of composite plates–analytical solution. Fibres and Textiles in Eastern Europe, 113(5), 92–98, 2015.
- [22] Dębski, H., Teter, A. and Kubiak, T.: Numerical and experimental studies of compressed composite columns, Composite Structures, 118, pp. 28–36, 2014.
- [23] Banat, D., Mania, R. J.: Comparison of failure criteria application for FML column buckling strength analysis, Composite Structures, 140, 806–815, 2016.
- [24] Kołakowski, Z. and Mania, R. J.: Semi–analytical method versus the FeM for analyzing of the local post–buckling of thin–walled composite structures, Composite Structures, 97, 99–106, 2013.
- [25] Kopecki, T. and Mazurek, P.: Numerical representation of post-critical deformations in the processes of determining stress distributions in closed multi–segment thin–walled aircraft load–bearing structures, Maintenance and Reliability, 16(1), 164–169, 2014.
Uwagi
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-0cea9364-cfbb-42e2-8618-0e708f6c3caa