PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Local Buckling of Thin-Walled Column of Square Cross-Section Made of In-Plane Coupled Laminate

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The non–symmetric, general laminate exhibits different types of coupling between the extension, shearing, bending and twisting. For practical reasons, the in–plane coupled laminate is a particularly interesting. In this case, the coupling between shearing and extension takes place. Details calculations were performed for a short columns of square cross-section made of in–plane coupled and fully uncoupled laminate under uniform compression. Finite element method (FEM) and analytical–numerical method (ANM) were performed. In FEM analyses, the eigenbuckling problem has been solved using the Lanczos method, whereas the nonlinear buckling analysis were performed using the Newton– Raphson method and the Ritz method. In ANM analyses, the Koiter’s asymptotic theory is applied. The relationship between forces/moments and deformations/curvature were described using classical lamination theory (CLT). The coupling between in–plane shearing and extension has a significant influence on the behavior of thin–walled structures under compression.
Słowa kluczowe
Rocznik
Strony
129--141
Opis fizyczny
Bibliogr. 26 poz.
Twórcy
autor
  • Department of Applied Mechanics Lublin University of Technology Nadbystrzycka 36 St., PL-20-618 Lublin, Poland
  • Department of Applied Mechanics Lublin University of Technology Nadbystrzycka 36 St., PL-20-618 Lublin, Poland
  • Department of Strength of Materials Lodz University of Technology Stefanowskiego 1/15, 90-924 Łódź, Poland
Bibliografia
  • [1] York, C. B.: On extension–shearing coupled laminates, Composite Structures, 120, 472–482, 2015.
  • [2] Shamsudin, M. H. and York, C. B.: Mechanically coupled laminates with balanced plain weave, Composite Structures, 107, 416–428, 2014.
  • [3] Valot, E., Vannucci, P. and Verchery, G.: A linear theory for laminates composed of coupled layers, Composite Structures, 60, 413–429, 2003.
  • [4] Baker, N., Butler, R. and York, C. B.: Damage tolerance of fully orthotropic laminates in compression, Composites Science and Technology, 72, 1083–1089, 2012.
  • [5] York, C. B.: Coupled quasi-homogeneous orthotropic laminates, Mechanics of Composite Materials, 47(7), 405–426, 2011.
  • [6] York, C. B.: Characterization of nonsymmetric forms of fully orthotropic laminates, Journal of Aircraft, 46(4), 1114–1125, 2009.
  • [7] de Goeij, W. C., van Tooren, M. J. L. and Beukers, A.: Implementation of bending–torsion coupling in the design of a wind–turbine rotor–blade, Applied Energy, 63, 191–207, 1999.
  • [8] Murray, R. E., Doman, D. A. and Pegg, M. J.: Finite element modeling and effects of material uncertainties in a composite laminate with bend–twist coupling, Composite Structures, 121, 362–376, 2015.
  • [9] Vannucci, P. and Verchery, G.: A special class of uncoupled and quasihomogeneous laminates, Composites Science and Technology, 61, 1465–1473, 2001.
  • [10] Haynes, R. A. and Armanios, E. A.: New families of hygrothermally stable composite laminates with optimal extension–twist coupling, AIAA Journal, 48, (12), 2954–2961, 2010.
  • [11] Bhaskar, K., Varadan, T. K. and Ali, J. S. M.: Thermoelastic solutions for orthotropic and anisotropic composite laminates, Composites, Part B, 27B, 415–420, 1996.
  • [12] Jin, L. and Daokui, L.: Multi–objective optimization of hygro–thermally curvature–stable antisymmetric laminates with extension–twist coupling, Journal of Mechanical Science and Technology, 28, (4), 1373–1380, 2014.
  • [13] Jin, L. and Daokui, L.: Extension–shear coupled laminates with immunity to hygrothermal shearing distortion, Composite Structures, 123, 401–407, 2015.
  • [14] York, C. B.: Tapered hygro–thermally curvature–stable laminates with non–standard ply orientations, Composites, Part A, 44, 140–148, 2013.
  • [15] Loughlan, J.: The influence of mechanical couplings on the compressive stability of anti-symmetric angleply laminates, Composite Structures, 57, 473–482, 2002.
  • [16] Ovesy, H. R. and Assaee, H.: Semi–energy finite strip post–buckling analysis of laminated plates concerning the effects of mechanical coupling, Composite Structures, 89, 120–125, 2009.
  • [17] Walker, M., Adali, S. and Verijenkolg, V.: Optimization of symmetric laminates for maximum buckling load including the effects of bending-twisting coupling, Computers & Structures, 58, (2), 313–319, 1995.
  • [18] Walker, M., Adali, S. and Verijenkolg, V.: Optimal design of symmetric angleply laminates subject to nonuniform buckling loads and in-plane restraints, Thin-Walled Structures, 26, (1), 45–60, 1996.
  • [19] Band, U. N. and Desai, Y. M.: Coupled higher order and mixed layerwise finite element based static and free vibration analyses of laminated plates, Composite Structures, 128, 406–414, 2015.
  • [20] Jones, R. M.: Mechanics of composite materials, Taylor & Francis, Inc., Philadelphia, 1999.
  • [21] Kołakowski, Z. and Kowal{Michalska, K. (eds.): Selected problems of instabilities in composite structures, Wyd. Politechniki Łódzkiej, 1999.
  • [22] Teter, A. and Kołakowski, Z.: Coupled dynamic buckling of thin–walled composite columns with open cross-sections, Composite Structures, 95, 28–34, 2013.
  • [23] Byskov, E. and Hutchinson J. W.: Mode interaction in axially stiffened cylindrical shells, AIAA J., 15 (7), 941–948, 1977.
  • [24] van der Heijden, A. M. A. (ed.): W.T. Koiter’s Elastic Stability of Solids and Structures, Cambridge University Press, 2009.
  • [25] Kubiak, T.: Static and dynamic buckling of thin–walled plate structures, Springer, Verlag, London, 2013.
  • [26] Królak, M. (ed.): Postbuckling states and load carrying capacity of girders of flat walls, (in Polish), PWN, (Polish Scientific Publishers), Warsaw–Lodz, 1990.
Uwagi
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-25ef3469-acb8-4535-a9e7-7c24dc3707c7
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.