Buckling analysis of Levy-type orthotropic stiffened plate and shell based on different strain-displacement models

Abstract In the present work a model able to predict the buckling behavior of thin, orthotropic, stiffened plates and shells subject to axial compression is proposed. In the context of the Kirchhoff-Love plate theory and making use of different strain-displacement models – namely the von Karman model, the Koiter–Sanders shell model, an enhanced von Karman model and a spurious model commonly adopted in literature – the equilibrium equations have been solved by the Levy-type approach. The results obtained highlight the influence of each non-linear strain-displacement term and show that the von Karman model can noticeably overestimate the buckling load when the critical mode involves significant in-plane displacements.

[1]  W. H. Wittrick,et al.  Numerical Results for the Initial Buckling of Some Stiffened Panels in Compression , 1972 .

[2]  J. N. Reddy,et al.  Vibration and stability analyses of cross-ply laminated circular cylindrical shells , 1992 .

[4]  J. H. Starnes,et al.  Buckling behavior of compression-loaded composite cylindrical shells with reinforced cutouts , 2005 .

[5]  S. Ciaramella,et al.  Isoparametric FEM vs. BEM for Elastic Functionally Graded Materials , 2009 .

[6]  M. Aliabadi,et al.  Local buckling of thin-walled structures by the boundary element method , 2009 .

[7]  D. H. Campen,et al.  Semi-analytical stability analysis of doubly-curved orthotropic shallow panels - considering the effects of boundary conditions , 2002 .

[8]  T. Lewiński,et al.  Plates, Laminates and Shells: Asymptotic Analysis and Homogenization , 2000 .

[9]  Eugenio Ruocco,et al.  An analytical model for the buckling of plates under mixed boundary conditions , 2012 .

[10]  H. Rothert,et al.  An idealization concept for the stability analysis of ring-reinforced cylindrical shells under external pressure , 2002 .

[11]  H. Matsunaga Vibration and buckling of cross-ply laminated composite circular cylindrical shells according to a global higher-order theory , 2007 .

[12]  M. Aliabadi,et al.  Post buckling analysis of shear deformable shallow shells by the boundary element method , 2010 .

[13]  E. Ruocco,et al.  BUCKLING OF COMPOSITE PLATES WITH ARBITRARY BOUNDARY CONDITIONS BY A SEMI-ANALYTICAL APPROACH , 2012 .

[14]  Qiang Han,et al.  Nonlinear buckling and postbuckling of heated functionally graded cylindrical shells under combined axial compression and radial pressure , 2009 .

[15]  Kent A. Harries,et al.  PREDICTIVE RESPONSE OF NOTCHED STEEL BEAMS REPAIRED WITH CFRP STRIPS INCLUDING BOND-SLIP BEHAVIOR , 2012 .

[16]  Gajbir Singh,et al.  Some simple solutions for buckling loads of thin and moderately thick cylindrical shells and panels made of laminated composite material , 1997 .

[17]  F. Guarracino,et al.  An improved formulation for the assessment of the capacity load of circular rings and cylindrical shells under external pressure. Part 1. Analytical derivation , 2011 .

[18]  Massimiliano Fraldi,et al.  An improved formulation for the assessment of the capacity load of circular rings and cylindrical shells under external pressure. Part 2. A comparative study with design codes prescriptions, experimental results and numerical simulations , 2011 .

[19]  E. Ruocco,et al.  Critical behavior of flat and stiffened shell structures through different kinematical models: A comparative investigation , 2012 .

[20]  Faruk Sen,et al.  Buckling analysis of laminated composite plates with an elliptical/circular cutout using FEM , 2010, Adv. Eng. Softw..

[21]  Mark W. Hilburger,et al.  Effects of Imperfections on the Buckling Response of Compression-Loaded Composite Shells , 2000 .