文摘
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 K¨¢rm¨¢n model, the Koiter-Sanders shell model, an enhanced von K¨¢rm¨¢n 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 K¨¢rm¨¢n model can noticeably overestimate the buckling load when the critical mode involves significant in-plane displacements.