In the last 3 decades, sinusoidal theory has been increasingly utilized to research mechanical behaviors of layered composite and sandwich structures. Nevertheless, the existing sinusoidal model will encounter trouble in precisely yielding the buckling loads of layered structures composed of layers with different material properties. Thus, a refined sinusoidal model is offered for the buckling analysis of composite and sandwich structures that can simulate the zigzag effect of the in-plane displacement and meet the free conditions of transverse shear stresses on the surfaces. In the light of the elegant sinusoidal model, a three-node beam element has been constructed to work out the discrete eigenvalue equation coming from the stability behavior. Making use of a mixed variational theorem from the literature, the finite-element formulation can meet beforehand the continuous conditions of transverse stress at the interfaces. The three-dimensional finite element method (3D-FEM) results are utilized to evaluate the precision and efficiency of the proposed approach through a numerical example. The proposed finite-element formulation can produce satisfactory results with lower calculational cost, and some interesting conclusions are presented. However, the results for stability of layered structures made of plies with different material properties will be overestimated by utilizing the models violating the continuous prerequisite of interlaminar stresses.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Mixed Finite-Element Formulation Based on Refined Sinusoidal Model for Buckling of Layered Beams


    Contributors:
    Xiaohui, Ren (author) / Zhen, Wu (author)

    Published in:

    Publication date :

    2020-04-17




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown



    Reinvestigation of Buckling of Shells of Revolution by a Refined Finite Element

    G. VENKATWARA RAO / S.K. RADHAMOHAN / AND I.S. RAJU | AIAA | 1974


    Refined Design Curves for Shear Buckling of Curved Panels Using Nonlinear Finite Element Analysis

    Domb, M. / Leigh, B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002