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  • COMSOL Multiphysics
  • 공학설계D/B

    공학설계D/B 게시판 내용
    Volume Title Structures
    Volume No Buckling of sandwich panels - under direct or shear loading, corrugated/orthotropic cores, local instability, face plate wrinkling.
    DATA Title Wrinkling of sandwich panel face plates (isotropic face plates on orthotropic cores, in-plane loading or bending).
    DATA Item 88032
    KEYWORD bending, compression, direct, faceplate, inelastic, instability, loading, panel, plasticity, sandwich, shear, wrinkling
    ISBN 0 85679 664 6
    ABSTRACT ESDU 88032 provides comprehensive data for estimating the wrinkling stress of the faceplates. The effect is taken into account of the faceplate properties and dimensions, the core shear moduli and through-thickness modulus, and the core dimensions. For in-plane loads (any combination o8f direct and shear) both symmetric and antisymmetric wrinkling modes are considered. The effect of material plasticity can be allowed for and comprehensive example calculations illustrate that. The implications of the theoretical models used are considered and guidance is provided on conditions where they may lead to an under- or over-estimate of the wrinkling stress of real structures. A method is given for estimating the reduction in wrinkling stress due to initial faceplate irregularities. Notes discuss the effects of variations in core properties and the possible influence of the faceplate/core adhesive layer.

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