journal article·2008-11

Symmetrical Facing Wrinkling of Composite Sandwich Panels

A.V. Lopatin, E.V. Morozov

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Abstract

The article presents the solution of symmetrical face sheet wrinkling problem for sandwich panel with composite facings and an orthotropic core. The new model is proposed for elastic core that takes into account compressive and shear stiffnesses as well as nonlinear change of transverse displacement over the core thickness at wrinkling. The governing buckling equation is derived using energy method. Analysis of cylindrical face wrinkling is performed for sandwich strips subjected to compressive loads applied to the two opposite simply supported edges. The effects of elastic and geometric parameters on the critical buckling stresses and wrinkling waves' formation are examined.
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Research context

OpenAlex topics: Structural Analysis and Optimization · Composite Structure Analysis and Optimization · Structural Analysis of Composite Materials

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Aerospace Engineering Siberian State Aerospace University, Krasnoyarsk, Russia

School of Aerospace, Civil & Mechanical Engineering University of New South Wales, University College at the Australian Defence Force Academy, Canberra, Australia,

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