3rd and 4th Aerospace Sciences Meeting 1966
DOI: 10.2514/6.1966-138
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General instability and face wrinkling of sandwich plates - Unified theory and applications

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Cited by 7 publications
(6 citation statements)
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“…Different approaches have been used for representing the core's behavior, all of which retain the transverse normal deformation in order to capture the wrinkling modes. A common assumption makes use of anti-plane cores, which disregards the in-plane load carrying capability of the core [21,[41][42][43]. This hypothesis has been shown to give misleading results not only when the core is isotropic [44], but also when the core is highly orthotropic, e.g., for honeycomb cores [30].…”
Section: Models For Overall Buckling and Wrinkling Of Sandwich Strutsmentioning
confidence: 99%
“…Different approaches have been used for representing the core's behavior, all of which retain the transverse normal deformation in order to capture the wrinkling modes. A common assumption makes use of anti-plane cores, which disregards the in-plane load carrying capability of the core [21,[41][42][43]. This hypothesis has been shown to give misleading results not only when the core is isotropic [44], but also when the core is highly orthotropic, e.g., for honeycomb cores [30].…”
Section: Models For Overall Buckling and Wrinkling Of Sandwich Strutsmentioning
confidence: 99%
“…Therefore, the natural frequencies of the sandwich beam, which are approximated using the procedure outlined above, do not differ significantly from those obtained from the consistent formulation where the two Timoshenko beam equations are used, and the main unknowns are the transverse displacement, w, and bending slope, . The term ''consistent'' as used here implies that the total order of the governing differential equations matches the number of boundary conditions imposed on the beam [19].…”
Section: Classical Sandwich Analysismentioning
confidence: 99%
“…If the global buckling of a sandwich material can be easily viewed as the classical buckling of a homogeneous structure (as soon as the equivalent properties have been properly derived), the local buckling analysis requires the use of advanced models. If the earliest contributions rely on uncoupled formulations, where the global and local buckling analyses are treated separately, many authors have tried to achieve unified models capable of describing both global and local modes (both symmetric/hourglass and antisymmetric/snaking) in the particular case of a sandwich column under axial compression (Benson and Mayers [3] have been the first to suggest a unified approach to solve the overall buckling and wrinkling problems simultaneously). Among them, a hybrid beam/2D model (with no kinematic assumption in the core layer) was recently developed by Douville and Le Grognec [4] which was first able to derive closed-form expressions of both buckling and wrinkling critical values of sandwich beamcolumns (accounting for all mode types) with a very good accuracy, compared to the numerous simplified models in earlier literature (see also [4] for a comprehensive review of analytical or numerical models for the buckling analysis of sandwich beam-columns/plates under various loading conditions, using different simplified kinematic assumptions).…”
Section: Introductionmentioning
confidence: 99%