On a theory of sandwich construction

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dc.contributor.author W. S. Hemp en_US
dc.date.accessioned 2014-10-21T15:52:16Z
dc.date.available 2014-10-21T15:52:16Z
dc.date.issued 1948 en_US
dc.identifier.other ARC/R&M-2672 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3215
dc.description.abstract The theory of sandwich construction developed in this paper proceeds from the simple assumption that the filling has only transverse direct and shear stiffnesses, corresponding to its functional requirements. This supposition permits integration of the equilibrium equations for the filling. The resulting integrals are used to study the compression buckling of a flat sandwich plate. The formulae obtained are complex, but may be simplified in practical cases. A second approach to sandwich problems is made in section 5, where a theory of 'bending' of plates is outlined. This generalises the usual theory, malting allowance for flexibility in shear. This approach is applied to overall compression buckling of a plate, and agreement with the previous calculations is found. This suggests the possibility of calculating budding loads Ior curved sandwich shells. A simple example, the symmetrical buckling of a circular cylinder in compression is worked out. The theory developed would seem applicable to all cases of buckling of not too short a wave length. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title On a theory of sandwich construction en_US


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