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Journal ArticleDOI

Notes on Sandwich Construction

01 Jun 1949-Aircraft Engineering and Aerospace Technology (MCB UP Ltd)-Vol. 21, Iss: 6, pp 196-196
TL;DR: This is the type of panel which has received most attention from investigators and the critical load for local wrinkling of a single skin of thickness t is most simply expressed as as mentioned in this paper.
Abstract: THIS is the type of panel which has received most attention from investigators and the critical load for local wrinkling of a single skin of thickness t is most simply expressed as
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01 Jan 1967

7 citations

Journal ArticleDOI
TL;DR: In this article, an edge-supported sandwich panel with a honeycomb core tested in bending in two directions was constructed and the experimental data were compared with theoretical results obtained from equations proposed by the authors.
Abstract: Results are given for edge-supported sandwich panels with a honeycomb core tested in bending in two directions The experimental data are compared with theoretical results obtained from equations proposed by the authors It is established that in designing honeycomb panels for bending in two directions it is possible to treat the panel material as virtually isotropic in the plane of the laminations and to use the authors' equations for determining the deflections and the normal and shear stresses