| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 254437 | Composite Structures | 2006 | 7 Pages |
Abstract
Analytical approximations are developed for the central deflection and edge stress induced by a uniform pressure load applied to a square flat top sandwich panel with a curved bottom skin. The accuracy of the solutions is investigated by making comparisons with the results obtained from a finite element model.
Keywords
Related Topics
Physical Sciences and Engineering
Engineering
Civil and Structural Engineering
Authors
K.R. Drake, S.C. Neo, A.P. Blackie,