A high-order theory for the analysis of circular cylindrical composite sandwich shells with transversely compliant core subjected to external loads
A high-order theory for the analysis of circular cylindrical composite sandwich shells with transversely compliant core subjected to external loads
A new model based on the high order sandwich panel theory is proposed to study the effect of external loads on the free vibration of circular cylindrical composite sandwich shells with transversely compliant core, including also the calculation of the buckling loads. In the present model, in contrast to most of the available sandwich plate and shell theories, no prior assumptions are made with respect to the displacement field in the core. Herein the displacement and the stress fields of the core material are determined through a 3D elasticity solution. The performance of the present theory is compared with that of other sandwich theories by the presentation of comparative results obtained for several examples encompassing different material properties and geometric parameters. It is shown that the present model produce results of very high accuracy, and it is suggested that the present model, which is based on a 3D elasticity solution for the core material, can be used as a benchmark in future studies of the free vibration and buckling of circular cylindrical composite sandwich shells with a transversely compliant core.
composite sandwich structures, transversely compliant core, free vibration, buckling, circular cylindrical shell, elasticity solution
2129-2142
Rahmani, O.
d54202c9-5980-4f37-aa24-9640c10d6b2f
Khalili, S.M.R.
551e374e-d499-40f9-a09e-0a77008345b4
Thomsen, O.T.
f3e60b22-a09f-4d58-90da-d58e37d68047
June 2012
Rahmani, O.
d54202c9-5980-4f37-aa24-9640c10d6b2f
Khalili, S.M.R.
551e374e-d499-40f9-a09e-0a77008345b4
Thomsen, O.T.
f3e60b22-a09f-4d58-90da-d58e37d68047
Rahmani, O., Khalili, S.M.R. and Thomsen, O.T.
(2012)
A high-order theory for the analysis of circular cylindrical composite sandwich shells with transversely compliant core subjected to external loads.
Composite Structures, 94 (7), .
(doi:10.1016/j.compstruct.2012.02.002).
Abstract
A new model based on the high order sandwich panel theory is proposed to study the effect of external loads on the free vibration of circular cylindrical composite sandwich shells with transversely compliant core, including also the calculation of the buckling loads. In the present model, in contrast to most of the available sandwich plate and shell theories, no prior assumptions are made with respect to the displacement field in the core. Herein the displacement and the stress fields of the core material are determined through a 3D elasticity solution. The performance of the present theory is compared with that of other sandwich theories by the presentation of comparative results obtained for several examples encompassing different material properties and geometric parameters. It is shown that the present model produce results of very high accuracy, and it is suggested that the present model, which is based on a 3D elasticity solution for the core material, can be used as a benchmark in future studies of the free vibration and buckling of circular cylindrical composite sandwich shells with a transversely compliant core.
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More information
e-pub ahead of print date: 10 February 2012
Published date: June 2012
Keywords:
composite sandwich structures, transversely compliant core, free vibration, buckling, circular cylindrical shell, elasticity solution
Organisations:
Engineering Mats & Surface Engineerg Gp
Identifiers
Local EPrints ID: 339256
URI: http://eprints.soton.ac.uk/id/eprint/339256
ISSN: 0263-8223
PURE UUID: 49dd74dd-05c7-48e8-9fd9-ba260ca0e445
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Date deposited: 25 May 2012 11:03
Last modified: 14 Mar 2024 11:12
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Contributors
Author:
O. Rahmani
Author:
S.M.R. Khalili
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