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Dynamic response of composite sandwich plates subjected to initial stresses

Dynamic response of composite sandwich plates subjected to initial stresses
Dynamic response of composite sandwich plates subjected to initial stresses
The transient response of composite sandwich plates under initial stresses is investigated using a new finite element formulation. An assumed strain nine node shear deformable plate bending element with nine degrees of freedom per node is formulated based on a refined higher order theory. The higher order theory contains in-plane displacements that are expanded to include the higher order terms in the Taylor series expansion as a result of which there is no need for shear correction factors. The popular assumed strain concept is used to ensure that the developed nine node element passes the patch test and shows no signs of shear locking and spurious zero energy modes in the present finite element formulation. The Newmark time integration algorithm is used to solve the time dependent equations of the plate. Numerical results are presented to show the effects of initial stresses on deflection and stresses of composite sandwich plates.
b. buckling, c. finite element analysis (fea), assumed strain concept
1359-835X
1189-1205
Nayak, A.K.
20538650-e051-4cbc-803c-0398fc181aaf
Shenoi, R.A.
a37b4e0a-06f1-425f-966d-71e6fa299960
Moy, S.S.J.
d1b1f023-d32a-4b00-8a3f-17c89f91a51e
Nayak, A.K.
20538650-e051-4cbc-803c-0398fc181aaf
Shenoi, R.A.
a37b4e0a-06f1-425f-966d-71e6fa299960
Moy, S.S.J.
d1b1f023-d32a-4b00-8a3f-17c89f91a51e

Nayak, A.K., Shenoi, R.A. and Moy, S.S.J. (2006) Dynamic response of composite sandwich plates subjected to initial stresses. Composites Part A: Applied Science and Manufacturing, 37 (8), 1189-1205. (doi:10.1016/j.compositesa.2005.05.034).

Record type: Article

Abstract

The transient response of composite sandwich plates under initial stresses is investigated using a new finite element formulation. An assumed strain nine node shear deformable plate bending element with nine degrees of freedom per node is formulated based on a refined higher order theory. The higher order theory contains in-plane displacements that are expanded to include the higher order terms in the Taylor series expansion as a result of which there is no need for shear correction factors. The popular assumed strain concept is used to ensure that the developed nine node element passes the patch test and shows no signs of shear locking and spurious zero energy modes in the present finite element formulation. The Newmark time integration algorithm is used to solve the time dependent equations of the plate. Numerical results are presented to show the effects of initial stresses on deflection and stresses of composite sandwich plates.

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More information

Submitted date: 27 April 2005
Published date: August 2006
Keywords: b. buckling, c. finite element analysis (fea), assumed strain concept
Organisations: Civil Engineering & the Environment, Engineering Sciences

Identifiers

Local EPrints ID: 28856
URI: http://eprints.soton.ac.uk/id/eprint/28856
ISSN: 1359-835X
PURE UUID: 3ecb6eb3-a980-415b-8891-6be73c7e207e

Catalogue record

Date deposited: 08 May 2006
Last modified: 15 Mar 2024 07:27

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Contributors

Author: A.K. Nayak
Author: R.A. Shenoi
Author: S.S.J. Moy

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