Analysis of sandwich plates with a new layerwise formulation
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作者:
Maturi, D. A.
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King Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi ArabiaKing Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Maturi, D. A.
[1
]
Ferreira, A. J. M.
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King Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Univ Porto, Fac Engn, P-4100 Oporto, PortugalKing Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Ferreira, A. J. M.
[1
,2
]
Zenkour, A. M.
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King Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Kafrelsheikh Univ, Fac Sci, Dept Math, Kafr Al Sheikh 33516, EgyptKing Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Zenkour, A. M.
[1
,3
]
Mashat, D. S.
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King Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi ArabiaKing Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
Mashat, D. S.
[1
]
机构:
[1] King Abdulaziz Univ, Fac Sci, Dept Math, Jeddah 21589, Saudi Arabia
[2] Univ Porto, Fac Engn, P-4100 Oporto, Portugal
[3] Kafrelsheikh Univ, Fac Sci, Dept Math, Kafr Al Sheikh 33516, Egypt
In the analysis of sandwich laminates, where core and skin materials are so different, layerwise formulations should be adopted. In this paper the static and free vibration analysis of sandwich plates by the use of collocation with radial basis functions and using a new layerwise theory with independent rotations in each layer and thickness stretching was performed. With this formulation, transverse normal and shear deformations and stresses are accurately computed. The equations of motion were automatically implemented via a Unified Formulation and interpolated with radial basis functions. Finally composite laminated plate and sandwich plate examples were tested and discussed. (C) 2013 Elsevier Ltd. All rights reserved.