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2021
DOI: 10.1016/j.istruc.2020.11.067
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Free vibration analysis of a laminated composite sandwich plate with compressible core placed at the bottom of a tank filled with fluid

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Cited by 6 publications
(1 citation statement)
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“…To obtain the vibration solution of the MECFRPSS structure with a high accuracy, the classical laminate theory [ 48 ] (applied to the top and bottom panels) and the Reddy’s high-order shear deformation theory [ 49 ] (applied to the MREC) were adopted in this paper. As a result, the displacement field functions of the structure studied can be given as: where u c , v c , and w c are the displacement components of the panels; u h , v h , and w h are the displacement components of the MREC; u 0 , v 0 , and w 0 are the displacement components of the mid-plane of the structure along with the x , y , and z directions, respectively; and are the transverse normal rotation variables in the xoz and yoz planes.…”
Section: Analysis Of Bending and Vibration Resistancesmentioning
confidence: 99%
“…To obtain the vibration solution of the MECFRPSS structure with a high accuracy, the classical laminate theory [ 48 ] (applied to the top and bottom panels) and the Reddy’s high-order shear deformation theory [ 49 ] (applied to the MREC) were adopted in this paper. As a result, the displacement field functions of the structure studied can be given as: where u c , v c , and w c are the displacement components of the panels; u h , v h , and w h are the displacement components of the MREC; u 0 , v 0 , and w 0 are the displacement components of the mid-plane of the structure along with the x , y , and z directions, respectively; and are the transverse normal rotation variables in the xoz and yoz planes.…”
Section: Analysis Of Bending and Vibration Resistancesmentioning
confidence: 99%