Ashoke Kumar Rath scite author profile

SummaryThe paper deals with the free transverse vibration and stability analysis of circular cylindrical composite panels. The panels are assumed to be composed of an arbitrary sequence of 0° and 90° layers. The non-dimensional vibration and buckling parameters are computed for simply-supported panels consisting of antisymmetric crossply graphite-epoxy laminates. The influence of the coupling between bending and extension, shear deformation, the panel curvature, and the aspect ratio are then discussed.

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Blends of Thermoplastic Polyesters: Sections 1–5

Nadkarni

Rath

2002

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Thermal post-buckling behaviour of laminated plates using a shear-flexible element based on coupled-displacement field

Thankam

Singh

Rao

et al. 2003

Composite Structures

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Acid, Alkali and Chloride Resistance of High Volume Fly Ash Concrete

Sahoo¹,

Das²,

Rath³

et al. 2015

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