The article presents an analytical theory for multilayered composite beams subjected to transverse uniformly distributed loads. The formulation is based on a layerwise model characterized by third-order approximation of the axial displacements and fourth-order approximation of the transverse displacements. The layerwise kinematical model is rewritten in terms of generalized variables. The beam equilibrium equations, expressed in terms of stress resultant, allow writing the boundary value governing problem. The layerwise fields are obtained by postprocessing steps. The main advantage is to ensure the accuracy level associated to the layerwise formulations preserving the computational efficiency of the equivalent-single-layer theories.

Alaimo, A., Davì, G., Milazzo, A., Orlando, C. (2017). Analytical solution for composite layered beam subjected to uniformly distributed load. MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 1-10 [10.1080/15376494.2016.1227512].

Analytical solution for composite layered beam subjected to uniformly distributed load

DAVI', Giuseppe;MILAZZO, Alberto;
2017-01-01

Abstract

The article presents an analytical theory for multilayered composite beams subjected to transverse uniformly distributed loads. The formulation is based on a layerwise model characterized by third-order approximation of the axial displacements and fourth-order approximation of the transverse displacements. The layerwise kinematical model is rewritten in terms of generalized variables. The beam equilibrium equations, expressed in terms of stress resultant, allow writing the boundary value governing problem. The layerwise fields are obtained by postprocessing steps. The main advantage is to ensure the accuracy level associated to the layerwise formulations preserving the computational efficiency of the equivalent-single-layer theories.
2017
Settore ING-IND/04 - Costruzioni E Strutture Aerospaziali
Alaimo, A., Davì, G., Milazzo, A., Orlando, C. (2017). Analytical solution for composite layered beam subjected to uniformly distributed load. MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 1-10 [10.1080/15376494.2016.1227512].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/10447/221441
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