Free Vibration Analysis of Thin-Walled Cylinders Reinforced With Longitudinal and Transversal Stiffeners

Author:

Carrera E.1,Zappino E.2,Filippi M.3

Affiliation:

1. Professor of Aerospace Structures and Aeroelasticity, e-mail:

2. e-mail:

3. e-mail:  Department of Aeronautic and Space Engineering, Politecnico di Torino, Corso Duca degli Abruzzi 24, 10129 Torino, Italy

Abstract

This paper deals with the dynamic analysis of reinforced thin-walled structures by means of refined one-dimensional models. Complex reinforced structures are considered which are built by using different components: skin, ribs, and stringers. Higher-order one-dimensional model based on the Carrera unified formulation (CUF) are used to model panels, stringer, and ribs by referring to a unique model. The finite element method (FEM) is used to provide a solution that deals with any boundary condition configuration. The structure is geometrically linear and the materials are isotropic and elastic. The dynamic behavior of a number of reinforced thin-walled cylindrical structures have been analyzed. The effects of the reinforcements (ribs and stringers) are investigated in terms of natural frequencies and modal-shapes. The results show a good agreement with those from commercial codes by reducing the computational costs in terms of degrees of freedom (DOFs).

Publisher

ASME International

Subject

General Engineering

Reference49 articles.

1. The Modified Compression-Field Theory for Reinforced Concrete Elements Subjected to Shear;ACI J.,1986

2. The Orthogonally Stiffened Plate Under Uniform Lateral Load;ASME J. Appl. Mech.,1940

3. The Analysis of a Flat Plated Grillage;Eur. Shipbuilding,1956

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