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FEM Simulation of a FML Full Scale Aeronautic Panel Undergoing Static Load | OMICS International | Abstract
ISSN: 2169-0316

Industrial Engineering & Management
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Research Article

FEM Simulation of a FML Full Scale Aeronautic Panel Undergoing Static Load

R. Citarella1*, E Armentani2, R Sepe2 and F Caputo3

1 Department of Industrial Engineering, University of Salerno, Fisciano (SA), Italy

2 Department of Materials Engineering and Production, University of Naples, P.le V. Tecchio, 80–80125 Naples, Italy

3 Department of Industrial and Information Engineering, Second University of Naples, via Roma 29 – 81031 Aversa (CE) Italy

*Corresponding Asuthor:
R Citarella
Department of Industrial Engineering
University of Salerno, Fisciano (SA), Italy
E-mail: [email protected]

Received December 10, 2013; Accepted January 22, 2014; Published January 29, 2014

Citation: Citarella R, Armentani E, Sepe R, Caputo F (2014 FEM Simulation of a FML Full Scale Aeronautic Panel Undergoing Static Load. Ind Eng Manage 3:122. doi:10.4172/2169-0316.1000122

Copyright: © 2014 Citarella R, et al. This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.

Abstract

This paper concerns the numerical characterization of the static strength of a flat stiffened panel, designed as a fiber metal laminates (FML) and made of Aluminium alloy and Fiber Glass FRP. The panel is full scale and was tested under static loads, applied by means of an in house designed and built multi-axial fatigue machine. The static test is simulated by the Finite Element Method (FEM) in a three-dimensional approach. The strain gauge outcomes are compared with corresponding numerical results, getting a satisfactory correlation.

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