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A Numerical–Analytical Approach for the Preliminary Design of Thin-Walled Cylindrical Shell Structures with Elliptical Cut-Outs

Authors :
Angela Russo
Andrea Sellitto
Salvatore Saputo
Valerio Acanfora
Aniello Riccio
Source :
Aerospace, Vol 6, Iss 5, p 52 (2019)
Publication Year :
2019
Publisher :
MDPI AG, 2019.

Abstract

The presence of cut-outs within thin-walled shell structures is unavoidable, holes being needed for the passage of electrical cables, fuel, or just to reduce the weight of the components. Nevertheless, the high stress concentration can lead to a premature collapse of the structure. For this reason, the preliminary design of cylindrical shell structures with holes needs a profound knowledge of the stress distribution for different loading conditions and constraints. In this paper, a parametric study of a fiber-reinforced composite shell cylinder with an elliptical cut-out has been performed. Three different loading conditions were analyzed: Tension, bending, and torsion. Ansys® script, capable of easily generating and analyzing different geometrical configurations, was used to study the dependence of the geometry on the stress distribution near the cut-out. Finally, graphical and analytical relationships were tentatively extrapolated from numerical results, aimed at linking the geometrical parameters of the cut-out to the maximum stress near the cut-out.

Details

Language :
English
ISSN :
22264310
Volume :
6
Issue :
5
Database :
Directory of Open Access Journals
Journal :
Aerospace
Publication Type :
Academic Journal
Accession number :
edsdoj.797e27bc4bfa438ba73f54be4a27e8ed
Document Type :
article
Full Text :
https://doi.org/10.3390/aerospace6050052