Publications

Version: 1.0 Approved

LDO-ID 2022-02-25-12

Title Numerical investigation on the stringer termination debonding in tensile loaded hybrid metallic-CFRP stiffened aeronautical panel

Abstract

In this work, the stringer termination debonding on a tensile-loaded hybrid metallic-composite stiffened panel is numerically investigated. The analyzed structure consists of an omega-reinforced CFRP panel joined with a Z-reinforced aluminum plate. An initial debonding is considered between the composite skin and the omega stringers, and the delamination propagation is investigated as the applied load increases. Subsequently, additional sub-components are introduced to mitigate the delamination propagation. The numerical results are compared and critically discussed.

Authors Sellitto Andrea, Saputo Salvatore, Russo Angela, Innaro Vincenzo, Riccio Aniello, Acerra Francesco, Russo Salvatore

Type Paper for Specialistic Magazine

Media Materialstoday: proceedings (Elsevier B.V., Volume: 34, Part 1, February 2021)

Web site

https://digital-library.theiet.org/content/books/tr/pbtr030e

Anno 2021

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