Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression

In this paper, the skin−stringer separation phenomenon that occurs in stiffened composite panels under compression is numerically studied. Since the mode I fracture toughness and, consequently, the skin−stringer separation can be influenced by the fibre bridging phenomenon at the...

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Main Authors: Angela Russo, Andrea Sellitto, Salvatore Saputo, Valerio Acanfora, Aniello Riccio
Format: Article
Language:English
Published: MDPI AG 2019-06-01
Series:Materials
Subjects:
Online Access:https://www.mdpi.com/1996-1944/12/11/1856
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spelling doaj-153a4a725dc4460b8e0e34b67c63cfa62020-11-25T01:52:00ZengMDPI AGMaterials1996-19442019-06-011211185610.3390/ma12111856ma12111856Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under CompressionAngela Russo0Andrea Sellitto1Salvatore Saputo2Valerio Acanfora3Aniello Riccio4University of Campania “L. Vanvitelli”-Department of Engineering, via Roma, 29, 81031 Aversa, ItalyUniversity of Campania “L. Vanvitelli”-Department of Engineering, via Roma, 29, 81031 Aversa, ItalyUniversity of Campania “L. Vanvitelli”-Department of Engineering, via Roma, 29, 81031 Aversa, ItalyUniversity of Campania “L. Vanvitelli”-Department of Engineering, via Roma, 29, 81031 Aversa, ItalyUniversity of Campania “L. Vanvitelli”-Department of Engineering, via Roma, 29, 81031 Aversa, ItalyIn this paper, the skin−stringer separation phenomenon that occurs in stiffened composite panels under compression is numerically studied. Since the mode I fracture toughness and, consequently, the skin−stringer separation can be influenced by the fibre bridging phenomenon at the skin−stringer interface, in this study, comparisons among three different material systems with different fibre bridging sensitivities have been carried out. Indeed, a reference material system has been compared, in terms of toughness performance, against two materials with different degrees of sensitivity to fibre bridging. A robust numerical procedure for the delamination assessment has been used to mimic the skin−stringer separation. When analysing the global compressive behaviour of the stiffened panel, intra-laminar damages have been considered in conjunction with skin−stringer debonding to evaluate the effect of the fibre and matrix breakage on the separation between the skin and the stringer for the three analysed material systems. The latter are characterised by different toughness characteristics and fibre bridging sensitivities, resulting in a different material toughness.https://www.mdpi.com/1996-1944/12/11/1856debondingintra-laminar damagesdelaminationstiffened panel
collection DOAJ
language English
format Article
sources DOAJ
author Angela Russo
Andrea Sellitto
Salvatore Saputo
Valerio Acanfora
Aniello Riccio
spellingShingle Angela Russo
Andrea Sellitto
Salvatore Saputo
Valerio Acanfora
Aniello Riccio
Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression
Materials
debonding
intra-laminar damages
delamination
stiffened panel
author_facet Angela Russo
Andrea Sellitto
Salvatore Saputo
Valerio Acanfora
Aniello Riccio
author_sort Angela Russo
title Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression
title_short Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression
title_full Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression
title_fullStr Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression
title_full_unstemmed Cross-Influence between Intra-Laminar Damages and Fibre Bridging at the Skin–Stringer Interface in Stiffened Composite Panels under Compression
title_sort cross-influence between intra-laminar damages and fibre bridging at the skin–stringer interface in stiffened composite panels under compression
publisher MDPI AG
series Materials
issn 1996-1944
publishDate 2019-06-01
description In this paper, the skin−stringer separation phenomenon that occurs in stiffened composite panels under compression is numerically studied. Since the mode I fracture toughness and, consequently, the skin−stringer separation can be influenced by the fibre bridging phenomenon at the skin−stringer interface, in this study, comparisons among three different material systems with different fibre bridging sensitivities have been carried out. Indeed, a reference material system has been compared, in terms of toughness performance, against two materials with different degrees of sensitivity to fibre bridging. A robust numerical procedure for the delamination assessment has been used to mimic the skin−stringer separation. When analysing the global compressive behaviour of the stiffened panel, intra-laminar damages have been considered in conjunction with skin−stringer debonding to evaluate the effect of the fibre and matrix breakage on the separation between the skin and the stringer for the three analysed material systems. The latter are characterised by different toughness characteristics and fibre bridging sensitivities, resulting in a different material toughness.
topic debonding
intra-laminar damages
delamination
stiffened panel
url https://www.mdpi.com/1996-1944/12/11/1856
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