Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams

The debonding toughness between unidirectional glass fiber reinforced polymer face sheets and cellularic cores of sandwich structures is experimentally measured under static and fatigue loading conditions. The effect of various core geometries, such as regular honeycomb and closed-cell foams of two...

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Main Authors: Selvam, Vignesh, Sridharan, Vijay Shankar, Idapalapati, Sridhar
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2022
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Online Access:https://hdl.handle.net/10356/162826
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1628262022-11-10T07:49:54Z Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams Selvam, Vignesh Sridharan, Vijay Shankar Idapalapati, Sridhar School of Mechanical and Aerospace Engineering Engineering::Mechanical engineering Sandwich Composite Secondary Bonding The debonding toughness between unidirectional glass fiber reinforced polymer face sheets and cellularic cores of sandwich structures is experimentally measured under static and fatigue loading conditions. The effect of various core geometries, such as regular honeycomb and closed-cell foams of two relative densities on the adhesive interfacial toughness is explored using the single cantilever beam (SCB) testing method. The steady-state crack growth measurements are used to plot the Paris curves. The uniformity of adhesive filleting and the crack path was found to affect the interfacial toughness. The static Mode-1 interfacial toughness of high-density foam cores was witnessed to be maximal, followed by low-density honeycomb, high-density honeycomb, and low-density foam core. Similarly, the fatigue behavior of the low-density honeycomb core has the lowest crack growth rates compared to the other samples, primarily due to uniform adhesive filleting. Published version 2022-11-10T07:49:54Z 2022-11-10T07:49:54Z 2022 Journal Article Selvam, V., Sridharan, V. S. & Idapalapati, S. (2022). Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams. Journal of Composites Science, 6(2), 51-. https://dx.doi.org/10.3390/jcs6020051 2504-477X https://hdl.handle.net/10356/162826 10.3390/jcs6020051 2-s2.0-85124652463 2 6 51 en Journal of Composites Science © 2022 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https:// creativecommons.org/licenses/by/ 4.0/). application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering
Sandwich Composite
Secondary Bonding
spellingShingle Engineering::Mechanical engineering
Sandwich Composite
Secondary Bonding
Selvam, Vignesh
Sridharan, Vijay Shankar
Idapalapati, Sridhar
Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams
description The debonding toughness between unidirectional glass fiber reinforced polymer face sheets and cellularic cores of sandwich structures is experimentally measured under static and fatigue loading conditions. The effect of various core geometries, such as regular honeycomb and closed-cell foams of two relative densities on the adhesive interfacial toughness is explored using the single cantilever beam (SCB) testing method. The steady-state crack growth measurements are used to plot the Paris curves. The uniformity of adhesive filleting and the crack path was found to affect the interfacial toughness. The static Mode-1 interfacial toughness of high-density foam cores was witnessed to be maximal, followed by low-density honeycomb, high-density honeycomb, and low-density foam core. Similarly, the fatigue behavior of the low-density honeycomb core has the lowest crack growth rates compared to the other samples, primarily due to uniform adhesive filleting.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Selvam, Vignesh
Sridharan, Vijay Shankar
Idapalapati, Sridhar
format Article
author Selvam, Vignesh
Sridharan, Vijay Shankar
Idapalapati, Sridhar
author_sort Selvam, Vignesh
title Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams
title_short Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams
title_full Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams
title_fullStr Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams
title_full_unstemmed Static and fatigue debond resistance between the composite facesheet and Al cores under Mode-1 in sandwich beams
title_sort static and fatigue debond resistance between the composite facesheet and al cores under mode-1 in sandwich beams
publishDate 2022
url https://hdl.handle.net/10356/162826
_version_ 1749179241769992192