Comparative fractographic analysis of composites adhesive joints subjected to mode I delamination

Published on Aug 1, 2019in Polymer Composites2.265
· DOI :10.1002/PC.25139
Núbia Nale Silveira3
Estimated H-index: 3
(Aeronáutica),
Rita de Cássia Mendonça Sales6
Estimated H-index: 6
+ 2 AuthorsMaurício Vicente Donadon15
Estimated H-index: 15
(Aeronáutica)
Source
Abstract
📖 Papers frequently viewed together
2008
3 Authors (Carl C. M. Wu, ..., Todd L. Jessen)
1 Citations
2018
1 Citations
References24
Newest
#1Camila Belo Gomes Brito (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 2
#1Camila Belo Gomes Brito (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 1
Last. Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
view all 6 authors...
7 CitationsSource
#1Jared Tracy (Stanford University)H-Index: 6
#2Yikai Yin (Stanford University)H-Index: 1
Last. Reinhold H. Dauskardt (Stanford University)H-Index: 67
view all 6 authors...
Abstract Adhesively bonding composite components is a reliable alternative to conventional joining processes that minimizes part weight and reduces fabrication costs. Regarding performance and reliability, of particular interest is developing adherend surface treatments that enhance adhesion of the joint interfaces in aggressive chemical environments. Using fracture mechanics-based adhesion metrologies, critical and subcritical crack growth were evaluated for several peel-ply-treated, adhesively...
4 CitationsSource
#1Rita de Cássia Mendonça Sales (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 6
Last. Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
view all 7 authors...
The increasing use of composite in the aircraft industry has raised the interest for a better understanding of the failure process in these materials, which can be also influenced by the manufacturing process of the laminate. Some materials used in vacuum assisted resin transfer molding process have been studied in the open literature but very few data have been published for resin transfer molding-6 epoxy based laminates, in particular studies showing the influence of the temperature on the int...
6 CitationsSource
#1S. Budhe (CEFET-MG: Centro Federal de Educação Tecnológica de Minas Gerais)H-Index: 12
#2Mariana D. Banea (CEFET-MG: Centro Federal de Educação Tecnológica de Minas Gerais)H-Index: 33
Last. L.F.M. da Silva (Faculdade de Engenharia da Universidade do Porto)H-Index: 24
view all 4 authors...
Abstract Continuing interest and more developments in recent years indicated that it would be useful to update Banea and da Silva paper entitled “Adhesively bonded joints in composite materials: an overview”. This paper presents an updated review of adhesively bonded joints in composite materials, which covers articles published from 2009 to 2016. The main parameters that affect the performance of bonded joints such as surface treatment, joint configuration, geometric and material parameters, fa...
223 CitationsSource
#1G. Borstnar (University of Southampton)H-Index: 4
#2Mark Mavrogordato (University of Southampton)H-Index: 18
Last. S.M. Spearing (University of Southampton)H-Index: 55
view all 5 authors...
With recent advances in computational resources and the development of arbitrary cracking methods, such as the Augmented Finite Element Method (A-FEM), more complex simulations can now be represented featuring multiple interacting cracks. It has been established that Mode I crack propagation in particle-toughened interlayers within some toughened Carbon Fibre Reinforced Polymer (CFRP) laminates involves a discontinuous process zone, rather than a distinct crack tip. This results from multiple cr...
12 CitationsSource
#1Thomas Löbel (DLR: German Aerospace Center)H-Index: 3
#2Dirk Holzhüter (DLR: German Aerospace Center)H-Index: 5
Last. Christian Hühne (Braunschweig University of Technology)H-Index: 22
view all 4 authors...
Abstract Based on the experience in the past and the occurrence of in-service damages, the authorities restrict today the application of adhesive bonding of composite structures for aircraft applications. However, certification limitations can be overcome if occurring disbonds within a bond are stopped by implemented design features, so-called disbond stopping features. Consequently, a novel bondline architecture for bonded composite joints is proposed. By implementing a distinct rather ductile ...
23 CitationsSource
#1I.S. Floros (University of Patras)H-Index: 1
#2Konstantinos Tserpes (University of Patras)H-Index: 21
Last. T. Löbel (DLR: German Aerospace Center)H-Index: 1
view all 3 authors...
Abstract The fracture behavior of composite bonded joints subjected to mode-I, mode-II and mixed-mode I + II loading conditions was characterized by mechanical testing and numerical simulation. The composite adherents were bonded using two different epoxy adhesives; namely, the EA 9695 film adhesive and the mixed EA 9395-EA 9396 paste adhesive. The fracture toughness of the joints was evaluated in terms of the critical energy release rate. Mode-I tests were conducted using the double-cantilever ...
44 CitationsSource
#1Mikko Kanerva (Aalto University)H-Index: 12
#2Olli Saarela (Aalto University)H-Index: 11
Abstract This paper reviews existing literature related to the peel ply surface treatment of composite materials. A peel ply fabric is used as a removable layer in a composite lay-up and ripped off to modify the surface for adhesive bonding. A peel ply can affect the elemental composition of a surface and it is possible to distinguish between either a polyester or a polyamide peel ply treatment for a specific composite system and application. However, consistent and generalised relationships bet...
67 CitationsSource
#1M.R. Gude (URJC: King Juan Carlos University)H-Index: 13
#2Silvia G. Prolongo (URJC: King Juan Carlos University)H-Index: 24
Last. Alejandro Ureña (URJC: King Juan Carlos University)H-Index: 33
view all 3 authors...
Abstract The effect of water absorption on the strength of single lap adhesive joints subjected to accelerated hygrothermal ageing (55 °C, 95% relative humidity, 800 h) was analysed. Two different variables were studied: the surface treatment of the carbon fibre/epoxy laminates (peel ply, grit blasting and atmospheric pressure plasma) and the addition of carbon nanofillers (0.5 wt% nanofibres and 0.25 wt% nanotubes) to the epoxy adhesive. The joint strength and the failure mode of the joints wer...
25 CitationsSource
#1Min-Gyu Song (Gyeongsang National University)H-Index: 2
#2Jin-Hwe Kweon (Gyeongsang National University)H-Index: 23
Last. Tae-Joo Lee (Korea Aerospace Industries)H-Index: 3
view all 7 authors...
The present paper experimentally addresses the effect of manufacturing methods on the strength of composite bonded joints. A total of 391 specimens, manufactured by four different fabrication methods, were tested. For each method, various overlap lengths, adherend thicknesses and lay-up patterns were examined. The failure strength was higher in thicker adherend joints and lower in specimens with larger overlap length. Results showed that the secondary bonded joints had higher strength than the c...
40 CitationsSource
Cited By2
Newest
#1Arief Yudhanto (KAUST: King Abdullah University of Science and Technology)H-Index: 14
#2Marco Alfano (UW: University of Waterloo)H-Index: 2
Last. Gilles Lubineau (KAUST: King Abdullah University of Science and Technology)H-Index: 39
view all 3 authors...
Abstract A considerable weight reduction in thermoset-based composite is attained by replacing mechanical fasteners with a structural adhesive during the secondary bonding. The quality of this adhesively-bonded joint greatly depends on the surface preparation strategies applied to the mating composites as they influence the surface morphology, topography, interface composition, and mechanical performance of the adherend-adhesive interphase. We reviewed the recent progress of surface preparation ...
Source
Abstract Adhesive bonding technologies exhibit several advantages over conventional mechanical fasteners which include lower weight, reduced stress concentration in the adherents and excellent fatigue properties allowing the design of smooth surface contour and damage tolerant aerostructures. The overall structural performance of the composite joint depends on several factors related to the manufacturing process, such as surface preparation procedure, adhesive type, aging effects, and deficiency...
2 CitationsSource