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Persistent Identifier
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perma:LIST.MM8E1F |
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Publication Date
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2026-07-06 |
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Title
| Design, manufacturing and testing of 3D printed variable-stiffness laminates for improved open-hole tensile behaviour [* Cross-Reference *] |
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Other Identifier
| https://doi.org/10.1016/j.addma.2023.103418
OpenAlex ID: https://openalex.org/W4317356579 |
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Author
| M. Iragi (Mondragon Unibertsitatea)Mondragon UnibertsitateaORCIDhttps://orcid.org/0000-0003-0229-1297
Cristina Pascual-González (Universidad Rey Juan Carlos, IMDEA Materials)Universidad Rey Juan Carlos, IMDEA MaterialsORCIDhttps://orcid.org/0000-0002-5838-1366
A. Esnaola (Mondragon Unibertsitatea)Mondragon UnibertsitateaORCIDhttps://orcid.org/0000-0003-0955-7545
U. Morales (Mondragon Unibertsitatea)Mondragon UnibertsitateaORCIDhttps://orcid.org/0000-0003-3036-5855
J. Aurrekoetxea (Mondragon Unibertsitatea)
C.S. Lopes (IMDEA Materials, Luxembourg Institute of Science and Technology)IMDEA Materials, Luxembourg Institute of Science and TechnologyORCIDhttps://orcid.org/0000-0003-4895-683X
L. Aretxabaleta (Mondragon Unibertsitatea)Mondragon UnibertsitateaORCIDhttps://orcid.org/0000-0002-9525-8340 |
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Point of Contact
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LIST QDKM (LIST) |
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Description
| Using 3D printing, continuous fibre can be steered in high curvature paths to create variable-stiffness (VS) laminates for applications such as notched laminates. In the present study, VS 3D printed continuous carbon fibre-reinforced thermoplastic laminates were designed, manufactured, and tested, to improve open-hole tensile behaviour. The design was carried out taking into account the current limitations of fused filament fabrication. A curvilinear function was used to describe the fibre trajectory of the VS laminates, which enabled the parametrisation of the design-oriented meso-scale model based on the finite element method. Conventional stress-based models for the estimation of damage initiation and ultimate failure strengths were adapted to the behaviour of the 3D printed material. These models successfully reproduced the fibre-dominated behaviour of the printed laminate. An as-manufactured model was also developed to analyse the effect of defects caused by manufacturing constraints. VS laminates presented higher strength than quasi-isotropic reference laminates for holes larger than ∅1mm, increasing to more than 30% for holes of ∅6mm or larger. In addition, this increase in strength combined with the slight decrease in stiffness significantly increased the energy absorbed up to failure (up to 200%). (2023-01-18)
***This entry has been automatically imported via OpenAlex by LIST harvest scripts. Please refer to https://doi.org/10.1016/j.addma.2023.103418 for the original and latest version of the publication*** (2026-07-01) |
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Subject
| Engineering; Physics |
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Keyword
| Materials science
Composite material
Ultimate tensile strength
Composite laminates
Stiffness
Fused filament fabrication
Curvature
Finite element method
Curvilinear coordinates
Fabrication
Isotropy
Structural engineering
3D printing
Composite number |
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Topic Classification
| Mechanical Behavior of Composites
Additive Manufacturing and 3D Printing Technologies
Structural Analysis and Optimization |
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Deposit Date
| 2023-01-18 |
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Data Type
| Article |
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Data Source
| Additive manufacturing |