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Article

The Effect of Continuous Carbon Fiber Reinforcement on 3D-Printed Honeycomb and Re-Entrant Sandwich Panels Subjected to In-Plane Compression

by
Andrei Nenciu
1,2,
Dragoş Alexandru Apostol
2 and
Dan Mihai Constantinescu
2,3,4,*
1
INCAS—National Institute for Aerospace Research “Elie Carafoli”, Bulevardul Iuliu Maniu 220, 061136 Bucharest, Romania
2
Department of Strength of Materials, National University of Science and Technology POLITEHNICA Bucharest, Splaiul Independenţei 313, 060042 Bucharest, Romania
3
Institute of Solid Mechanics of the Romanian Academy, Str. Constantin Mille 15, 010141 Bucharest, Romania
4
Technical Sciences Academy of Romania, Bulevardul Dacia 26, 030167 Bucharest, Romania
*
Author to whom correspondence should be addressed.
Materials 2025, 18(24), 5594; https://doi.org/10.3390/ma18245594
Submission received: 10 November 2025 / Revised: 2 December 2025 / Accepted: 10 December 2025 / Published: 12 December 2025
(This article belongs to the Special Issue Novel Materials for Additive Manufacturing)

Abstract

This study examines the in-plane compression behavior of sandwich panels produced with additive manufacturing. This study focuses on two types of honeycomb unit cell topologies with larger dimensions: a hexagonal one and a re-entrant one. For each panel geometry, two material configurations were examined: Onyx (a nylon-based composite) and Onyx reinforced with 10% continuous carbon fibers (CCFs) by mass. The objective was to assess the influence of fiber reinforcement on the mechanical performance and deformation response of the panel structures. In-plane compression tests were conducted to determine the stiffness, strength, and failure modes of the specimens. Additionally, the digital image correlation (DIC) technique was used to capture full-field strain distributions and analyze local deformation mechanisms during loading. The results revealed distinct mechanical responses between the two geometries: the re-entrant structure exhibited auxetic behavior and enhanced energy absorption characteristics. Although reinforced honeycomb panels have an average load capacity that is 35% higher, they fail at a displacement that is approximately 55% smaller compared to unreinforced panels. Despite accounting for only 25% of the total number of layers and 10% of the panel’s mass, the reinforcement achieved superior strength. Re-entrant panel testing showed a 25% force increase in favor of the reinforced variant. They fail at a displacement that is 36.5% greater than that of reinforced honeycombs. This demonstrates a more compliant response while also maintaining 4.9% greater strength, indicating the superior behavior of auxetic reinforced sandwich panels. Introducing CCF reinforcement increased the load-bearing capacity and reduced localized strain concentrations without altering the overall deformation pattern. These findings suggest that enhancing materials can increase the strength and flexibility of 3D-printed re-entrant structures, providing valuable insights for lightweight design and optimized material use in structural applications.
Keywords: printed sandwich panels; honeycomb; re-entrant; continuous carbon fiber; in-plane compression; digital image correlation; energy absorption printed sandwich panels; honeycomb; re-entrant; continuous carbon fiber; in-plane compression; digital image correlation; energy absorption

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MDPI and ACS Style

Nenciu, A.; Apostol, D.A.; Constantinescu, D.M. The Effect of Continuous Carbon Fiber Reinforcement on 3D-Printed Honeycomb and Re-Entrant Sandwich Panels Subjected to In-Plane Compression. Materials 2025, 18, 5594. https://doi.org/10.3390/ma18245594

AMA Style

Nenciu A, Apostol DA, Constantinescu DM. The Effect of Continuous Carbon Fiber Reinforcement on 3D-Printed Honeycomb and Re-Entrant Sandwich Panels Subjected to In-Plane Compression. Materials. 2025; 18(24):5594. https://doi.org/10.3390/ma18245594

Chicago/Turabian Style

Nenciu, Andrei, Dragoş Alexandru Apostol, and Dan Mihai Constantinescu. 2025. "The Effect of Continuous Carbon Fiber Reinforcement on 3D-Printed Honeycomb and Re-Entrant Sandwich Panels Subjected to In-Plane Compression" Materials 18, no. 24: 5594. https://doi.org/10.3390/ma18245594

APA Style

Nenciu, A., Apostol, D. A., & Constantinescu, D. M. (2025). The Effect of Continuous Carbon Fiber Reinforcement on 3D-Printed Honeycomb and Re-Entrant Sandwich Panels Subjected to In-Plane Compression. Materials, 18(24), 5594. https://doi.org/10.3390/ma18245594

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