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Hybrid Dovetail Core Joints for Composite Sandwich Structures: Mechanical–Adhesive Splicing for Improved Strength and Toughness

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Title: Hybrid Dovetail Core Joints for Composite Sandwich Structures: Mechanical–Adhesive Splicing for Improved Strength and Toughness

Authors: Rawan Aqel, Patrick Severson, Rani Elhajjar

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Abstract: Composite sandwich structures are widely deployed in aerospace and transportation because of their high stiffness-to-weight ratio. However, when joining large sections, traditional straight adhesive splices often reduce strength and toughness, creating weak points in otherwise highperformance systems. This work introduces a hybrid dovetail splice that combines adhesive bonding with a mechanical interlock to improve load transfer and joint reliability in carbon fiber/aluminum honeycomb sandwich panels. Two dovetail geometries were fabricated and tested under four-point bending alongside conventional straight splices and control (no splice) specimens. The dovetail design integrates adhesive bonding with a bioinspired mechanical interlock, aiming to reduce stress concentrations at the core/splice interface. Parametric finite element models were also developed to evaluate the influence of dovetail height and angle on normal and shear stresses within the adhesive and core. Experimental results show that dovetail splices can substantially outperform conventional straight joints. Depending on configuration, ultimate strength increased by 13–51% and toughness improved by 2–35%. Dovetail Style A joints achieved the highest load-carrying capacity, while Style B provided superior toughness and energy absorption. The numerical results corroborated the experimental findings, demonstrating stress reductions in the splice material and adhesive/core interface, particularly for dovetails with tenon heights of 15–30 mm and angles of 70°–80°. This hybrid joining strategy demonstrates how mechanical interlocking can complement adhesive bonding to create stronger and more damage-tolerant joints in composite sandwich structures. The approach offers direct relevance to aerospace and transportation applications, where reducing failure risks at splice joints is critical to safety and performance.

References: [1] Y. Hirose et al., "The CFRP sandwich panel for aircraft nose structure," in Proceedings 23rd International Congress of Aeronautical Sciences, 2002. [2] [3] [4] [5] [6] [7] [8] [9] [10] [11] [12] [13] [14] [15] [16] L. J. Gibson and M. F. Ashby, Cellular Solids: Structure and Properties. Cambridge University Press, 1997. L. Tong, A. P. Mouritz, and M. Bannister, 3D fibre reinforced polymer composites. Elsevier, 2002. R. Aqel, P. Severson, and R. Elhajjar, "A dovetail core design for joints in composite sandwich structures," Composite Structures, vol. 327, p. 117700, 2024. W. Wang, N. N. Yang, X. L. Yao, and D. N. Fang, "Influence of core splice to the mechanical behavior of sandwich plate," in Materials Science Forum, 2015, vol. 813: Trans Tech Publ, pp. 220-239. A. Nettles, J. Jackson, and W. Guin, "Sandwich structure risk reduction in support of the payload adapter fitting," 2018. W. E. Guin and A. T. Nettles, "Effects of core splice joint width on the performance of composite san dwich structures with honeycomb core: An experimental study," (in en), Jnl of Sandwich Structures & Materials, vol. 24, no. 1, pp. 720-741, 2021/6/23/ 2021, doi: 10.1177/10996362211020413. V. Goyal, J. Rome, P. Schubel, D. Patel, and G. Steckel, "Predicting and measuring the strength reduction of sandwich structures with spliced foam cores," presented at the 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference20th AIAA/ASME/AHS Adaptive Structures Conference14th AIAA, 2012/4/23, 2012. [Online]. Available: http://dx.doi.org/10.2514/6.2012-1773. R. Aqel, P. Severson, and R. Elhajjar, "Experimental and Numerical Investigation of Core Splicing Configurations in an Advanced Composite Sandwich Structural System," Journal of Reinforced Plastics and Composites, vol. 42, no. 23-24, pp. 1242-1251, 2023, doi: 10.1177/07316844221150423. T. Tannert, F. Lam, and T. Vallée, "Structural performance of rounded dovetail connections: experimental and numerical investigations," European Journal of Wood and Wood Products, vol. 69, no. 3, pp. 471-482, 2011. S.-M. Park, H.-K. Noh, J. H. Lim, and Y.-H. Choi, "Numerical Investigation of the Progressive Failure Behavior of the Composite Dovetail Specimens under a Tensile Load," Composites Research, vol. 34, no. 6, pp. 337-344, 2021. G. Jeong, M. Park, J. Park, and K. Hwang, "Predicting load-carrying capacity of dovetail connections using the stochastic finite element method," Wood and Fiber Science, pp. 430-439, 2012. H. D. Espinosa, A. L. Juster, F. J. Latourte, O. Y. Loh, D. Gregoire, and P. D. Zavattieri, "Tablet-level origin of toughening in abalone shells and translation to synthetic composite materials," Nature communications, vol. 2, no. 1, p. 173, 2011. A. International, "ASTM D7249/D7249M-16: Standard Test Method for Facing Properties of Sandwich Constructions by Long Beam Flexure," 2016. A. International, "ASTM C393/C393M-16: Standard Test Method for Core Shear Properties of Sandwich Constructions by Beam Flexure," 2016. P. C. Kohnke, ANSYS theory reference: release 5.5. ANSYS, Incorporated, 1998. 13 [17] A. Puck and H. Schürmann, "Failure analysis of FRP laminates by means of physically based phenomenological models," in Failure criteria in fibre-reinforced-polymer composites: Elsevier, 2004, pp. 832-876. [18] J. Qi, Y. Bao, J. Wang, L. Li, and W. Li, "Flexural behavior of an innovative dovetail UHPC joint in composite bridges under negative bending moment," Engineering Structures, vol. 200, p. 109716, 2019.

Conference: SAMPE 2026

Publication Date: 2026/04/27

SKU: 140

Pages: 14

Price: $28.00

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