Experimental and Numerical Analysis of Compression and Shear Wrinkling in Sandwich Beams under Three-Point Bending

Experimental and Numerical Analysis of Compression and Shear Wrinkling in Sandwich Beams under Three-Point Bending

Befekadu GASHE, Abdulmaliq ALAWODE, Samuel RIVALLANT, Bruno CASTANIE

Abstract. Wrinkling is a local instability that can greatly reduce the load-carrying capacity of lightweight sandwich structures. This paper presents an experimental and numerical study of the wrinkling response of sandwich beams tested under three-point bending, with particular attention to the difference between compression-driven and shear-driven wrinkling. The specimens were made of glass fiber-epoxy skins bonded to a PMI ROHACELL® foam core. Two different stacking configurations were selected so that one specimen was more likely to develop compression wrinkling, while the other was intended to promote shear wrinkling. The experimental campaign was carried out to capture both the overall structural response and the local deformation patterns associated with the onset of instability. Force and displacement were recorded throughout the tests, and Digital Image Correlation (DIC) was used to monitor the deformation field and follow the development of wrinkling in detail. Alongside the experiments, finite element analyses were performed in ABAQUS, and the numerical results were compared with the test observations as well as with available analytical predictions. The comparison showed a good agreement for the compression-wrinkling case, where the numerical model was able to reproduce the measured behaviour with reasonable accuracy. In contrast, for the shear-wrinkling case, the numerical simulations predicted higher wrinkling loads than those observed experimentally. This difference suggests that shear wrinkling is more sensitive to modelling choices, especially geometric imperfections and mesh discretization. Overall, the results show that combining experiments, numerical simulations, and analytical estimates is a useful approach for better understanding wrinkling mechanisms and improving the prediction of instability-related failure in sandwich structures.

Keywords
Sandwich, Three-Point Bending, Compression, Wrinkling, Shear Wrinkling, Finite Element Analysis, Digital Image Correlation

Published online 11/8/2026, 6 pages
Copyright © 2026 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA

Citation: Befekadu GASHE, Abdulmaliq ALAWODE, Samuel RIVALLANT, Bruno CASTANIE, Experimental and Numerical Analysis of Compression and Shear Wrinkling in Sandwich Beams under Three-Point Bending, Materials Research Proceedings, Vol. 73, pp 37-42, 2026

DOI: https://doi.org/10.21741/9781644904459-8

The article was published as article 8 of the book Mechanics of Advanced Materials and Structures

Content from this work may be used under the terms of the Creative Commons Attribution 3.0 license. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.

References
[1] A. Petras and M. P. F. Sutcliffe, “Failure mode maps for honeycomb COMPOSITE STRUCTURES sandwich panels,” 1999.
[2] I. M. Daniel, E. E. Gdoutos, I. M. Daniel, R. R. Mccormick, and E. E. Gdoutos, “Failure Modes of Composite Sandwich Beams,” 2009.
[3] L. Léotoing, S. Drapier, and A. Vautrin, “First applications of a novel unified model for global and local buckling of sandwich columns,” 2002.
[4] E. E. Gdoutos, I. M. Daniel, K.-A. Wang, and R. R. Mccormick, “Compression facing wrinkling of composite sandwich structures,” 2002. [Online]. Available: www.elsevier.com/locate/mechmat
[5] N. J. HOFF and S. E. MAUTNER, “Bending and Buckling of Sandwich Beams,” Journal of the Aeronautical Sciences, vol. 15, no. 12, pp. 707–720, Dec. 1948. https://doi.org/10.2514/8.11699
[6] S. Yusuff, “Theory of Wrinkling in Sandwich Construction,” The Journal of the Royal Aeronautical Society, vol. 59, no. 529, pp. 30–36, Jan. 1955. https://doi.org/10.1017/s0368393100131761
[7] H. G. ALLEN, “WRINKLING AND OTHER FORMS OF LOCAL INSTABILITY,” in Analysis and Design of Structural Sandwich Panels, Elsevier, 1969, pp. 156–189. https://doi.org/10.1016/b978-0-08-012870-2.50012-2
[8] G. S. Gough, C. F. Elam, G. H. Tipper, and N. A. De Bruyne, “The Stabilisation of a Thin Sheet by a Continuous Supporting Medium,” The Journal of the Royal Aeronautical Society, vol. 44, no. 349, pp. 12–43, Jan. 1940. https://doi.org/10.1017/s036839310010495x
[9] V. Birman and C. W. Bert, “Wrinkling of composite-facing sandwich panels under biaxial loading,” Journal of Sandwich Structures and Materials, vol. 6, no. 3, pp. 217–237, May 2004. https://doi.org/10.1177/1099636204033643
[10] M. Ginot, C. Bouvet, B. Castanié, M. D’Ottavio, J. Serra, and N. Mahuet, “Local buckling on large sandwich panels applied to light aviation: Experimental and computation dialogue,” Int. J. Solids Struct., vol. 268, Apr. 2023. https://doi.org/10.1016/j.ijsolstr.2023.112170
[11] L. Fagerberg and D. Zenkert, “Effects of anisotropy and multiaxial loading on the wrinkling of sandwich panels,” Journal of Sandwich Structures and Materials, vol. 7, no. 3, pp. 177–194, May 2005. https://doi.org/10.1177/109963205048525
[12] L. Fagerberg and D. Zenkert, “Imperfection-induced wrinkling material failure in sandwich panels,” Journal of Sandwich Structures and Materials, vol. 7, no. 3, pp. 195–219, May 2005. https://doi.org/10.1177/1099636205048526
[13] B. Gashe, A. Alawode, S. Rivallant, and B. Castanié, “Shear and Compression Wrinkling Experimental Analysis with a Sandwich Beam Submitted to Three-Point Bending,” Materials, vol. 18, no. 18, Sep. 2025. https://doi.org/10.3390/ma18184286
[14] J. Susainathan, F. Eyma, E. DE Luycker, A. Cantarel, and B. Castanie, “Numerical modeling of impact on wood-based sandwich structures,” Mechanics of Advanced Materials and Structures, vol. 27, no. 18, pp. 1583–1598, Sep. 2020. https://doi.org/10.1080/15376494.2018.1519619
[15] M. Ginot, C. Bouvet, B. Castanié, J. Serra, and N. Mahuet, “Local buckling on large sandwich panels used in light aviation: Experimental setup and failure scenarios,” Compos. Struct., vol. 304, Jan. 2023. https://doi.org/10.1016/j.compstruct.2022.116439
[16] B. CASTANIE, C. BOUVET, and M. Ginot, “Review of composite sandwich structure in aeronautic applications,” Aug. 01, 2020, Elsevier B.V. doi: 10.1016/j.jcomc.2020.100004