Influence of fiber misalignment on the thermal buckling of variable angle tows laminated plates

Influence of fiber misalignment on the thermal buckling of variable angle tows laminated plates

Francesca Bracaglia

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Abstract. Variable Angle Tows (VAT) are a class of composite materials with curved fiber paths within the lamina plane. The tailoring of VATs is a virtue that increased the interest in their study. On the other hand, the same freedom in the fiber deposition inevitably leads to manufacturing defects like misalignment that impact the structure behavior, particularly buckling. The present study investigates the influence of manufacturing fiber misalignment on the thermal buckling response of a VAT composite square plate. The governing equations are obtained within the Carrera Unified Formulation (CUF) framework combined with Finite Element Method. The thermal problem is schematized with a decoupled approach, and the critical loads are evaluated through the solution of an eigenvalue problem. The results show how the presence of random misalignment influences both the buckling critical temperature and the buckling mode.

Keywords
Variable Angle Tow Composite, Misalignment Sensitivity, Thermal Buckling

Published online 6/1/2024, 5 pages
Copyright © 2024 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA

Citation: Francesca Bracaglia, Influence of fiber misalignment on the thermal buckling of variable angle tows laminated plates, Materials Research Proceedings, Vol. 42, pp 56-60, 2024

DOI: https://doi.org/10.21741/9781644903193-13

The article was published as article 13 of the book Aerospace Science and Engineering

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] Y. Zhu, Y. Qin, S. Qi, H. Xu, D. Liu, C. Yan. Variable angle tow reinforcement design for locally reinforcing an open-hole composite plate. Compos Struct, 2018;202:162–9.
[2] R. Vescovini, V. Oliveri, D. Pizzi, L. Dozio, P.M. Weaver. Pre-buckling and Buckling Analysis of Variable-Stiffness, Curvilinearly Stiffened Panels. Aerotec. Missili Spaz., 2020;99:43-52. https://doi.org/10.1007/s42496-019-00031-4
[3] A.V. Duran, N.A. Fasanella, V. Sundararaghavan, A.M. Waas. Thermal buckling of composite plates with spatial varying fiber orientations. Compos. Struct. (2015):124:228–35. https://doi.org/10.1016/j.compstruct.2014.12.065
[4] A. Pagani, and A.R. Sanchez-Majano. Stochastic stress analysis and failure onset of variable angle tow laminates affected by spatial fibre variations. Compos. Part C, 4 (2021): 100091. https://doi.org/10.1016/j.jcomc.2020.100091
[5] A.R. Sanchez-Majano, A. Pagani, M. Petrolo, C. Zhang. Buckling sensitivity of tow steered plates subjected to multiscale defects by high-order finite elements and polynomial chaos expansion. Materials 2021;14(11):2706. https://doi.org/10.3390/ma14112706
[6] N. Sharma, M. Nishad, D.K. Maiti, M.R. Sunny, B.N. Singh,. Uncertainty quantification in buckling strength of variable stiffness laminated composite plate under thermal loading. Compos. Struct. 275 (2021): 114486. https://doi.org/10.1016/j.compstruct.2021.114486
[7] E. Carrera, M. Cinefra, M. Petrolo, and E. Zappino. Finite Element Analysis of Structures through Unified Formulation. John Wiley & Sons, Chichester, West Sussex, UK, 2014.
[8] Z. Gu ̈rdal, B.F. Tatting, C.K. Wu. Variable stiffness composite panels: Effects of stiffness variation on the in-plane and buckling response. Composites Part A: Applied Science and Manufacturing, 39(5):911–922, May 2008.
[9] R.G. Ghanem, P.D. Spanos. Stochastic finite elements: a spectral approach. Dover Publications, Inc. 31 East 2nd Street, Mineola, N.Y. 11501