Advanced numerical modeling of flexural response in axisymmetric CFRP composite laminates

Advanced numerical modeling of flexural response in axisymmetric CFRP composite laminates

Afsar HUSAIN, Sanan H. KHAN, Abdel Hamid I. MOURAD

Abstract. Axisymmetric carbon fiber reinforced polymer (CFRP) laminates are designed to achieve enhanced load-bearing efficiency and balanced mechanical performance under complex stress states. In this study, the flexural response of axisymmetric CFRP laminates is numerically investigated using two modeling approaches: a three-dimensional Hashin progressive damage model implemented through a user-defined VUMAT subroutine in Abaqus/CAE, and the built-in two-dimensional Hashin failure criterion. The numerical predictions are validated against previously reported experimental results. The 3D Hashin model shows improved accuracy in predicting peak load and provides a more detailed representation of progressive damage mechanisms, including delamination initiation and matrix cracking, compared to the 2D model. These results further demonstrate the superior capability of three-dimensional damage models in capturing the complex flexural behavior of axisymmetric CFRP laminates.

Keywords
CFRP, Flexural Test, Finite Element Method, Abaqus, VUMAT, 3D Hashin Progressive Damage Model

Published online 6/20/2026, 7 pages
Copyright © 2026 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA

Citation: Afsar HUSAIN, Sanan H. KHAN, Abdel Hamid I. MOURAD, Advanced numerical modeling of flexural response in axisymmetric CFRP composite laminates, Materials Research Proceedings, Vol. 67, pp 300-306, 2026

DOI: https://doi.org/10.21741/9781644904176-41

The article was published as article 41 of the book Climate Action and Sustainability

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.

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