A COUPLED NONLINEAR BUCKLING AND PROGRESSIVE DAMAGE MODEL FOR COMPOSITE SHELL STRUCTURES
DOI:
https://doi.org/10.30888/2663-5712.2026-35-01-098Keywords:
Composite shells, Nonlinear buckling, Progressive damage, CFRP, GFRP, Finite element modelingAbstract
Thin-walled composite shells fabricated from carbon fiber–reinforced polymer (CFRP) and glass fiber–reinforced polymer (GFRP) are widely employed in aerospace structures due to their high specific stiffness and strength. Their structural response under coReferences
Jones, R.M. (1999). Mechanics of Composite Materials. 2nd ed., Taylor & Francis, New York.
Hashin, Z. (1980). Failure criteria for unidirectional fiber composites. Journal of Applied Mechanics, 47(2), 329–334.
Puck, A., & Schürmann, H. (2002). Failure analysis of FRP laminates by physically based phenomenological models. Composites Science and Technology, 62(12–13), 1633–1662.
Bisagni, C., & Cordisco, P. (2004). Post-buckling and collapse of CFRP composite cylindrical shells under axial compression. Composite Structures, 63(3–4), 499–514.
Koiter, W.T. (1945). On the stability of elastic equilibrium. PhD Thesis, Delft University of Technology.
Budiansky, B., & Hutchinson, J.W. (1966). A survey of some buckling problems. AIAA Journal, 4(9), 1505–1510.
ABAQUS Documentation (2024). ABAQUS Analysis User’s Guide. Dassault Systèmes.
Tsai, S.W., & Wu, E.M. (1971). A general theory of strength for anisotropic materials. Journal of Composite Materials, 5(1), 58–80.
Reddy, J.N. (2004). Mechanics of Laminated Composite Plates and Shells. 2nd ed., CRC Press.
Müzel, S.D., Degenhardt, R., & Bisagni, C. (2015). Buckling and imperfection sensitivity of composite cylindrical shells. Thin-Walled Structures, 94, 163–173.
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2026 Authors

This work is licensed under a Creative Commons Attribution 4.0 International License.


