A COUPLED NONLINEAR BUCKLING AND PROGRESSIVE DAMAGE MODEL FOR COMPOSITE SHELL STRUCTURES

Basheer Younis; Vitaly Miroshnikov; Basheer Younis; Vitaly Miroshnikov

doi:10.30888/2663-5712.2026-35-01-098

A COUPLED NONLINEAR BUCKLING AND PROGRESSIVE DAMAGE MODEL FOR COMPOSITE SHELL STRUCTURES

Authors

Basheer Younis National Aerospace University “Kharkiv Aviation Institute https://orcid.org/0000-0002-5693-6954
Vitaly Miroshnikov National Aerospace University “Kharkiv Aviation Institute https://orcid.org/0000-0002-9491-0181

DOI:

https://doi.org/10.30888/2663-5712.2026-35-01-098

Keywords:

Composite shells, Nonlinear buckling, Progressive damage, CFRP, GFRP, Finite element modeling

Abstract

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 co

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Published

2026-01-30

How to Cite

Юніс, Б., & Мірошников, В. (2026). A COUPLED NONLINEAR BUCKLING AND PROGRESSIVE DAMAGE MODEL FOR COMPOSITE SHELL STRUCTURES. SWorldJournal, 1(35-01), 113–123. https://doi.org/10.30888/2663-5712.2026-35-01-098