PG-EAM - Programa de Pós-Graduação em Engenharia Aeronáutica e Mecânica
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Artigo 2011

An experimental and numerical analysis for the post-buckling behavior of composite shear webs

Autores

de Almeida, Sérgio Frascino M.

Composite Structures , vol. 93 , no. 2 , pp. 465-473

ISSN: 02638223

16
Citações
3
Autores

Resumo

This paper presents a detailed experimental and numerical investigation on the structural behavior of stiffened composite panels subjected to in-plane shear loads. The experimental work includes the development of a test device for post-buckling analyses of laminated panels subjected to shear loads. The panels out-of-plane displacement field in the post-buckling regime was experimentally characterized using a non-contact 3-D optical device. A test procedure was proposed to obtain reliable and reproducible results. The following parameters were established: geometry and instrumentation of the specimens, test mechanisms, data acquisition procedures and analysis procedures for test data.The numerical objective of this work is to implement a modeling methodology for analysis of composite stiffened panels using finite elements. The proposed methodology takes into account large displacements and material nonlinearity effects by using a damage mechanics based progressive failure model.Preliminary results for tested specimens with the proposed configuration indicate that the stiffened composite shear webs have significant post-buckling strength. © 2010 Elsevier Ltd.

Palavras-chave

Composites Damage Finite elements Post-buckling

Ceramics and Composites (MATE) Civil and Structural Engineering (ENGI)
: Scopus
Última atualização: 2026-06-25
: 2-s2.0-79951517237
PII: S0263822310003004