A nonlinear finite element analysis of laminated shells with a damage model

被引：1

作者：

Santana, Pedro Buhrer ^{[1
]}

Ferreira, A. J. M. ^{[3
]}

Gomes, Herbert Martins ^{[1
]}

Tita, Volnei ^{[2
,3
]}

机构：

[1] Univ Fed Rio Grande do Sul, Dept Mech Engn, R Sarmento Leite 425,Room 202,2nd Floor, BR-90050170 Porto Alegre, RS, Brazil

[2] Univ Sao Paulo, Sao Carlos Sch Engn, Dept Aeronaut Engn, Ave Joao Dagnone 1100, BR-13563120 Sao Carlos, SP, Brazil

[3] Univ Porto, Fac Engn, Dept Mech Engn, Rua Dr Roberto Frias S-N, P-4200465 Porto, Portugal

来源：

COMPOSITES PART C: OPEN ACCESS | 2024年 / 15卷

关键词：

Finite element analysis; Nonlinear analysis; Damage analysis; Laminated shells; CONSTITUTIVE MODEL; COMPOSITES; BEHAVIOR; PLATES;

D O I：

10.1016/j.jcomc.2024.100505

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

This paper presents a study on the development and validation of a nonlinear finite element model for laminated composite shells, that considers a first-order shear deformation theory (FSDT) and an explicit through-thickness integration. The model integrates a meso-scale damage analysis that considers progressive matrix and fiber failures. The model is compared with envelopes of experimental curves extracted from 3-point bending test coupons and shows accurate predictions.

引用

页数：14

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