A finite element unified formulation for composite laminates in bending considering progressive damage

被引:16
|
作者
Ferreira, Gregorio F. O. [1 ]
Almeida, Jose Humberto S., Jr. [2 ,3 ]
Ribeiro, Marcelo L. [1 ]
Ferreira, Antonio J. M. [4 ]
Tita, Volnei [1 ,4 ]
机构
[1] Univ Sao Paulo, Sao Carlos Sch Engn, Aeronaut Engn Dept, Sao Carlos, SP, Brazil
[2] Aalto Univ, Dept Mech Engn, Espoo, Finland
[3] Queens Univ Belfast, Sch Mech & Aerosp Engn, Adv Composites Res Grp, Belfast, Antrim, North Ireland
[4] Univ Porto, Fac Engn, Dept Mech Engn, Porto, Portugal
基金
巴西圣保罗研究基金会;
关键词
Unified formulation; Finite element modeling; Progressive damage analyses; Continuum damage mechanics (CDM); LOW-VELOCITY IMPACT; HIGHER-ORDER THEORY; PLATE THEORIES; PART I; MODEL; FAILURE; TUBES; THICK;
D O I
10.1016/j.tws.2021.108864
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This works proposes a novel approach to develop higher-order finite elements by taking progressive damage into account in the formulation. The approach is based on Carrera's unified formulation (CUF) while the damage model is based on continuum damage mechanics (CDM) principles, which is implemented as a UEL (User Element subroutine) written in FORTRAN and linked to Abaqus. The approach is assessed by simulating a plate under distributed and sinusoidal loads. Besides, a progressive damage analysis of a composite coupon under three-point bending is simulated, and the numerical predictions are compared against experimental results, showing good correlation. The main findings show that the implemented UEL is accurate and fast enough to predict progressive failure events and the in-plane damage mechanisms for composite laminates under bending loadings.
引用
收藏
页数:13
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