Multiscale Modeling of a Notched Coupon Test for Triaxially Braided Composites

Article Preview

Abstract:

Braided composites have been widely used in aerospace and automotive structures due to their light weight and high strength. Unlike metal or laminated composite material, the complex braided structure brings a lot of challenges when conducting numerical simulation. In this paper, a finite element analysis based meso-mechanical modeling for the two dimensional triaxially braided composite was developed. This mesoscale modeling method is capable of considering the detailed braiding geometry and architecture as well as the mechanical behavior of fiber tows, matrix and the fiber tow interface. Furthermore, a multiscale model combined both macroscale and mesoscale approaches and it is realized within LS-DYNA environment through Interface_components and Interface_linking. This combined multiscale modeling approach enables the full advantage of both the macroscale and mesoscale approaches, which can describe the details of local deformation and the global overall response features of the entire structure with the minimum computational expense. The evaluation and verification of the mesoscale approach and combined multiscale modeling method is through a notched coupon tensile tests conducted by Kohlman in both axial and transverse direction. The multiscale modeling method captures the response feature accurately so it has the ability to analyze large scale structures.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

172-179

Citation:

Online since:

March 2019

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2019 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] X. Li, W. K. Binienda, R.K. Goldberg, Finite Element Model for Failure Study of Two Dimensional Triaxially Braided Composite, Journal of Aersopsace Engineering, 2011, 24(2):170-180.

DOI: 10.1061/(asce)as.1943-5525.0000029

Google Scholar

[2] Ivanov DS, Baudry F, Van Den Broucke B, Lomov SV, Xie H, Verpoest I. Failure analysis of triaxial braided composite. Composites Science and Technology, 2009, 69(9):1372-1380.

DOI: 10.1016/j.compscitech.2008.09.013

Google Scholar

[3] C. R. Cater, X. Ran, et al. Single Ply and Multi-Ply Braided Composite Response Predictions Using Modified Subcell Approach. Journal of Aerospace Engineering, 2015, 28(5): 04014117.

DOI: 10.1061/(asce)as.1943-5525.0000445

Google Scholar

[4] B. Yang, Z. Wang, L. Zhou, et al. Experimental and Numerical Investigation of Interplay Hybrid Composites Based on Woven Fabrics and PCBT Resin Subjected to Low-velocity Impact, Composite Structure, 2015, 132(2015): 464-476.

DOI: 10.1016/j.compstruct.2015.05.069

Google Scholar

[5] X. Li, W. K. Binienda, Mesomechanical Model for Numerical Study of Two-Dimensional Triaxially Braided Composite, Journal of Engineering Mechanics, 2010, 136(11): 1366-1379.

DOI: 10.1061/(asce)em.1943-7889.0000181

Google Scholar

[6] C. Zhang, W. K. Binienda. A meso-scale finite element model for simulating free-edge effect in carbon/epoxy textile composite. Mechanics of Materials 76(2014): 1-19.

DOI: 10.1016/j.mechmat.2014.05.002

Google Scholar

[7] C. Zhang, N. Li, et al. Progressive damage simulation of triaxially braided composite using a 3D meso-scale finite element model. Composite Structures 125 (2015): 104-116.

DOI: 10.1016/j.compstruct.2015.01.034

Google Scholar

[8] Zifeng Nie, Advanced Mesomechanical Modeling of Triaxially Braided Composites for Dynamic Impact Analysis with Fialure, University of Akron, (2014).

Google Scholar

[9] Brina J. Blinzler, Systematic approach to simulating impact for triaxially braided composites. The University of Akron, (2012).

Google Scholar

[10] C. Zhang, W. K. Binienda, et al. Meso-scale failure modeling of single layer triaxial braided composite using finite element method. Composites Part A: Applied Science and Manufacturing 58 (2014): 36-46.

DOI: 10.1016/j.compositesa.2013.11.009

Google Scholar

[11] B. A. Bednarcyk, J. Arnold, MAC/GMC 4.0 User's Manuals, (2002).

Google Scholar

[12] LS-DYNA Keyword User's Manual, Volume II material models. 2018, Livermore Software Technology Corporation (LSTC).

Google Scholar

[13] C. R. Cater, X. Xiao. Experimental and Numerical Analysis of Triaxially Braided Composites Utilizing a Modified Subcell Modeling Approach. NASA/TM-2015-218814.

Google Scholar