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Single Ply and Multi-Ply Braided Composite Response Predictions Using Modified Subcell Approach.

Authors :
Cater, Christopher R.
Xinran Xiao
Goldberg, Robert K.
Kohlman, Lee. W.
Source :
Journal of Aerospace Engineering; Sep2015, Vol. 28 Issue 5, p1-12, 12p
Publication Year :
2015

Abstract

In this work, the modeling of triaxially braided composites was explored through a subcell approach using an improved semianalytical discretization scheme. The unit cell of the braided composite was divided into four unique subcells, each approximated by a mosaic stacking of unidirectional composite plies and modeled through the use of layered-shell elements within the finite-element model. Two subcell discretization schemes were investigated: a model explicitly capturing pure matrix regions, and a model which absorbed pure matrix pockets into neighboring tow plies. Differences in the mesostructure between single-ply and multi-ply braid coupons were addressed through modifications to the subcell discretization. The absorbed matrix model simulated the unique out-of-plane deformations observed experimentally in single-ply tensile tests with acceptable moduli predictions. An investigation of single-shell versus multi-shell coupons for the analysis of multi-ply braids revealed the through-thickness modeling approach was found to have a significant effect on the apparent transverse modulus. Improved moduli predictions in both the axial and transverse directions were obtained by explicitly modeling braided plies with individual layers of shell elements. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
08931321
Volume :
28
Issue :
5
Database :
Complementary Index
Journal :
Journal of Aerospace Engineering
Publication Type :
Academic Journal
Accession number :
109020050
Full Text :
https://doi.org/10.1061/(ASCE)AS.1943-5525.0000445