Back to Search
Start Over
Single Ply and Multi-Ply Braided Composite Response Predictions Using Modified Subcell Approach.
- 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