Published Date
Composites Part A: Applied Science and Manufacturing
March 2017, Vol.94:86–92, doi:10.1016/j.compositesa.2016.12.012
Abstract
An original experimental method is proposed to characterize the influence of matrix damage on the compressive strength of laminated composites in the fiber direction using tubes. These composite tubes have a dumbbell-shaped geometry so that rupture occurs in the specimen center without stress concentration. They can be constituted of unidirectional or woven plies aligned with the axial direction. First, a torsional cyclic load is applied in order to damage the matrix. This damage is measured at the tube scale via the reduction in shear modulus. Second, a compressive load is applied up to failure for various damage levels.
The method is applied to a woven carbon/epoxy material. Results show that the matrix damage affects significantly the compressive strength in the fiber direction. It is yet observed that longitudinal stiffness is not modified by damage. Finally, a simple model is proposed to describe this decrease of strength vs. matrix damage.
Keywords
A. Polymer-matrix composites (PMCs)
B. Strength
C. Damage mechanics
D. Mechanical testing
For further details log on website :
http://www.sciencedirect.com/science/article/pii/S1359835X16304390
Composites Part A: Applied Science and Manufacturing
March 2017, Vol.94:86–92, doi:10.1016/j.compositesa.2016.12.012
Received 1 May 2016. Revised 2 December 2016. Accepted 10 December 2016. Available online 19 December 2016.
An original experimental method is proposed to characterize the influence of matrix damage on the compressive strength of laminated composites in the fiber direction using tubes. These composite tubes have a dumbbell-shaped geometry so that rupture occurs in the specimen center without stress concentration. They can be constituted of unidirectional or woven plies aligned with the axial direction. First, a torsional cyclic load is applied in order to damage the matrix. This damage is measured at the tube scale via the reduction in shear modulus. Second, a compressive load is applied up to failure for various damage levels.
The method is applied to a woven carbon/epoxy material. Results show that the matrix damage affects significantly the compressive strength in the fiber direction. It is yet observed that longitudinal stiffness is not modified by damage. Finally, a simple model is proposed to describe this decrease of strength vs. matrix damage.
Keywords
Nomenclature
- matrix damage (–)
- longitudinal modulus of the ply (MPa)
- shear modulus of the ply (MPa)
- shear modulus of the matrix (MPa)
- non linear parameter (–)
- longitudinal strain (%)
- longitudinal stress (MPa)
- fiber volume fraction (–)
Subscript
- compression
- tension
Superscript
- undamaged material
- damaged material
- ⁎ Corresponding author at: Centre de Recherche de l’Armée de l’Air, École de l’air, B.A. 701, 13661 Salon-Air, France.
For further details log on website :
http://www.sciencedirect.com/science/article/pii/S1359835X16304390
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