4.7 Article

Experimental investigation on the effects of fabric architectures on mechanical and damage behaviors of carbon/epoxy woven composites

Journal

COMPOSITE STRUCTURES
Volume 257, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2020.113366

Keywords

Woven fabric composite; Crimp ratio; Mechanical behavior; Damage

Funding

  1. Ford Motor Company
  2. U.S. Department of Energy's Office of Energy Efficiency and Renewable Energy (EERE) [DE-EE0006867]
  3. Clemson University [P20 GM121342]

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The study investigates the mechanical behaviors and damage evolutions of carbon/epoxy woven fabric composites with different geometries under tensile loading. It is found that the crimp ratio is a critical factor governing mechanical properties, with composites having smaller crimp ratios showing quasi-linear stress-strain curves with higher elastic modulus and strength. The study also reveals that regardless of fabric pattern, the elastic modulus, strength, and damage initiation are linearly correlated with the crimp ratio.
The mechanical behaviors and damage evolutions of carbon/epoxy woven fabric composites with three different geometries, i.e., one plain weave and two twill weave patterns with different areal densities, are studied under tensile loading. The effects of weave patterns on mechanical properties are investigated by monotonic and cyclic tension tests. Remarkable variations in stress-strain curve, Poisson's ratio, residual strain and strain map exist in the three composites. Crimp ratio is found to be a critical factor to govern the mechanical properties. With smaller crimp ratio, a quasi-linear stress-strain curve with higher elastic modulus and strength is observed. The stress-strain curves of composites with higher crimp ratio contain transition stages with significant tangent modulus degradation. Elastic modulus, strength and damage initiation are all correlated with the crimp ratio linearly regardless of the fabric pattern. Dramatic nonlinear evolution in Poisson's ratio occurs in the composite with higher crimp ratio. Cyclic tension results indicate that the residual strain is a more appropriate damage indicator than the unloading elastic modulus. Microstructure examination shows that damage developments are essentially related to the fabric geometry, and result in various mechanical behaviors. This study provides important insights into the geometry-deformation mechanism-mechanical property relationship of the woven composites.

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