4.6 Article

Effect of Strain Rate on the Transverse Tension and Compression Behavior of a Unidirectional Non-Crimp Fabric Carbon Fiber/Snap-Cure Epoxy Composite

Journal

MATERIALS
Volume 14, Issue 23, Pages -

Publisher

MDPI
DOI: 10.3390/ma14237314

Keywords

non-crimp fabric composites; snap-cure epoxy; split Hopkinson pressure bar; dynamic testing; pulse shaping; transverse tension; transverse compression

Funding

  1. Natural Sciences and Engineering Research Council of Canada (NSERC) through CRD [CRDPJ 507776-16]
  2. Ontario Advanced Manufacturing Consortium
  3. NSERC through a Canadian Graduate Scholarship (CGS)
  4. Honda Development and Manufacturing of America LLC
  5. Hexion Inc.
  6. Zoltek Corp.
  7. Laval International

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The study characterized the strain rate-dependent behavior of a UD-NCF carbon fiber/snap-cure epoxy composite loaded in the transverse direction under different strain rates, revealing higher tensile and compressive strength at high strain rates. Distinct localized fracture surfaces were observed for specimens tested at different strain rates, while the initial fracture plane orientation in transverse compression tests was found to increase with increasing strain rate.
The strain rate-dependent behavior of a unidirectional non-crimp fabric (UD-NCF) carbon fiber/snap-cure epoxy composite loaded along the transverse direction under quasi-static and dynamic conditions was characterized. Transverse tension and compression tests at quasi-static and intermediate strain rates were performed using hydraulic testing machines, while a split Hopkinson pressure bar (SHPB) apparatus was used for transverse compression tests at high strain rates. A pulse shaper was used on the SHPB apparatus to ensure dynamic equilibrium was achieved and that the test specimens deformed homogenously with a nearly constant strain rate. The transverse tensile strength at a strain rate of 16 s(-1) increased by 16% when compared to that at quasi-static strain rates, while distinct localized fracture surface morphology was observed for specimens tested at different strain rates. The transverse compressive yield stress and strength at a strain rate of 325 s(-1) increased by 94% and 96%, respectively, when compared to those at quasi-static strain rates. The initial fracture plane orientation for the transverse compression tests was captured with high-speed cameras and found to increase with increasing strain rate. The study provides an important data set for the strain rate-dependent response of a UD-NCF composite material, while the qualitative fracture surface observations provide a deeper understanding of the failure characteristics.

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