A failure model for the analysis of cross-ply Non-Crimp Fabric (NCF) composites under in-plane loading: Experimental & numerical study

Author:

Gouskos D.ORCID,Iannucci L.

Funder

Airbus UK

Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference76 articles.

1. Mechanical characterisation of glass- and carbon-fibre-reinforced composites made with non-crimp fabrics;Bibo;Compos Sci Technol,1997

2. Non-crimp fabric composites: manufacturing, properties and applications;Lomov,2011

3. Carbon-fibre non-crimp fabric laminates for cost-effective damage-tolerant structures;Bibo;Compos Sci Technol,1998

4. Asp LE. Competing factors in the selection and design of NCF architectures (processing/performance optimisation). Validation of local models by comparison with coupon data. Document No: FALCOM/WP4/SI/PM004, Deliverable D4.5-01, Report prepared under contract No: G4RD-CT-00694, 2005, p. 1–5.

5. The influence of the stitching pattern on the internal geometry, quasi-static and fatigue mechanical properties of glass fibre non-crimp fabric composites;Vallons;Composites A,2014

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