4.7 Article

Linear-Nonlinear Stiffness Responses of Carbon Fiber-Reinforced Polymer Composite Materials and Structures: A Numerical Study

Journal

POLYMERS
Volume 13, Issue 3, Pages -

Publisher

MDPI
DOI: 10.3390/polym13030344

Keywords

CFRP composites; material behavior; structural analysis; stiffness response; damage mechanics; finite element method

Funding

  1. Universiti Putra Malaysia [GP/2018/9635100]
  2. Ministry of Education, Youth, and Sports of the Czech Republic [CZ.02.1.01/0.0/0.0/16_025/0007293]
  3. European Union (European Structural and Investment Funds Operational Program Research, Development, and Education) [CZ.02.1.01/0.0/0.0/16_025/0007293]
  4. Research University Grant from Universiti Teknologi Malaysia [HIR-Q.J130000.2424.04G40]
  5. Ministry of Higher Education (MOHE)
  6. Universiti Teknologi Malaysia

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This study explores the linear-nonlinear stiffness behavior of CFRP composites at material and structural levels, revealing a direct dependency of material-level stiffness response on elastic properties, while structural stiffness behavior is influenced by configuration, geometry, and lay-ups in addition to mechanical properties of CFRP composites.
The stiffness response or load-deformation/displacement behavior is the most important mechanical behavior that frequently being utilized for validation of the mathematical-physical models representing the mechanical behavior of solid objects in numerical method, compared to actual experimental data. This numerical study aims to investigate the linear-nonlinear stiffness behavior of carbon fiber-reinforced polymer (CFRP) composites at material and structural levels, and its dependency to the sets of individual/group elastic and damage model parameters. In this regard, a validated constitutive damage model, elastic-damage properties as reference data, and simulation process, that account for elastic, yielding, and damage evolution, are considered in the finite element model development process. The linear-nonlinear stiffness responses of four cases are examined, including a unidirectional CFRP composite laminate (material level) under tensile load, and also three multidirectional composite structures under flexural loads. The result indicated a direct dependency of the stiffness response at the material level to the elastic properties. However, the stiffness behavior of the composite structures depends both on the structural configuration, geometry, lay-ups as well as the mechanical properties of the CFRP composite. The value of maximum reaction force and displacement of the composite structures, as well as the nonlinear response of the structures are highly dependent not only to the mechanical properties, but also to the geometry and the configuration of the structures.

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