4.7 Article

Experimental and numerical studies on low-velocity impact of laminated C/SiC structures

Journal

COMPOSITE STRUCTURES
Volume 329, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2023.117765

Keywords

CMCs; 3D FE-PDM; Constitutive relation; Micro -CT; Impact

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In this paper, a new conceptual 3D FEPDM (Finite Element - Progressive Damage Method) is proposed to tackle the complex failure characteristics of laminated C/SiC composites. The 3D FE-PDM lies between the macro and meso scales and is validated through experiments on 2D C/SiC and 3D needled C/SiC. The method is able to predict damage initiation, evolution, and load-displacement curve with good convergence for low-velocity impact cases. It offers a solution to the technical challenge of solving complicated mechanics problems.
Laminated C/SiC(carbon fiber reinforced silicon carbide composites) has the complicated nature of composite failure which include cracks for void defects at the meso and micro scales, complex cracks propagation of tunnel cracks, matrix cracks, delaminations and fiber cracks, orthotropic, and pseudoplastic behavior. It has technical challenge to solve all of them for complicated-mechanics problems by using multi-scale methodology. This paper focused tackling it by a model that lies between macro and meso scales, and proposed a new conceptual 3D FEPDM(Finite Element - Progressive Damage Method). 3D FE-PDM was validated by the experiments of lowvelocity impact of 2D C/SiC and 3D needled C/SiC. Damage initiation and evolution were controlled by strain in order to preventing stress chaos which could occur as cracks leading local stress relief. The multi-linear constitutive relations were adopted in orthotropic directions. The coupled effects of stresses between in-plane and out-of-plane were computed by adding damage coefficients into stiffness matrix. Cohesive Zone Method was used for delamination. The PDM approach was introduced for the 3D elements for intralaminar and cohesive elements for the interfaces. A parametric inversion methodology was put forward to determine the model parameters iteratively by comparing simulation results with the load-time curves, damage CT details of the experiments. Validation implies that, with small number of parameters, 3D FE-PDM is able to predict damage initiation of each phase knee, damage evolution, and load-displacement curve with good convergence for the low-velocity impact case. 2D woven and 3D needled non-woven C/SiC both have impact energy threshold and different damage evolution types.

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