Multi-Scale Experimental Characterization for LS-DYNA MAT213 Modeling of Composite Structures under High Strain Rate
Jackob Black, Ryan Premo, Robert K. Goldberg, Trenton M. Ricks, Troy, Lyons, Han-Gyu Kim

TL;DR
This paper develops and characterizes a material model for simulating the high strain rate response of a specific composite material in LS-DYNA, using multi-scale experiments and digital image correlation techniques.
Contribution
It introduces a multi-scale experimental approach to accurately characterize material parameters for the MAT213 model of a composite under dynamic loading.
Findings
Successful multi-scale testing method for transverse strains
Reliable stress-strain data obtained via digital image correlation
Enhanced material model parameters for composite under high strain rates
Abstract
Aerospace structures often experience high strain rate events such as ballistic impact, crash, or crush. A material model has been developed that enhances the capability to simulate the dynamic response of composite materials under these loading conditions. The material model has been implemented into the commercially available transient dynamic finite element code LS-DYNA as MAT213. The model can simulate the nonlinear deformation, damage, and failure that takes place in a composite under dynamic loading conditions. The specific goal of this work is to characterize the MAT213 input for the representative material. The specific composite material being examined consists of T700G unidirectional carbon fibers and a low-melt PolyArylEtherKetone (LMPAEK) thermoplastic resin system. It is formally referred to as Toray TC1225 LMPAEK T700G. As the initial part of this work, this paper is…
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Taxonomy
TopicsHigh-Velocity Impact and Material Behavior · Mechanical Behavior of Composites · Structural Response to Dynamic Loads
