An integrated computational materials engineering framework to analyze the failure behaviors of carbon fiber reinforced polymer composites for lightweight vehicle applications
Graphical abstract
Introduction
With the growing attention on energy conservation and environmental protection, lightweight design for automobiles is becoming increasingly attractive in the automotive industry. Generally speaking, material replacement, structural optimization, and application of new manufacturing technology can be adopted in the lightweight design process, among which material replacement is arguably the most effective approach [1]. Carbon fiber reinforced polymer (CFRP) composites, with a density of 1.55 g/cm3 and a tensile strength of up to 2000 MPa along the fiber direction, stand as one of the most promising classes of materials to replace the engineered metals for automotive structural components. In particular, chopped carbon fiber sheet molding compound (SMC) and woven composites have great potential in automotive manufacturing due to their excellent mechanical performance, moderate cost, and easier fabrication compared to unidirectional (UD) CFRP composites [[2], [3], [4]]. In order to fully exploit the potential of these CFRP composites, we need to target increasing the accessibility of CFRP component designs, improving the robustness of initial designs, and most importantly, reducing the development to deployment lead time of CFRP components. These targets will eventually help mitigate greenhouse gas emissions from passenger vehicles and improve national energy independence [5].
The typical material design (or replacement) cycle consists of appropriate material selection followed by component size, shape design, and optimization [6]. In woven and chopped SMC CFRP composites, material selection also involves the size of representative element selection at the microstructure level. For instance, changing the size and/or angle of fiber tows for woven composites or changing the chip orientation for SMC composites significantly alter the anisotropic behavior of the material as well as its failure mechanisms, which in turn influence failure strength and fracture toughness of the material [3]. Thus, material design is not only limited to the size and geometry of constituents but also closely connected to the microstructural design. Traditionally, characterization of materials is done by carrying out expensive and time-consuming material tests to establish stiffness (elastic modulus) as well as strength properties in all material coordinates. With the advancements in computational materials science and engineering as well as multi-scale modeling, the “validation through simulation” approach has been increasingly adopted to decrease the time and cost of applying new materials to automotive components. Integrated Computational Materials Engineering (ICME) is the integration of materials information captured through computational tools with engineering product performance analysis and manufacturing process simulation [7]. This concept was first described by the U. S. National Materials Advisory Board Committee in 2008. Since then, ICME has become a fast-growing discipline within materials science and engineering and has been successfully employed in the design of metallic metals [[8], [9], [10]]. Compared to advanced metallic systems, the CFRP composites have the unique features of anisotropic and heterogeneous multi-scale microstructures and even larger variations in the material properties induced by the unique injecting/compression molding processes. Currently, there still exist two major challenges in developing ICME tool for CFRP composites: (1) development of high fidelity computational models; and (2) integration of the validated models and computational tools into one automated workflow so that the material processing, microstructure, and component structure can be optimized simultaneously [11].
In line with the overarching goal of ICME to reduce the time and the cost in the discovery and development of novel CFRP composites structures, multi-scale computational models have been established and embraced in our previous work and those of other researchers [[12], [13], [14], [15], [16], [17], [18], [19], [20], [21], [22], [23], [24]]. A majority of those models deliver the concerned information embedded in equations and parameters from lower-scale simulations to higher-scale, which is termed as the bottom-up hierarchical approach [17]. These previous studies on multi-scale model development have addressed the first challenge to a large extent. The primary objective of the present work is to address the second challenge, i.e., to integrate the multi-scale computational models and demonstrate an ICME framework of CFRP composites for lightweight vehicles, with a particular focus on three types of widely-used thermoset epoxy based CFRP composites in structural parts: long fiber UD composites, chopped short fiber SMC composites, and woven composites.
Section snippets
Synopsis of ICME framework
In the ICME framework considered in the present work, the intrinsic relationship between material microstructure (i.e., the fiber volume fraction of UD CFRP composites, woven yarn angle, SMC chip orientation, and size, etc.) and the mechanical performance of CFRP composites will be systematically developed by a bottom-up multi-scale modeling approach with the aim of structural design and failure analysis. As shown in Fig. 1, we use a four-scale model to describe the cured CFRP composites:
Nano-scale model of the interphase region based on MDA
Down to the nano-scale level, the carbon fiber surface is quite rough, partially due to the treatments applied to the carbon fibers during the fiber manufacturing process [27]. In addition, there is a significant nano-confinement effect from the carbon fibers on matrix resins [[28], [29], [30]]. As a result, a submicron-thick interphase region exists between carbon fibers and the matrix, as shown schematically in Fig. 2(a). It has been demonstrated that the interphase property has a significant
UD RVE model and constitutive laws for constituents
For model development, a cross-section of the microstructure of the UD RVE model with cylindrical fibers randomly distributed in the matrix is obtained using an algorithm proposed by Melro et al. [34]. The average fiber diameter of 7 μm and fiber volume fraction () of 51.4% are utilized based on experimental material characterization. In addition to the fiber and matrix phase, the UD RVE model includes a finite thickness (~200 nm) interphase region adjacent to fibers, consistent with the
Chopped SMC and woven composites description
Chopped SMC and woven fabric composites are produced using the same DowAksa A42 carbon fiber and Dow thermoset epoxy as the UD CFRP composites. The fiber diameter and fiber volume fraction of chips for SMC as well as fiber tows (yarns) for woven are 7 μm and 51.4% respectively, which are the same as for UD CFRP composites.
For chopped SMC composites, long continuous UD prepregs are chopped into sections approximately 25 mm in length, which are then distributed onto a resin film to create an SMC
Macro-scale bending model of hat-section-shaped parts made of UD and woven CFRP composites
In this section, we use a hat-section-shaped part subjected to four-point bending load to demonstrate the final stage of the proposed bottom-up multi-scale ICME framework. The detailed geometry of the hat-section-shaped part is shown in Fig. 9(a). The UD CFRP hat-section-shaped part is made up of [0/90/90/0/0/0]s and [0/60/-60/0/60/-60]s layup with 12 layers (noted as UD 0–90 and UD 0–60, respectively), and the layups of woven CFRP hat-section-shaped part are [90/0/90/0]s and [45/-45/45/-45]s
Conclusions
This study presents a systematic investigation into the failure behaviors of UD, woven, and chopped SMC CFRP composites at different scales by developing an ICME framework with a bottom-up multi-scale modeling approach. The multi-scale models combine MDA at the nano-scale, UD RVE model at the micro-scale, chopped SMC, and woven RVE models at the meso-scale, and hat-section-shaped parts at the macro-scale. The major insights/conclusions are summarized below.
- (1)
At the nano-scale, the average
CRediT authorship contribution statement
Qingping Sun: Conceptualization, Methodology, Software, Data curation, Writing - original draft, Writing - review & editing. Guowei Zhou: Conceptualization, Methodology, Writing - review & editing. Zhaoxu Meng: Conceptualization, Methodology, Writing - review & editing. Mukesh Jain: Supervision, Writing - review & editing. Xuming Su: Supervision, Resources, Project administration, Funding acquisition.
Declaration of competing interest
The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
Acknowledgments
The authors acknowledge support from the Ford Motor Company with funding from the U.S. Department of Energy's Office of Energy Efficiency and Renewable Energy (EERE), under Award Number DE-EE0006867. Q. Sun acknowledges support from the China Scholarship Council (CSC). Z. Meng would like to acknowledge startup funds from Clemson University and SC TRIMH support (P20 GM121342).
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