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Interface-driven mechanisms in cubic/noncubic nanolaminates at different scales

Published online by Cambridge University Press:  10 January 2019

I.J. Beyerlein
Affiliation:
Department of Mechanical Engineering, Materials Department, University of California, Santa Barbara, USA; beyerlein@ucsb.edu
J. Wang
Affiliation:
Department of Mechanical and Materials Science Engineering, University of Nebraska, USA; jianwang@unl.edu

Abstract

Superior structural properties of materials are generally desired in harsh environments, such as elevated temperatures, high rates of impact, and radiation. Composite nanolaminates, built with alternating stacks of crystalline layers, each with nanoscale individual thickness, are proving to exhibit many of these target properties. In principle, the nanolaminate concept can be applied to any two-phase, bimetallic system; however, for a number of reasons, they have been limited to combinations of metals with a cubic crystal structure. There is growing demand to increase the number of advanced materials systems containing noncubic metals, since these metals bear several desirable intrinsic properties. In this article, we cover recent modeling and experimental efforts to understand the complexity in structure, mechanisms, and behavior of noncubic/cubic nanolaminates. We hope this article will facilitate and encourage future studies in this promising area.

Information

Type
Mechanical Behavior of Nanocomposites
Copyright
Copyright © Materials Research Society 2019 
Figure 0

Figure 1. (a) Hexagonal close-packed (hcp) Mg/Nb nanolaminate with an incoherent interface, (b) a body-centered-cubic (bcc) Mg/Nb nanolaminate with a coherent interface, and (c) hardness of the Mg/Nb nanolaminates.30 The x-axis is the inverse square root of the bilayer thickness, 2h. The numbers in the plot indicate 2h of the nanolaminate.

Figure 1

Figure 2. Interface dislocation network of the Mg/Nb interface.44 (a) Disregistry plot of the Mg/Nb interface showing spatial shears, three sets of partial dislocations and two types of coherent interfaces, normal face-centered-cubic (fcc) stacking and stacking fault (SF). Dislocation structures around a node. (b) Local shears around a node corresponding to six coherent interface regions and (c) schematic of formation mechanisms of coherent interfaces and interface dislocations.

Figure 2

Figure 3. Snapshots from a molecular dynamics simulation showing the formation of a twin subdomain in the Mg phase from a Mg/Nb interface.45 (a) A twin nucleus nucleates at the Mg/Nb interface. (b) Growth of the twin nucleus via migration of BP/PB and T-PP1 interfaces. (c, d) The twin grows through the thickness of the model and continues transverse growth via the migration of PB/BP interfaces.

Figure 3

Figure 4. Faulted structure in nanoscale Al2Cu lamellae of rolled laser-treated material.50 (a, b) Multiple straight fault bands in nanoscale Al2Cu lamellae; the rolling direction and normal direction are indicated by arrows in (a), the inset diffraction pattern is from the Al2Cu lamella in (b). (c) High-resolution high-angle annular dark-field (HAADF) (z-contrast) image of the straight band showing a fault structure on $(\bar 121)_{Al_2 Cu} $ plane.

Figure 4

Figure 5. Comparison of the engineering stress–strain responses30 between (a) Mg/Nb 5 nm/5 nm and (b) Mg/Nb 50 nm/50 nm multilayered nanocomposites with interfaces oriented normal (isostress) and parallel (isostrain) to the loading direction. (c, d) Scanning electron microscope images for each combination of layer thickness and orientation are shown below the stress–strain graphs displaying the pillar deformation at yield and after instability (as indicated by the black dots on the stress–strain graph in [a]).

Figure 5

Figure 6. (a) Three-dimensional model microstructure of Zr/Nb.77 (b) Spatial map of the normalized value of equivalent plastic strain (PEEQ) showing strain heterogeneities developing at grain boundaries and triple/quadruple junctions. Red circles indicate hot spots forming a band. Black circles indicate hot spots disappearing and not forming a band. Blue circles indicate cold spots. (c) Shear banding after softening elements experience hot spots: deformed grain structure (top) and distributions of equivalent strain normalized by the applied equivalent plastic strain (bottom) after subsequent straining of 0.2. Note: RD, rolling direction; ND, normal direction; TD, transverse direction.