Abstract
We derive and analyze a novel approach for modeling and computing the mechanical relaxation of incommensurate two dimensional heterostructures. Our approach parametrizes the relaxation pattern by the compact local configuration space rather than real space, thus bypassing the need for the standard supercell approximation and giving a true aperiodic atomistic configuration. Our model extends the computationally accessible regime of weakly coupled bilayers with similar orientations or lattice spacing, for example materials with a small relative twist where the widely studied large-scale moiré patterns arise (Kim et al. in Proc Natl Acad Sci 114:3364–3369, 2017; Yoo et al. in Atomic and electronic reconstruction at van der Waals interface in twisted bilayer graphene, Nat Mater 18:448–453, 2019). Our model also makes possible the simulation of multi-layers for which no inter-layer empirical atomistic potential exists, such as those composed of \(\hbox {MoS}_2\) layers, and more generally makes possible the simulation of the relaxation of multi-layer heterostructures for which a planar moiré pattern does not exist.
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Notes
A configuration is rigorously defined as the position of all atoms in the system relative to the origin, given an arbitrary translation of the system corresponding to a change of viewpoint, typically encoded as a Radon measure in \(\mathfrak {M}(\mathbb {R}^3)\). Formally, the hull is a dynamical system \((\Omega , \mathbb {R}^2, \mathtt {T})\) where \(\Omega \) is the closure of the orbit of the atomic distribution generated by the atoms of all p layers under the action of \(\mathbb {R}^2\) through \(\mathtt {T}\). Note that the group of translations \(\mathtt {T}_\mathbf {a}\) with \(\mathbf {a}\in \mathbb {R}^2\) acts on the space of compactly supported continuous functions \(\mathcal {C}_c(\mathbb {R}^3)\) naturally through \(\mathtt {T}_\mathbf {a}f(\mathbf {x}) = f(\mathbf {x}- \mathbf {a})\), and thus on the space of Radon measures \(\mathfrak {M}(\mathbb {R}^3)\) through \(\mathtt {T}_\mathbf {a}\mu (f) = \mu (\mathtt {T}_{-\mathbf {a}} f)\).
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This work was supported in part by ARO MURI Award W911NF-14-1-0247 and by the National Science Foundation under NSF Award DMS-1819220.
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Appendix A. Proof of Prop. 3.2
Appendix A. Proof of Prop. 3.2
In this appendix, we detail the technical proof of Proposition 3.2, which we recall first for ease of reading.
Proposition A.1
Let \(\mathbf {u}\in W^{2,q}(X)\), then
where is the subset of the transversal corresponding to lattice sites of layer j, \(\nabla ^2_\omega \mathbf {u}_j\) is understood as a 2-linear form for which the norm is defined as \(\Vert \ell \Vert := \sup _{\vert \mathbf {h}_1 \vert = \vert \mathbf {h}_2 \vert = 1 } \left| \ell [\mathbf {h}_1, \mathbf {h}_2] \right| \) and
Proof
It is natural to relate this result to local finite element interpolant error estimation and follow similar steps. Let \(\omega \in \Omega \) be an arbitrary configuration, j be an arbitrary layer number. Consider a Taylor expansion up to degree 1 of \(\mathbf {u}_j\) around the point \(\Pi _j\omega \):
Using the integral formula for the residual of the Taylor series, we have
so by Jensen’s inequality we obtain the estimate
As earlier (see (3.2)), let us write \(\varvec{\gamma }_j = \mathrm {E}_j \begin{bmatrix} s \\ t \end{bmatrix}\) with \(0 \leqq s, t < 1\). The lattice sites in layer j around the origin are located at the four points \(\mathbf {r}_{ab}\) with \(a, b \in \{ 0,1 \}\) defined as in (2.12). One checks easily from the definition (3.4) that
where the shifts \(\delta \omega _{00}\), \(\delta \omega _{10}\), \(\delta \omega _{01}\), \(\delta \omega _{11}\) can be chosen as
since \(\delta \omega _{ab}\) is defined on \(\Omega \) and is thus invariant under lattice shifts. Note that for \(a,b \in \{0,1\}\),
where \(\theta \) is defined in (3.6). Furthermore, the weighted average of these shifts is zero:
where we have introduced the bilinear weights
As a consequence, by the affine character of the Taylor approximant \(T_\omega ^1 \mathbf {u}_j\) defined above,
Let us now rewrite the definition (3.2) of the bilinear interpolant \(\widetilde{\mathbf {u}}_j\) as
Taking the difference of the identities (A.4), (A.5) and using convexity of the norm and the above Taylor estimate (A.3), we find the pointwise estimate
We may now integrate over the configuration parameter \(\omega = (\varvec{\gamma }_1, \ldots , \varvec{\gamma }_p)\). The difference between \(\omega \) and \(\left( \Pi _j \omega + h \delta \omega _{ab}\right) \) depends only on s, t and h, for example
Integrating over the variables \(\varvec{\gamma }_i\) for \(i \ne j\) with fixed values of \(\varvec{\gamma }_j= \mathrm {E}_j \begin{bmatrix} s \\ t \end{bmatrix}\) and h we find that by translation invariance of the Lebesgue measure,
This leads to
Since the right-hand side does not depend on the remaining variable \(\varvec{\gamma }_j\), one last integration over it yields
which proves the desired estimate (3.5). \(\quad \square \)
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Cazeaux, P., Luskin, M. & Massatt, D. Energy Minimization of Two Dimensional Incommensurate Heterostructures. Arch Rational Mech Anal 235, 1289–1325 (2020). https://doi.org/10.1007/s00205-019-01444-y
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DOI: https://doi.org/10.1007/s00205-019-01444-y