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Scrambling with conservation laws

Gong Cheng Condensed Matter Theory Center and Department of Physics, University of Maryland, College Park, MD 20742, USA Brian Swingle Condensed Matter Theory Center and Department of Physics, University of Maryland, College Park, MD 20742, USA Department of Physics, Brandeis University, Waltham, MA 02453, USA
Abstract

In this article we discuss the impact of conservation laws, specifically U(1)U(1) charge conservation and energy conservation, on scrambling dynamics, especially on the approach to the late time fully scrambled state. As a model, we consider a d+1d+1 dimensional (d2d\geq 2) holographic conformal field theory with Einstein gravity dual. Using the holographic dictionary, we calculate out-of-time-order-correlators (OTOCs) that involve the conserved U(1)U(1) current operator or energy-momentum tensor. We show that these OTOCs approach their late time value as a power law in time, with a universal exponent d2\frac{d}{2}. We also generalize the result to compute OTOCs between general operators which have overlap with the conserved charges.

1 Introduction

1.1 Motivation

Quantum information scrambling [1, 2, 3] is a fundamental phenomenon in chaotic many-body systems that has been under wide discussion in recent years. On the theoretical side, this activity focused on the study of out-of-time-order correlators (OTOCs) [4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16]. For a chaotic system with large NN number of degrees of freedom per unit volume, the OTOC displays an exponentially increasing deviation from its initial value which is characterized by a quantum Lyapunov exponent. This period of growth occurs after local equilibrium is achieved but before the scrambling time, when the system approaches global equilibrium. Schematically, given simple Hermitian operators WW and VV, one has

OTOC=W(t)V(0)W(t)V(0)f0f1NeλLt+.\text{OTOC}=\langle W(t)V(0)W(t)V(0)\rangle\sim f_{0}-\frac{f_{1}}{N}e^{\lambda_{L}t}+\cdots. (1)

For a large NN conformal field theory (CFT) holographically described by Einstein gravity, earlier works [5][6][17][18][19] calculated OTOCs through geometric methods, by studying shockwave geometries. The Lyapunov exponent in such a theory is equal to 2πβ\frac{2\pi}{\beta}, saturating the conjectured chaos bound [20]. For times much larger than scrambling time (the late time regime), the OTOC decays to zero exponentially fast, with a different but related exponent. By contrast, it was shown in [21] that in a random circuit model with local charge conservation law, the OTOC between the charge density operator and a non-conserved operator displays a power law tail at late time. While such power law tails are expected to be generic, they have not yet been seen in holographic systems. This missing piece of physics motivated the present study. Other studies of the interplay between conservation laws, hydrodynamics, and OTOCs include [22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35].

The bulk of this work focuses on the U(1)U(1) case: we compute OTOCs between the conserved charge density and a (non-conserved) scalar operator and show that holographic systems also exhibit power law tails consistent with the random circuit result. We also argue that power law tails will be induced by energy conservation. This has not been shown before, but it is important since Hamiltonian systems generically have energy conservation but not charge conservation. In the remainder of the introduction, we review existing holographic calculations, focusing on the scattering approach. Then, in the rest of the article, we show how these calculations are modified due to U(1)U(1) charge conservation and we interpret the result physically. We also discuss the extension to energy conservation. Overall, we view this work as a study of the interplay between slow modes, as in hydrodynamics, and the fast dynamics of scrambling.

1.2 Review of the holographic calculation

The holographic calculation of OTOCs for scalar operators is discussed in many works. The approach that we follow here is based on the scattering approach discussed in [6]. In this approach, the boundary OTOC is written as an inner product of inin and outout asymptotic states.

W(t1,x1)V(t2,x2)W(t1,x1)V(t2,x2)=out|in|in=W(t1,x1)V(t2,x2)|TFD|out=V(t2,x2)W(t1,x1)|TFD.\begin{split}\langle W(t_{1},x_{1})&V(t_{2},x_{2})W(t_{1},x_{1})V(t_{2},x_{2})\rangle=\langle out|in\rangle\\ &|in\rangle=W(t_{1},x_{1})V(t_{2},x_{2})|TFD\rangle\\ &|out\rangle=V^{\dagger}(t_{2},x_{2})W^{\dagger}(t_{1},x_{1})|TFD\rangle.\end{split} (2)

From the bulk perspective, these inin and outout states may be written in terms of bulk wavefunctions as

|in=𝑑pu𝑑x𝑑pv𝑑xϕW(pv,x)ϕV(pu,x)|pu,x,pv,xin|out=𝑑pu𝑑x𝑑pv𝑑xϕW(pv,x)ϕV(pu,x)|pu,x,pv,xout.\begin{split}|in\rangle=\int dp^{u}dx\int dp^{v}dx^{\prime}\phi_{W}(p^{v},x)\phi_{V}(p^{u},x^{\prime})|p^{u},x,p^{v},x^{\prime}\rangle_{in}\\ |out\rangle=\int dp^{u}dx\int dp^{v}dx^{\prime}\phi_{W^{\dagger}}(p^{v},x)\phi_{V^{\dagger}}(p^{u},x^{\prime})|p^{u},x,p^{v},x^{\prime}\rangle_{out}.\end{split} (3)

Here uu and vv are null coordinates in the black hole geometry dual to the thermofield double state |TFD|TFD\rangle.

V(t2)V(t_{2})W(t1)W(t_{1})|in>|in>|out>|out>
Figure 1: inin and outout sates in the Penrose diagram. The data on the inin and outout slices are given by Eq. (3).

Note that the momentum states are only well-defined near the black hole horizon. We think of the scattering as taking place in the approximately flat near horizon region as described by Kruskal coordinates. This corresponds to the case of large time separation between t1t_{1} and t2t_{2}, as shown in Fig 1. The wave functions are given by bulk-to-boundary propagators. So

ϕW(p1v,x)=𝑑veip1uvϕW(u,v,x)W(t2,x2)|u=ϵϕV(p2u,x)=𝑑ueip2vuϕV(u,v,x)V(t1,x1)|v=ϵϕW(p1v,x)=𝑑veip1uvϕW(u,v,x)W(t2,x2)|u=ϵϕV(p2u,x)=𝑑ueip2vuϕV(u,v,x)V(t1,x1)|v=ϵ\begin{split}&\phi_{W}(p^{v}_{1},x)=\int dve^{ip_{1}^{u}v}\langle\phi_{W}(u,v,x)W(t_{2},x_{2})\rangle|_{u=-\epsilon}\\ &\phi_{V}(p^{u}_{2},x^{\prime})=\int due^{ip^{v}_{2}u}\langle\phi_{V}(u,v,x)V(t_{1},x_{1})\rangle|_{v=\epsilon}\\ &\phi_{W^{\dagger}}(p^{v}_{1},x)=\int dve^{ip^{u}_{1}v}\langle\phi_{W}(u,v,x)W^{\dagger}(t_{2},x_{2})\rangle|_{u=-\epsilon}\\ &\phi_{V^{\dagger}}(p^{u}_{2},x^{\prime})=\int due^{ip^{v}_{2}u}\langle\phi_{V}(u,v,x)V^{\dagger}(t_{1},x_{1})\rangle|_{v=\epsilon}\\ \end{split} (4)

These formulae have a direct interpretation as bulk scattering states sourced by boundary operators. The relevant energy scale is determined by the boundary time separation through the Mandelstam variable s:=2p1vp2ue2πβt12s:=2p_{1}^{v}p_{2}^{u}\sim e^{\frac{2\pi}{\beta}t_{12}}. For scrambling physics, we are interested in time scales that are larger than the relaxation time. The dominate contribution in this regime comes from summing ladder diagrams with graviton exchanges [36]. To leading order in ss, the S-matrix approaches a pure phase, obtained from the eikonal approximation,

|p1u,x,p2v,xouteiδ(s,b)|p1u,x,p2v,xin+|p_{1}^{u},x,p_{2}^{v},x^{\prime}\rangle_{out}\sim e^{i\delta(s,b)}|p_{1}^{u},x,p_{2}^{v},x^{\prime}\rangle_{in}+\cdots (5)

The physical interpretation of this phase factor is interaction of particle 11 with a gravitational shockwave sourced by particle 22 [37][38]. The shockwave metric is

ds2=A(uv)du[dvδ(u)h(x)du]+B(uv)ddx.ds^{2}=A(uv)du[dv-\delta(u)h(x)du]+B(uv)d^{d}x. (6)

While passing through the shockwave located near u0u\sim 0, the scalar wave function receives a jump in the vv coordinate,

𝑑p1uϕ(p1u,x)eip1uh(x)eip1uv=ϕ(vh(x),x).\int dp_{1}^{u}\phi(p_{1}^{u},x)e^{ip_{1}^{u}h(x)}e^{-ip_{1}^{u}v}=\phi(v-h(x),x). (7)

The phase δ(s,b)\delta(s,b) is then identified with the displacement factor h(x)=GNp2veμ|x||x|d12h(x)=G_{N}p_{2}^{v}\frac{e^{-\mu|x|}}{|x|^{\frac{d-1}{2}}}.

For scalar operators, the OTOC is evaluated in earlier works. In the limit ΔWΔV1\Delta_{W}\gg\Delta_{V}\gg 1, the heavy particle’s wavefunction is not much affected by the shockwave sourced by the light particle. So the amplitude is simply an inner product between VV particle wavefunctions with and without the shockwave,

OTOC𝑑v𝑑xϕV(v,x)vϕV(vh(x),x)[11+GNΔWΓe2πβtμ|x|]ΔV.\begin{split}\text{OTOC}&\sim\int dvdx\phi_{V}(v,x)\partial_{v}\phi_{V}(v-h(x),x)\\ &\sim\left[\frac{1}{1+\frac{G_{N}\Delta_{W}}{\Gamma}e^{\frac{2\pi}{\beta}t-\mu|x|}}\right]^{\Delta_{V}}.\end{split} (8)

Γ\Gamma is a constant depending on the regularization of the correlator.

At early time, when the second term in denominator is much smaller than the first term, the OTOC is decreasing as shown in Eq. (1). Note that e2πβte^{\frac{2\pi}{\beta}t} is roughly the colliding energy, and it enters through pp dependence of h(x)h(x). The exponent is 2πβ\frac{2\pi}{\beta}, independent of the operator. The correlator has decayed significantly when the second term in the denominator is O(1)O(1). After this time, the correlator experiences an expontial decay with an operator-dependent exponent. We refer to this as the late time regime of OTOC.

1.3 Results and outline

The situation is changed when we consider an OTOC that involves conserved charges. For example, the R-charge in 𝒩=4\mathcal{N}=4 SYM theory, and more generally the energy-momentum tensor. We will see that due to the hydrodynamical property of the conserved current, the particle sourced by these operators in the bulk spreads over a large region of space-time. As a result, the collision responsible for scrambling happens at a wide range of space-time points in the classical picture (see Fig 2). When the collision occurs near the horizon, the center of mass energy is large, but when the collision occurs further away from the horizon, the center of mass energy is smaller. This leads to a smearing of the exponential factor in Eq. (8), effectively replacing the OTOC formula with

OTOC0+𝑑s1sd2+1[11+cNe2πβ(ts)μ|x|]α\text{OTOC}\sim\int_{0}^{+\infty}ds\frac{1}{s^{\frac{d}{2}+1}}\left[\frac{1}{1+\frac{c}{N}e^{\frac{2\pi}{\beta}(t-s)-\mu|x|}}\right]^{\alpha} (9)

where cc and α\alpha are some constants. One can then show that at late time, the OTOC becomes td2\sim t^{-\frac{d}{2}}.

The article is organized as follows. For simplicity, we start with the conserved charge density of a U(1)U(1) symmetry. In section 2 we give an expression for the dual photon’s wave function, to lowest order in transverse momentum and frequency. Then we analyze the inner product and equation of motion for the photon field. Using these ingredients and some additional approximations, we calculate the OTOC. In section 3 we interpret these calculations in terms of the classical picture in Fig. 2. In section 4 we discuss the case of the energy-momentum tensor. Finally, we generalize the result in section 5 to the case of generic operators with overlap with the conserved currents.

J0(t2)J_{0}(t_{2})O(t1)O(t_{1})
Figure 2: Photon scatters with shockwave. The blue line denotes the shockwave sourced by scalar operator. The photon sourced by charge operator spreads in space-time. Classically, we can view it as a bunch of photons, with different longitudinal energy.

2 Correlator with U(1) charge

2.1 Solution to equation of motion

In an AdS-Schwarzschild black hole background, the metric is

ds2=L2[f(R)R2dt2+1R2f(R)dR2+1R2ddx]ds^{2}=L^{2}\left[-\frac{f(R)}{R^{2}}dt^{2}+\frac{1}{R^{2}f(R)}dR^{2}+\frac{1}{R^{2}}d^{d}\vec{x}\right] (10)

where R=R+R=R_{+} is the horizon and boundary is at R=0R=0. The inverse temperature is β=4πR+d+1\beta=\frac{4\pi R_{+}}{d+1} and f(R)=1(RR+)d+1f(R)=1-(\frac{R}{R_{+}})^{d+1}. It’s more convenient to use the tortoise coordinate, rr, defined by

dr=1f(R)dR.dr=-\frac{1}{f(R)}dR. (11)

The domain of rr is r(,0]r\in(-\infty,0] with -\infty corresponding to the horizon and 0 corresponding to the boundary. In this coordinate, the metric components are grr=gtt=L2f(R)R2g_{rr}=-g_{tt}=L^{2}\frac{f(R)}{R^{2}}. Here we use x\vec{x} to denote the coordinates of the transverse directions. We also consider a Maxwell field propagating in this geometry whose dynamics determines the behavior of a U(1)U(1) current operator J0J_{0} on the boundary. In this note, we will focus on the four-point correlation function with two insertions of J0J_{0} and two insertions of a scalar operator OO.

The Maxwell-Einstein equation is

μ(gFμν)=μ(ggμρgνσFρσ)=0.\partial_{\mu}(\sqrt{-g}F^{\mu\nu})=\partial_{\mu}(\sqrt{-g}g^{\mu\rho}g^{\nu\sigma}F_{\rho\sigma})=0. (12)

Consider the ansatz Ai=0A_{i}=0 for all the transverse directions. The Fourier mode decomposition is

Aμ(r,t,x)=𝑑ω𝑑kAμ(r,ω,k)eiωteikxA_{\mu}(r,t,\vec{x})=\int d\omega d\vec{k}A_{\mu}(r,\omega,k)e^{-i\omega t}e^{i\vec{k}\cdot\vec{x}} (13)

Using the trick in [39], we pick a transverse coordinate frame for each k\vec{k}, such that the xx-axis is parallel to k\vec{k} direction, with the other axes perpendicular to it. Then x\partial_{x} can be replaced by ikik when acting on that mode, and derivatives in other transverse direction are replaced by 0. We also assume that the AA field is spherically symmetric and excited by a point source sitting at x=0\vec{x^{\prime}}=0, so the momentum space AA only depends on norm of k\vec{k}.

Written in component form, the equations are

{r(ggrrgtt(rAttAr))+x(ggxxgttxAt)=0t(ggttgrr(tArrAt))+x(ggxxgrrxAr)=0r(ggrrgxx(xAr))+t(ggttgxx(xAt))=0.\Bigg{\{}\begin{array}[]{ccc}\partial_{r}(\sqrt{-g}g^{rr}g^{tt}(\partial_{r}A_{t}-\partial_{t}A_{r}))+\partial_{x}(\sqrt{-g}g^{xx}g^{tt}\partial_{x}A_{t})=0\\ \partial_{t}(\sqrt{-g}g^{tt}g^{rr}(\partial_{t}A_{r}-\partial_{r}A_{t}))+\partial_{x}(\sqrt{-g}g^{xx}g^{rr}\partial_{x}A_{r})=0\\ \partial_{r}(\sqrt{-g}g^{rr}g^{xx}(-\partial_{x}A_{r}))+\partial_{t}(\sqrt{-g}g^{tt}g^{xx}(-\partial_{x}A_{t}))=0.\end{array} (14)

From the second equation, one can deduce

ω2gttAr+iωgttrAtk2gxxAr=0Ar=iωgttrAtω2gtt+k2gxx\begin{split}-\omega^{2}g^{tt}A_{r}+i\omega g^{tt}\partial_{r}A_{t}-k^{2}g^{xx}A_{r}&=0\\ \implies A_{r}=\frac{i\omega g^{tt}\partial_{r}A_{t}}{\omega^{2}g^{tt}+k^{2}g^{xx}}\end{split} (15)

Then one can use the first equation to find a second order differential equation for AtA_{t},

r(ggrrgttk2gxxrAtω2gtt+k2gxx)k2ggxxgttAt=0.\partial_{r}(\sqrt{-g}g^{rr}g^{tt}\frac{k^{2}g^{xx}\partial_{r}A_{t}}{\omega^{2}g^{tt}+k^{2}g^{xx}})-k^{2}\sqrt{-g}g^{xx}g^{tt}A_{t}=0. (16)

This equation has two independent solutions. As rr\rightarrow\infty, they behave like e±iωre^{\pm i\omega r}, corresponding to out-going and in-falling boundary condition at the horizon. We focus on one of them, since the other one is obtained by complex conjugation. The solution can be found explicitly in the small frequency and small momentum limit by setting ωλω\omega\rightarrow\lambda\omega, kλkk\rightarrow\lambda k, and taking λ1\lambda\ll 1. Up to first order in λ\lambda, we have

At(r,ω,k)=eiωrC(ω,k)[1+iωr𝑑r(1(RR+)d2)+ik2ωr𝑑r(RR+)d2f+O(λ2)].A_{t}(r,\omega,k)=e^{-i\omega r}C(\omega,k)[1+i\omega\int_{-\infty}^{r}dr(1-(\frac{R}{R_{+}})^{d-2})+\frac{ik^{2}}{\omega}\int_{-\infty}^{r}dr(\frac{R}{R_{+}})^{d-2}f+O(\lambda^{2})]. (17)

The normalization constant CC is fixed by requiring limr0At(r,ω,k)1\lim_{r\rightarrow 0}A_{t}(r,\omega,k)\rightarrow 1. Then we find that

At(r,ω,k)=eiωr[1+iωH(r)+ik2ωR+1(RR+)d1d11+iωH(0)+ik2ωR+1d1+O(λ2)]A_{t}(r,\omega,k)=e^{-i\omega r}\left[\frac{1+i\omega H(r)+i\frac{k^{2}}{\omega}R_{+}\frac{1-(\frac{R}{R_{+}})^{d-1}}{d-1}}{1+i\omega H(0)+i\frac{k^{2}}{\omega}R_{+}\frac{1}{d-1}}+O(\lambda^{2})\right] (18)

The factor 1d1R+\frac{1}{d-1}R_{+} is identified as the diffusion constant DD. H(r)H(r) is the indeterminate integral of the second term in Eq. (18). If we ignore the ωH(0)\omega H(0) term in the denominator, then this function has a pole at ω=iDk2\omega=-iDk^{2}. With this ωk2\omega\sim k^{2} scaling, the ωH(0)\omega H(0) is indeed subleading compared to the ik2D/ωik^{2}D/\omega term at small ω\omega and kk. Moreover, we can anticipate that ω2\omega^{2} is of order k4k^{4} after using the residue theorem. Hence, to the leading order in small kk and ω\omega, we can neglect ω2\omega^{2} and higher order terms. Another approximation is to set (RR+)1(\frac{R}{R_{+}})\sim 1, corresponding to the near horizon region. Since the scrambling time is large, the relevant physics indeed happens within this region. In summary, we have

At(r,ω,k)eiωrωω+iDk2.A_{t}(r,\omega,k)\sim e^{-i\omega r}\frac{\omega}{\omega+iDk^{2}}. (19)

The real space form is

At(r,t,x)t[1(tt+r)d2e|xx|24D(tt+r)θ(tt+r)]A_{t}(r,t,\vec{x})\sim\partial_{t}\left[\frac{1}{(t-t^{\prime}+r)^{\frac{d}{2}}}e^{-\frac{|\vec{x}-\vec{x}^{\prime}|^{2}}{4D(t-t^{\prime}+r)}}\theta(t-t^{\prime}+r)\right] (20)

where tt^{\prime} and x\vec{x}^{\prime} label the position of the boundary source. We expect this expression to hold near the horizon when the transverse separation from the source is large. Now we use Eq. (15) to obtain the other components,

AriωrAt=At,Ftr=tArrAt=k2gxxrAtω2gtt+k2gxxik2ωgxxgttAt.\begin{split}A_{r}&\sim\frac{i}{\omega}\partial_{r}A_{t}=A_{t},\\ F_{tr}=\partial_{t}A_{r}-\partial_{r}A_{t}&=\frac{-k^{2}g^{xx}\partial_{r}A_{t}}{\omega^{2}g^{tt}+k^{2}g^{xx}}\sim\frac{ik^{2}}{\omega}g^{xx}g_{tt}A_{t}.\end{split} (21)

Since gtt0g_{tt}\rightarrow 0 near horizon, FtrF_{tr} is also very small there. (Note that the physical electric field Er=gttgrrFtrE_{r}=\sqrt{g^{tt}}\sqrt{g^{rr}}F_{tr} is still finite).

2.2 Inner product of gauge field

The gauge invariant inner product between two gauge field configurations A1A_{1} and A2A_{2} is

(A1,A2)=hnμ(F1μνA2νF2μνA1ν)(A_{1},A_{2})=\int\sqrt{h}n^{\mu}({F_{1}}^{*}_{\mu\nu}{A_{2}}^{\nu}-{F_{2}}_{\mu\nu}{A_{1}^{*}}^{\nu}) (22)

Where the integration is over a Cauchy surface. Following [6], we choose to integrate on constant u0u\sim 0 slice. Then this inner product becomes

𝑑v𝑑x(RL)dguv(F1vuA2vF2vuA1v),\int dvd\vec{x}\left(\frac{R}{L}\right)^{-d}g^{uv}({F_{1}}_{vu}^{*}{A_{2}}_{v}-{F_{2}}_{vu}{A_{1}^{*}}_{v}), (23)

with uu and vv related to tt and rr by

u=e2πβ(rt),v=e2πβ(t+r),(β2π)2guv=2uvgtt.\begin{split}u=-e^{\frac{2\pi}{\beta}(r-t)},\\ v=e^{\frac{2\pi}{\beta}(t+r)},\\ (\frac{\beta}{2\pi})^{2}g^{uv}=2uvg^{tt}.\end{split} (24)

The various components of gauge field are related to the old ones by

Av=tvAt+rvAr,=β2π12v(At+Ar),Fuv=turvFtr+rutvFrt,=(β2π)212uvFtr.\begin{split}A_{v}=&\frac{\partial t}{\partial v}A_{t}+\frac{\partial r}{\partial v}A_{r},\\ =&\frac{\beta}{2\pi}\frac{1}{2v}(A_{t}+A_{r}),\\ F_{uv}=&\frac{\partial t}{\partial u}\frac{\partial r}{\partial v}F_{tr}+\frac{\partial r}{\partial u}\frac{\partial t}{\partial v}F_{rt},\\ =&-(\frac{\beta}{2\pi})^{2}\frac{1}{2uv}F_{tr}.\end{split} (25)

Following Eq. (19) and Eq. (21),

Av=β2π1vAt=1vvv(𝑑ω𝑑kiω+iDk2viβω2πeikx)vϕ(v,x),gxxgttFtr=𝑑ω𝑑kik2ω+iDk2viβω2πeikx=2ϕ(v,x).\begin{split}A_{v}=\frac{\beta}{2\pi}\frac{1}{v}A_{t}=&\frac{1}{v}v\partial_{v}\left(\int d\omega d\vec{k}\frac{i}{\omega+iDk^{2}}v^{-i\frac{\beta\omega}{2\pi}}e^{i\vec{k}\cdot\vec{x}}\right)\\ \coloneqq&\partial_{v}\phi(v,\vec{x}),\\ g_{xx}g^{tt}F_{tr}=&\int d\omega d\vec{k}\frac{ik^{2}}{\omega+iDk^{2}}v^{-i\frac{\beta\omega}{2\pi}}e^{i\vec{k}\cdot\vec{x}}=-\vec{\nabla}^{2}\phi(v,\vec{x}).\end{split} (26)

Plug this into the inner product expression Eq. (23), we get

(A1,A2)=𝑑vddx(RL)2d[2ϕ1(v,x)vϕ2(v,x)+2ϕ2(v,x)vϕ1(v,x)]=𝑑vddx(RL)2d[ϕ1(v,x)vϕ2(v,x)ϕ2(v,x)vϕ1(v,x)]\begin{split}(A_{1},A_{2})=&\int dvd^{d}\vec{x}\left(\frac{R}{L}\right)^{2-d}[-\nabla^{2}\phi_{1}^{*}(v,\vec{x})\partial_{v}\phi_{2}(v,\vec{x})+\nabla^{2}\phi_{2}(v,\vec{x})\partial_{v}\phi_{1}^{*}(v,\vec{x})]\\ =&\int dvd^{d}\vec{x}\left(\frac{R}{L}\right)^{2-d}[\vec{\nabla}\phi_{1}^{*}(v,\vec{x})\cdot\partial_{v}\vec{\nabla}\phi_{2}(v,\vec{x})-\vec{\nabla}\phi_{2}(v,\vec{x})\cdot\partial_{v}\vec{\nabla}\phi_{1}^{*}(v,\vec{x})]\end{split} (27)

where ϕ(v,x)\phi(v,\vec{x}) is the diffusion kernel given in Eq. (26). We will see that the inner product written in this way is very convenient when discussing the shockwave.

2.3 Scattering states

The original definition of OTOC is complicated by a UV divergence arising from coincident operator insertions. To avoid this, one can consider a regularized version obtained by inserting operators at different values of imaginary time,

𝒞reg=Tr[ρ1ϵV(t2,x2)W(t1,x1)ρϵV(t2,x2)W(t1,x1)]\mathcal{C}_{reg}=Tr[\rho^{1-\epsilon}V(t_{2},\vec{x}_{2})W(t_{1},\vec{x}_{1})\rho^{\epsilon}V(t_{2},\vec{x}_{2})W(t_{1},\vec{x}_{1})] (28)

To simplify the discussion, we choose a symmetric regularization. In the following, we will consider the correlator

𝒞𝒥0𝒪=Tr[ρ12J0(t2,x2)O(t1,x1)ρ12J0(t2,x2)O(t1,x1)].\mathcal{C_{J_{0}O}}=Tr[\rho^{\frac{1}{2}}J_{0}(t_{2},\vec{x}_{2})O(t_{1},\vec{x}_{1})\rho^{\frac{1}{2}}J_{0}(t_{2},\vec{x}_{2})O(t_{1},\vec{x}_{1})]. (29)

It has a representation as an inner product of inin and outout states

|in=OL(t1,x1)J0R(t2,x2)|SAdS|out=J0L(t2,x2)OR(t1,x1)|SAdS\begin{split}|in\rangle=O^{L}(t_{1},\vec{x}_{1})J_{0}^{R}(t_{2},\vec{x}_{2})|S-AdS\rangle\\ |out\rangle=J_{0}^{L}(t_{2},\vec{x}_{2})O^{R}(t_{1},\vec{x_{1}})|S-AdS\rangle\end{split} (30)

where |SAdS|S-AdS\rangle denotes the Schwarzschild-AdS black hole thermal double state,

|SAdS=neβ2En|EnL|EnR.|S-AdS\rangle=\sum_{n}e^{-\frac{\beta}{2}E_{n}}|E_{n}\rangle_{L}|E_{n}\rangle_{R}. (31)
J0R(t2)J_{0}^{R}(t_{2})OL(t1)O^{L}(t_{1})J0L(t2)J_{0}^{L}(t_{2})OR(t1)O^{R}(t_{1})
Figure 3: inin and outout sates in a symmetric regularization scheme

The superscript LL and RR on each operator means that the excitation is created on the left or right side, respectively. For example, J0R(t2)J^{R}_{0}(t_{2}) creates a photon on the right. We denote the corresponding gauge field by AμRA_{\mu}^{R}. In general it is a linear superposition of in-falling and out-going solutions, depending on the state we are constructing. Following [40][41], we choose the coefficients such that the field has positive Kruskal frequency for in-falling mode and negative Kruskal frequency for out-going mode. For this purpose, we use the following combination

AμR(r,ω,k)=(1+n(ω))AμRin-falling(r,ω,k)n(ω)AμRin-falling(r,ω,k),A_{\mu}^{R}(r,\omega,k)=(1+n(\omega)){A_{\mu}^{R}}_{\tiny{\text{in-falling}}}(r,\omega,k)-n(\omega){A_{\mu}^{R}}_{\text{in-falling}}^{*}(r,\omega,k), (32)

n(ω)n(\omega) is the Boltzmann factor.

For the in-falling part, we use the ansatz:

AvRin-falling=vϕin-fallingR(v,x),ϕin-fallingR(v,x)=ddk(2π)d1(ve2πβt21)βDk22πθ(ve2πβt2)eik(xx2).\begin{split}{A^{R}_{v}}_{\text{in-falling}}&=\partial_{v}\phi^{R}_{\text{in-falling}}(v,\vec{x}),\\ \phi^{R}_{\text{in-falling}}(v,\vec{x})&=\int\frac{d^{d}k}{(2\pi)^{d}}\frac{1}{(ve^{-\frac{2\pi}{\beta}t_{2}}-1)^{\frac{\beta Dk^{2}}{2\pi}}}\theta(v-e^{\frac{2\pi}{\beta}t_{2}})e^{i\vec{k}\cdot(\vec{x}-\vec{x_{2}})}.\end{split} (33)

This is just rewritten from Eq. (26), except that we have inserted an extra 11 in the denominator. This change doesn’t modify the long time behavior of the wave function, but it does provide some convenience in the analysis. On the other hand, the out-going part in AvA_{v} is proportional to uu. To evaluate the OTOC, we choose to calculate the inner product on the surface u0u\sim 0. Hence, the out-going mode’s contribution can be neglected. The thermal factor (1+n(ω))(1+n(\omega)) is proportional to 12sin(βDk22)\frac{1}{2\sin(\frac{\beta Dk^{2}}{2})}, evaluated at the diffusive pole111The actual pole contains a small real part that is higher order in kk which keeps the integrand finite.. It suggests the following ansatz for AvRA_{v}^{R}

AvR=vϕR(v,x),ϕR(v,x)=ddk(2π)d12sin(βDk22)1(1ve2πβt2)βDk22πeik(xx2).\begin{split}A_{v}^{R}&=\partial_{v}\phi^{R}(v,\vec{x}),\\ \phi^{R}(v,\vec{x})&=\int\frac{d^{d}k}{(2\pi)^{d}}\frac{1}{2\sin(\frac{\beta Dk^{2}}{2})}\frac{1}{(1-ve^{-\frac{2\pi}{\beta}t_{2}})^{\frac{\beta Dk^{2}}{2\pi}}}e^{i\vec{k}\cdot(\vec{x}-\vec{x_{2}})}.\end{split} (34)

A nice property of the above expression is that the real space form of ϕR\phi^{R} and ϕinfallingR\phi^{R}_{in-falling} are related by analytical continuation, if we treat it as a complete solution of equation of motion. To see this, note that

1(1e2πβ(tt2+r+i0+))βDk22π1(1e2πβ(tt2+ri0+))βDk22π=2isin(βDk22)1(ve2πβt21)βDk22πθ(ve2πβt2)\frac{1}{(1-e^{\frac{2\pi}{\beta}(t-t_{2}+r+i0^{+})})^{\frac{\beta Dk^{2}}{2\pi}}}-\frac{1}{(1-e^{\frac{2\pi}{\beta}(t-t_{2}+r-i0^{+})})^{\frac{\beta Dk^{2}}{2\pi}}}=2i\sin(\frac{\beta Dk^{2}}{2})\frac{1}{(ve^{-\frac{2\pi}{\beta}t_{2}}-1)^{\frac{\beta Dk^{2}}{2\pi}}}\theta(v-e^{\frac{2\pi}{\beta}t_{2}}) (35)

Similarly, on the left side boundary, the operator J0LJ_{0}^{L} sources a wave function AvLA_{v}^{L}. By symmetry, AvLA_{v}^{L} is related to AvRA_{v}^{R} via the transformation (u,v)(u,v)(u,v)\rightarrow(-u,-v). Correspondingly, we define ϕL(v,x)=ϕR(v,x)\phi^{L}(v,\vec{x})=\phi^{R}(-v,\vec{x}). Then AvLA_{v}^{L} can be written as

AvL=vϕL(v,x),ϕL(v,x)=ddk(2π)d12sin(βDk22)1(1+ve2πβt2)βDk22πeik(xx2).\begin{split}A_{v}^{L}&=\partial_{v}\phi^{L}(v,\vec{x}),\\ \phi^{L}(v,\vec{x})&=\int\frac{d^{d}k}{(2\pi)^{d}}\frac{1}{2\sin(\frac{\beta Dk^{2}}{2})}\frac{1}{(1+ve^{-\frac{2\pi}{\beta}t_{2}})^{\frac{\beta Dk^{2}}{2\pi}}}e^{i\vec{k}\cdot(\vec{x}-\vec{x_{2}})}.\end{split} (36)

The scalar operator ORO^{R} and OLO^{L} create scalar mode in the bulk. For simplicity, we assume that the scalar operator OO has a large conformal dimension, corresponding to a particle in bulk with a large mass. As a consequence, we can treat the scalar particle semi-classically. As it moves deep into the bulk, the scalar mode carries the shockwave along with it, which modifies the photon’s wave function as we will analyze in the next section. In contrast, we will neglect the back-reaction from the photon on this scalar mode.

2.4 Shockwave geometry

Since we are interested in the large time limit of the OTOC, we will take t1βt_{1}\gg\beta and t2βt_{2}\ll-\beta. As a result, the geodesic of the scalar particle is approximated by u=ϵ0u=\epsilon\sim 0. The shockwave geometry is described by a metric that contains a singularity near the horizon,

ds2=2guvdu[dvδ(u)h(x)du]+gxxdΩd,ds^{2}=2g_{uv}du[dv-\delta(u)h(\vec{x})du]+g_{xx}d\Omega_{d}, (37)

where h(x)=ΔONe2πβt1μ|xx1|h(\vec{x})=\frac{\Delta_{O}}{N}e^{\frac{2\pi}{\beta}t_{1}-\mu|\vec{x}-\vec{x}_{1}|} and μ=2dd+12πβ\mu=\sqrt{\frac{2d}{d+1}}\frac{2\pi}{\beta}.

The Maxwell-Einstein equation in this background is

.v(γFuvguv)+i=1di(γgiiFiv)=0,u(γFvigii)+v(γFuigii)+v(ggvvFvigii)=0,.\begin{split}\partial_{v}(\sqrt{\gamma}F_{uv}g^{uv})+\sum_{i=1}^{d}\partial_{i}(\sqrt{\gamma}g^{ii}F_{iv})=0,\\ \partial_{u}(\sqrt{\gamma}F_{vi}g^{ii})+\partial_{v}(\sqrt{\gamma}F_{ui}g^{ii})+\partial_{v}(\sqrt{-g}g^{vv}F_{vi}g^{ii})=0,\end{split} (38)

where the ii’s run from 11 to dd and label the transverse directions. The effect of the shockwave is encoded in the gvvg^{vv} component. γ\gamma is the metric determinant in the transverse directions, so g=guv2γ-g=g_{uv}^{2}\gamma.

As before, we simplify the equation by approximating RR+1\frac{R}{R_{+}}\sim 1 such that we can set γ=(LR)2d\gamma=(\frac{L}{R})^{2d} and gii=(LR)2g^{ii}=(\frac{L}{R})^{2}. Then using gvv=(guv)2guu=2guvh(x)δ(u)g^{vv}=-(g^{uv})^{2}g_{uu}=2g^{uv}h(\vec{x})\delta(u), the second equation becomes

uiAvviAu2v(iAvh(x)δ(u))=0.-\partial_{u}\partial_{i}A_{v}-\partial_{v}\partial_{i}A_{u}-2\partial_{v}(\partial_{i}A_{v}h(\vec{x})\delta(u))=0. (39)

In the region u<ϵu<\epsilon and u>ϵu>\epsilon, the first two terms are finite. At u=ϵu=\epsilon, we are searching for a solution where AvA_{v} jumps and AuA_{u} may contain a delta function δ(u)\delta(u). On the other hand, from the first equation of Eq. (38), FuvF_{uv} must be finite. Therefore the delta functions in uAv\partial_{u}A_{v} and vAu\partial_{v}A_{u} must cancel each other at u=ϵu=\epsilon. Applying this condition, Eq. (39) can be written as

2uiAv2v(iAvh(x)δ(u))=0.-2\partial_{u}\partial_{i}A_{v}-2\partial_{v}(\partial_{i}A_{v}h(\vec{x})\delta(u))=0. (40)

Integrating over uu we obtain

iAv(v,x)|u=ϵ+0+=iAv(vh(x),x)|u=ϵ0+.\partial_{i}A_{v}(v,\vec{x})|_{u=\epsilon+0^{+}}=\partial_{i}A_{v}(v-h(\vec{x}),\vec{x})|_{u=\epsilon-0^{+}}. (41)

Note that this shift in vv doesn’t commute with derivatives in the transverse directions, so this simple shift rule only applies to A\vec{\nabla}A instead of AA itself. The first equation in Eq. (38) gives the same relation between FuvF_{uv} and AA as in Eq. (21). Comparing with Eq. (26), we find that this simple shift rule also applies to ϕ(v,x)\vec{\nabla}\phi(v,\vec{x}). Hence,

ϕ(v,x)|u=ϵ+0+=ϕ(vh(x),x)|u=ϵ0+,\vec{\nabla}\phi(v,\vec{x})|_{u=\epsilon+0^{+}}=\vec{\nabla}\phi(v-h(\vec{x}),\vec{x})|_{u=\epsilon-0^{+}}, (42)

which is the reason to write the inner product in the form of Eq. (27). In summary, after scattering with the shockwave, the wave function sourced by J0RJ_{0}^{R} is modified according to the rule Eq. (42). If we choose to evaluate the inner product, Eq. (27), just after the scattering, along u=ϵ+0+u=\epsilon+0^{+}, then ϕ1\phi_{1} and ϕ2\phi_{2} (in Eq. (27)) should be

ϕ1(v,x)=ϕL(v,x),ϕ2(v,x)=ϕR(vh(xx1),x).\begin{split}\vec{\nabla}\phi_{1}(v,\vec{x})&=\vec{\nabla}\phi^{L}(v,\vec{x}),\\ \vec{\nabla}\phi_{2}(v,\vec{x})&=\vec{\nabla}\phi^{R}(v-h(\vec{x}-\vec{x_{1}}),\vec{x}).\end{split} (43)

2.5 Calculation of OTOC

In this section, we evaluate the inner product in Eq. (27). It turns out that the relevant integral in is easier to do in momentum space. Define

ϕ(p,x)=𝑑veipvϕ(v,x),\phi(p,\vec{x})=\int dve^{ipv}\phi(v,\vec{x}), (44)

so that

ϕ1(p,x)=ddk(2π)dik2sin(βDk22)pβDk22π1eDk2t2Γ(β2πDk2)eipe2πβt2+iph(xx1)eik(xx2)θ(p),ϕ2(p,x)=ddk(2π)dik2sin(βDk22)pβDk22π1eDk2t2Γ(β2πDk2)eipe2πβt2eik(xx2)θ(p).\begin{split}\vec{\nabla}{\phi_{1}}(p,\vec{x})=&\int\frac{d^{d}\vec{k}}{(2\pi)^{d}}\frac{-i\vec{k}}{2\sin(\frac{\beta Dk^{2}}{2})}\frac{p^{\frac{\beta Dk^{2}}{2\pi}-1}e^{Dk^{2}t_{2}}}{\Gamma(\frac{\beta}{2\pi}Dk^{2})}e^{ipe^{\frac{2\pi}{\beta}t_{2}}+iph(\vec{x}-\vec{x}_{1})}e^{i\vec{k}\cdot(\vec{x}-\vec{x_{2}})}\theta(p),\\ \vec{\nabla}{\phi_{2}}(p,\vec{x})=&\int\frac{d^{d}\vec{k}}{(2\pi)^{d}}\frac{-i\vec{k}}{2\sin(\frac{\beta Dk^{2}}{2})}\frac{p^{\frac{\beta Dk^{2}}{2\pi}-1}e^{Dk^{2}t_{2}}}{\Gamma(\frac{\beta}{2\pi}Dk^{2})}e^{-ipe^{\frac{2\pi}{\beta}t_{2}}}e^{i\vec{k}\cdot(\vec{x}-\vec{x_{2}})}\theta(p).\end{split} (45)

Note that if we only keep the leading order terms in k2k^{2}, then the term sin(βDk22)\sin(\frac{\beta Dk^{2}}{2}) will cancel with Γ(β2πDk2)\Gamma(\frac{\beta}{2\pi}Dk^{2}). As long as we are considering large transverse coordinate separation, this approximation should be qualitatively correct. Plugging these into Eq. (27) and approximating RR+1\frac{R}{R_{+}}\sim 1, we obtain

(A1,A2)=1π𝑑pddxddk(2π)dddk(2π)d(kk)ppDk21eDk2t2pDk21eDk2t2e2ipet2eiph(xx1)ei(kk)(xx2).\begin{split}&(A_{1},A_{2})=\\ &\frac{1}{\pi}\int dp\int d^{d}\vec{x}\int\frac{d^{d}k}{(2\pi)^{d}}\int\frac{d^{d}k^{\prime}}{(2\pi)^{d}}(\vec{k}\cdot\vec{k^{\prime}})pp^{Dk^{2}-1}e^{Dk^{2}t_{2}}p^{Dk^{\prime 2}-1}e^{Dk^{\prime 2}t_{2}}e^{-2ipe^{t_{2}}}e^{-iph(\vec{x}-\vec{x_{1}})}e^{i(\vec{k^{\prime}}-\vec{k})\cdot(\vec{x}-\vec{x_{2}})}.\end{split} (46)

To save space, we have suppressed the factor β2π\frac{\beta}{2\pi} setting the units of time. After some changes of variable and approximations shown in Appendix B, we obtain the final expression for the OTOC as

(A1,A2)1[ln(2+ΔONe2πβt12μ|x12|)]d2.\begin{split}(A_{1},A_{2})\sim\frac{1}{\left[\ln{\left(2+\frac{\Delta_{O}}{N}e^{\frac{2\pi}{\beta}t_{12}-\mu|\vec{x}_{12}|}\right)}\right]^{\frac{d}{2}}}.\end{split} (47)

At early time, this expression admits a large NN expansion in which the leading term still grows exponentially with time. Moreover, one can identify the same Lyapunov exponent and butterfly velocity as in the non-conserved OTOC in Eq. (8). In the late time limit, the ln\ln of the exponentially growing part in the denominator gives rise to a power law time decay behavior. Hence, we find a significant difference from the OTOC of non-conserved operators in the late time regime.

3 Physical interpretation

In this section we try to understand the result in Eq. (47) in a more intuitive way. In the last section, we calculated the OTOC by integrating first over the radial momentum. Although this makes the calculation easier, the physical reason why we expect a power law decay at late time is somewhat obscured. As an alternative approach, we can perform the spatial momentum integral at the beginning and rewrite the integral in Eq. (46) as

0+𝑑sddx|(1(Ds)d2e|x|24Ds)|2e2iesei1Net12sμ|xx12|\int_{0}^{+\infty}ds\int d^{d}\vec{x}\left|\vec{\nabla}\left(\frac{1}{(Ds)^{\frac{d}{2}}}e^{\frac{-|\vec{x}|^{2}}{4Ds}}\right)\right|^{2}e^{-2ie^{-s}}e^{-i\frac{1}{N}e^{t_{12}-s-\mu|\vec{x}-\vec{x}_{12}|}} (48)

Here ss is defined as s=ln(et2p)s=\ln(\frac{e^{-t_{2}}}{p}) and we have cut-off the large momentum contribution for p>et2p>e^{-t_{2}}.

This formula has a direct physical interpretation. The squared term can be viewed as the photon’s wave function. From the solution Eq. (20), we see that the photon’s wave function is extended both in the radial direction and in the transverse directions. Although we obtain Eq. (48) in momentum space, it’s more inspiring to think of ss as the radial coordinate. Small values of ss correspond to regions close to the horizon, while larger values of ss correspond to regions further from the horizon. The last term is a phase induced by the gravitational scattering, and et12se^{t_{12}-s} measures the relative scattering energy of the two particles. Therefore, it is natural to think of the scattering between the photon’s large wave-packet and the scalar particle’s localized wave-packet as taking place over a large range of radial depths. Then as the scalar particle scans through the photon’s wave function, the colliding energy effectively becomes smaller and smaller.

The term in the middle can be thought of as a regulator for large momentum (small ss). Since we didn’t obtain the complete solution of the photon’s wave function in the black hole geometry, the regulator might be replaced by a more general function in the full solution. However, if we’re only interested in the late time behavior, meaning t12μ|x12|ln(N)t_{12}-\mu|\vec{x}_{12}|\gg\ln(N), then the integral in ss receives its dominate contribution from s>t12s>t_{12} due to the fast oscillation of the phase term for small ss. The regulator is therefore not important, and we can directly see that the result is proportional to 1t12d2\frac{1}{{t_{12}}^{\frac{d}{2}}}.

4 Correlator with stress-energy tensor

The low energy hydrodynamics of the stress-energy tensor shares some similarity with that of U(1)U(1) charge. In this section, we show that the OTOC has the same late time behavior. As shown in [42][43][44], in hydrodynamic limit, small perturbation of stress-energy tensor splits into sound and shear modes. The corresponding graviton wave functions in the bulk have a sound pole and a diffusive pole, respectively. The shear mode is relatively easier to analyze, as it involves less components of the metric perturbation, but we will see that they have the same qualitative effect on the OTOC in the late time regime.

As above, we take the k\vec{k} direction as the xx-axis. The shear modes consist of TtyT_{ty}, TxyT_{xy}. Here yy can be any direction perpendicular to xx, Sound modes are more involved, including TttT_{tt}, TtxT_{tx}, TxxT_{xx} and TyyT_{yy}. The shear and sound mode operators on the boundary excite bulk metric fluctuation corresponding to vector and scalar perturbations, respectively. Taking the operator TtyT_{ty} as an example, it sources the bulk metric perturbations htyh_{ty} and hyrh_{yr}. Other choices of non-zero metric components are related to this by a gauge transformation. The spherically symmetric choice of scalar perturbation sourced by TttT_{tt} involves htth_{tt}, htrh_{tr}, hxx=hyyh_{xx}=h_{yy}, and hrrh_{rr}. For simplicity, we mainly discuss the shear mode and comment on the sound mode in the end.

4.1 Wave function of graviton

For a given momentum k\vec{k}, choose the coordinate system such that the xx-axis is parallel to k\vec{k}. The shear modes involve the Tty(ω,k)T^{ty}(\omega,\vec{k}) and Txy(ω,k)T^{xy}(\omega,\vec{k}) components, and are described by

Txy=DTxTty,tTty+xTxy=0,\begin{split}&T^{xy}=-D_{T}\partial_{x}T^{ty},\\ &\partial_{t}T^{ty}+\partial_{x}T^{xy}=0,\end{split} (49)

which together imply

tTty=DTx2Tty.\partial_{t}T^{ty}=D_{T}\partial_{x}^{2}T^{ty}. (50)

In AdS/CFT, the dynamics of these modes can be found by solving the linearized Einstein equation,

δRμν=2dΛhμν,\delta R_{\mu\nu}=\frac{2}{d}\Lambda h_{\mu\nu}, (51)

where dd is the spacial dimension of boundary theory. hμνh_{\mu\nu} is the metric perturbation, δgμν=hμν\delta g_{\mu\nu}=h_{\mu\nu}. The equations are simplified if we set to zero all the components except htyh_{ty} and hryh_{ry}. Then there are only two independent equations,

(k2ω2f(R))hry+iωf(R)rhty=0,dRhry+1f(R)rhry+iωf(R)hty=0,\begin{split}(k^{2}-\frac{\omega^{2}}{f(R)})h^{y}_{r}+\frac{i\omega}{f(R)}\partial_{r}h^{y}_{t}=0,\\ \frac{d}{R}h^{y}_{r}+\frac{1}{f(R)}\partial_{r}h^{y}_{r}+\frac{i\omega}{f(R)}h^{y}_{t}=0,\end{split} (52)

where RR is the radial coordinate in the metric Eq. (10) and rr is the tortoise coordinate defined in Eq. (11). The two first order equations then lead to a second order differential equation for htyh^{y}_{t},

r2hty+rln(1Rd(ω2k2f))rhty+(ω2k2f)hty=0.\partial^{2}_{r}h^{y}_{t}+\partial_{r}\ln\left(\frac{1}{R^{d}(\omega^{2}-k^{2}f)}\right)\partial_{r}h^{y}_{t}+(\omega^{2}-k^{2}f)h^{y}_{t}=0. (53)

This equation is the same as equation in U(1)U(1) charge case except with d2d-2 replaced by dd (see Eq. (115)). Thus we have the same solution, except the diffusion constant DT=1d+1R+D_{T}=\frac{1}{d+1}R_{+} is different. Also, while the photon wave function excited by J0J_{0} is spherically symmetric in the boundary spatial plane, in this case, since the shear mode operator TtyT_{ty} contains a spatial index, it breaks the spherical symmetry. So we expect that the wave function given by Eq.(20) only captures the dependence on directions x\vec{x} satisfying xy\vec{x}\bot y. In the yy direction, the mode propagates as sound. To avoid the complexity of mixing sound and shear modes, we restrict to consider the string operator living in d1d-1 spatial dimensions, Ts(t,x):=+𝑑yTty(t,y,x)T^{s}(t,\vec{x}):=\int_{-\infty}^{+\infty}dyT_{ty}(t,y,\vec{x}). Note that the choice of line operators over point operators can change late-time exponents by shifting the effective dimension of space.

4.2 Interaction with the shockwave

We continue to focus on the OTOC between energy-momentum tensor and a scalar operator with large conformal dimension. As above, we approximate the shockwave as sourced by the heavy scalar without backreaction from the graviton. Then it remains to consider the evolution of the graviton wave function in the geometry. In the following, to distinguish the metric perturbation from the shockwave, we will use f(x)f(\vec{x}) as the displacement in the metric,

ds2=2guvdu[dvδ(u)f(x)du]+gxxdΩd.ds^{2}=2g_{uv}du[dv-\delta(u)f(\vec{x})du]+g_{xx}d\Omega_{d}. (54)

We solve the linearized equation

12(DρDμhνρ+DρDνhμρDρDρhμνDμDνhρρ)2dΛhμν=0.\frac{1}{2}(D_{\rho}D_{\mu}h^{\rho}_{\nu}+D_{\rho}D_{\nu}h^{\rho}_{\mu}-D_{\rho}D^{\rho}h_{\mu\nu}-D_{\mu}D_{\nu}h^{\rho}_{\rho})-\frac{2}{d}\Lambda h_{\mu\nu}=0. (55)

This is a very complicated equation in general. Some other components have to be generated even if we start with only the shear mode perturbation. However, if we restrict the shockwave term guug_{uu} to only depend on directions that are perpendicular to yy, the equation becomes easier to deal with. So we require SS to be a function of xix_{i} with xiy\vec{x}_{i}\bot y. Then the equations are simplified to

v[guv(vhuyuhvy)]+finite terms=0,guv(vihuy+uihvy)+2guvv[ihvyf(x)δ(u)]+finite terms=0,\begin{split}\partial_{v}[g^{uv}(\partial_{v}h_{u}^{y}-\partial_{u}h^{y}_{v})]+\text{finite terms}=0,\\ g^{uv}(\partial_{v}\partial_{i}h^{y}_{u}+\partial_{u}\partial_{i}h_{v}^{y})+2g^{uv}\partial_{v}[\partial_{i}h^{y}_{v}f(\vec{x})\delta(u)]+\text{finite terms}=0,\end{split} (56)

where ‘finite terms’ denotes terms that don’t contain a delta function. Here we are searching for a solution such that uhvy\partial_{u}h^{y}_{v} and huyh^{y}_{u} are proportional to δ(u)\delta(u). Requiring the cancellation of all δ(u)\delta(u)s, we find that

2guvuihvy+2guvv[ihvyf(x)δ(u)]=0.2g^{uv}\partial_{u}\partial_{i}h^{y}_{v}+2g^{uv}\partial_{v}[\partial_{i}h^{y}_{v}f(\vec{x})\delta(u)]=0. (57)

Hence, we again have the simple shift rule,

ihvy(v,x)ihvy(vf(x),x),\partial_{i}h^{y}_{v}(v,\vec{x})\rightarrow\partial_{i}h^{y}_{v}(v-f(\vec{x}),\vec{x}), (58)

after the graviton passing the shockwave. Finally, in order for ff to only depend on xy\vec{x}\bot y, we have to also consider a string operator built from the scalar Os(t,x)=𝑑yO(t,x,y)O^{s}(t,\vec{x})=\int dyO(t,\vec{x},y).

4.3 Inner product

As before, we construct the gauge invariant inner product using the symplectic form,

δ=δϕδδϕ+dθ(ϕ,δϕ).\delta\mathcal{L}=\delta\phi\frac{\delta\mathcal{L}}{\delta\phi}+d\theta(\phi,\delta\phi). (59)

We find that

(h1,h2)=gnρ[h1μνDμh2νρ+12h1μνDρh2μν+12h1ρνDνh2+12h1Dνh2ρν12h1Dρh2](12).\begin{split}&(h_{1},h_{2})=\\ &\int\sqrt{g}n^{\rho}[-h_{1}^{*\mu\nu}D_{\mu}{h_{2}}_{\nu\rho}+\frac{1}{2}h_{1}^{*\mu\nu}D_{\rho}{h_{2}}_{\mu\nu}+\frac{1}{2}{h_{1}^{*}}^{\nu}_{\rho}D_{\nu}{h_{2}}+\frac{1}{2}h_{1}^{*}D_{\nu}{h_{2}}^{\nu}_{\rho}-\frac{1}{2}h_{1}^{*}D_{\rho}h_{2}]-(1\longleftrightarrow 2).\end{split} (60)

Knowing that the trace of h1h_{1} and h2h_{2} are zero, we only keep the first two terms. Then, after some cancellations, a much simpler form remains

(h1,h2)=γgxxguv(h1vy[vh2u]yΓyvyh1[vyh2u]y)(12).(h_{1},h_{2})=\int\sqrt{\gamma}g^{xx}g^{uv}({h_{1}^{*}}_{v}^{y}\partial_{[v}{h_{2}}_{u]}^{y}-\Gamma^{y}_{yv}{h_{1}^{*}}_{[v}^{y}{h_{2}}_{u]}^{y})-(1\longleftrightarrow 2). (61)

We have chosen nn to be v\frac{\partial}{\partial_{v}}. This expression is very similar to the photon case (see Eq. (22)), except for second term, which is proportional to the connection. Then we observe that Γyvy\Gamma^{y}_{yv} is of order uu near the horizon, so if we choose to evaluate the inner product along the hyper-surface u0u\sim 0, the second term can be neglected.

4.4 OTOC of stress-energy tensor

4.4.1 Shear mode

Just like the U(1)U(1) case, the OTOC,

Tr(ρ12Ttys(t2,x2)Os(t1,x1)ρ12Ttys(t2,x2)Os(t1,x1)),Tr(\rho^{\frac{1}{2}}T^{s}_{ty}(t_{2},\vec{x}_{2})O^{s}(t_{1},\vec{x}_{1})\rho^{\frac{1}{2}}T^{s}_{ty}(t_{2},\vec{x}_{2})O^{s}(t_{1},\vec{x}_{1})), (62)

can be written as an inner product between the graviton wave functions, before and after passing the shockwave. Plugging the solution Eq. (20) and Eq. (58) into Eq. (61), we get exactly the same expression as in the U(1)U(1) case, and the subsequent calculation is completely parallel. Note that these string operators live in an effective d1d-1 spacial dimension. The exponent of power law tail is also modified to d12\frac{d-1}{2}.

4.4.2 Sound mode

We can also consider a local insertion of a stress-tensor operator that creates spherically symmetric wave function propagating in the bulk. At low energy, these modes have the dispersion relation of a sound wave. For instance, we can choose the insertion TttT_{tt} and i=1dTii\sum_{i=1}^{d}T_{ii}. The pole in the Green’s function is at

ω=±vskid1dDTk2,\omega=\pm v_{s}k-i\frac{d-1}{d}D_{T}k^{2}, (63)

where DTD_{T} is the diffusion constant (same as that of the shear mode). The quadratic term has the same effect as the shear mode, broadening the wave-packet. Hence, we expect the OTOC to have the same power law tail as in the photon case. Another interesting regime for the sound mode is at early time, where we have the shockwave that propagates at the butterfly velocity vBv_{B} as well as the hydrodynamical mode that propagates at the sound speed vsv_{s}. For the gravity model we considered in this work, vB>vsv_{B}>v_{s} for physically sensible spatial dimension. However, in other models the sound speed might be larger.222For example, in [45, 23] there is a case where vBv_{B} is small at low temperature. In this case we find that the information carried by sound mode can scramble faster, the spreading speed of which is determined by vsv_{s} instead. We solve the sound mode gravitaional perturbation equation and provide a detailed analysis of the OTOC in Appendix C.

5 Discussion and generalization

5.1 Higher order corrections

We have calculated the photon wave function by just keeping the leading order in ω\omega and kk. This gave an OTOC with a power law dependence on tt at large time. We may include higher order terms in the wave function, for example, consider

ϕ(ω,k)=i(1+Aω+Bk)ω+iDk2+Cω2+Dk3.\phi(\omega,k)=\frac{i(1+A\omega+Bk)}{\omega+iDk^{2}+C\omega^{2}+Dk^{3}}. (64)

The pole is now at

ω=iDk2(1+γk).\omega=-iDk^{2}(1+\gamma k). (65)

After Fourier transformation with respect to ω\omega, the wave function becomes

ϕ(v,k)=𝑑ωϕ(ω,k)eiωv,=(1+BkiADk2)vDk2(1+γk).\begin{split}\phi(v,k)=&\int d\omega\phi(\omega,k)e^{-i\omega v},\\ =&(1+Bk-iADk^{2})v^{-Dk^{2}(1+\gamma k)}.\end{split} (66)

Following the steps above, we should multiply the integrand of Eq. (46) by a factor (1+αk+βk2)(1+\alpha k+\beta k^{2}). Also we should modify the exponent of [2+f(x)et12][2+f(\vec{x})e^{t_{12}}] in second equation of Eq. (78) to Dk2(1+γk)-Dk^{2}(1+\gamma k). After performing integration with respect to kk, these modifications only contribute factors of higher order in t121t_{12}^{-1}, and do not change the leading long time behavior. One can also include loop corrections due to a graviton, as we discuss in Appendix D. This correction creates a branch cut in the wave function but doesn’t modify the long time behavior of the OTOC.

5.2 Hydrodynamics and OTOCs of non-conserved operator

In this section, we explore the question of how hydrodynamic modes may affect scrambling of non-conserved operators. In the process shown in Fig 4 (with the photon line representing either a photon mode or a sound mode), imagine that a massive scalar particle (created by a non-conserved operator) emits a hydrodynamic mode through a coupling of order O(gc)O(g_{c}) in the near boundary region. This mode grows in size as it falls into the black hole. The inin state before the shockwave scattering would contain a term gsfs(p,x)fm(p,x)|p,xs|p,xm|q,yg_{s}\int f_{s}(p,x)f_{m}(p^{\prime},x)|p,x^{\prime}\rangle_{s}|p^{\prime},x^{\prime}\rangle_{m}|q,y\rangle, where fsf_{s} is the sound mode wave function and fmf_{m} is the massive scalar wave function. The state with momentum qq is the second massive mode. The collidision induces a phase factor eiqph(x,y)+iqph(x,y)e^{iqph(x,y)+iqp^{\prime}h(x^{\prime},y)}. So we expect the scattering amplitude to be the one that involves hydrodynamic modes (like in Eq. (29)) multiplied with the one that involves only massive scalars. As discussed in the previous sections, the hydrodynamic OTOC has a power law tail at late time. However, the non-conserved OTOC is multiplied with it and the combination decays faster. Hence, the complete OTOC at late time is still controlled by massive particle scattering. On the other hand, the early time behavior can be modified, if we consider the non-conserved mode coupling with a sound mode, becuase the scattering amplitude between the sound mode and the second massive particle starts to decay earlier if vs>vBv_{s}>v_{B} (see Appendix C for details). Since the hydrodynamic mode’s wave function is created with amplitude O(gc)O(g_{c}), its influence on the OTOC is of order O(gc2)O(g_{c}^{2}). So even if vs>vBv_{s}>v_{B}, the fast propagating wave-front cannot grow to exceed the same order,

OTOC1c1Net|x|vBc2gc2Net|x|vs.OTOC\sim 1-\frac{c_{1}}{N}e^{t-\frac{|x|}{v_{B}}}-\frac{c_{2}g_{c}^{2}}{N}e^{t-\frac{|x|}{v_{s}}}. (67)
{feynman}\vertex\vertex\vertex\vertex\vertex\vertex\vertex\vertex\vertex\vertex\vertexgcg_{c}\vertexgcg_{c}\vertexgNg_{N}\vertexgNg_{N}\vertexgNg_{N}\vertexgNg_{N}\diagram
Figure 4: intermediate hydrodynamic state in scalar-scalar scattering

Since all modes couple to gravity, they also couple to the sound mode of the gravitational perturbation. In this case, gc21Ng_{c}^{2}\sim\frac{1}{N}, and the last term can grow with time up to order O(1N)O(\frac{1}{N}). A similar situation has been discussed in [22], where they gave a bound on the squared commutator of the form

squared commutatoret|x|vBN+a(x,t)N+O(1N2),\text{squared commutator}\leq\frac{e^{t-\frac{|x|}{v_{B}}}}{N}+\frac{a(x,t)}{N}+O(\frac{1}{N^{2}}), (68)

where the function a(x,t)a(x,t) is non-zero when |x|<vst|x|<v_{s}t, and is bounded by an O(1)O(1) quantity. However, the picture we considered here (Fig 4) is slightly different.

5.3 Summary

In conclusion, we have explored OTOCs between hydrodynamic operators and generic operators. In the late time regime, these OTOCs obey a power law scaling, while at early time the deviation still grows exponentially. In some models where the sound speed vsv_{s} is large, the information near the wave-front scrambles with a velocity that depends on vsv_{s}. Finally, when generalizing to OTOCs of generic operators that couple to hydrodynamic modes, we found that the late time power law decay is absent, while there can be a small amount of information scrambling faster than vBv_{B} (when vs>vBv_{s}>v_{B}) near the wave-front.

We can also understand the conclusion intuitively in the boundary picture. Starting with a non-conserved operator OO. A part of it evolves into gcJOg_{c}JO, where JJ represents a hydrodynamic operator. Then a small part of the information is carried by the hydrodynamic mode. A pure hydrodynamic operator JJ may spread fast (in sound mode case) but release its information slowly (which causes the late time power law tail). Therefore, although the order gc2g_{c}^{2} amount of information may propagate fast and lead to a rapidly moving wave-front in the OTOC, the scalar operator accompanied with JJ releases most of the information and breaks the power law tail at late time. Due to conservation law constraints, the dynamics prevents OO from turning into pure JJ’s. In bulk theory, this is a constraint from gauge symmetry.

6 Acknowledgements

This work is supported in part by the Simons Foundation through the It From Qubit Collaboration.

Appendix A Solution to the Maxwell-Einstein differential equation

In our metric, gtt=grr=R2f-g^{tt}=g^{rr}=\frac{R^{2}}{f} and g=R(d+2)f\sqrt{-g}=R^{-(d+2)}f. The Maxwell equation simplifies to

r2At+rln(1Rd2(ω2k2f))rAt+(ω2k2f)At=0\partial^{2}_{r}A_{t}+\partial_{r}\ln\left(\frac{1}{R^{d-2}(\omega^{2}-k^{2}f)}\right)\partial_{r}A_{t}+(\omega^{2}-k^{2}f)A_{t}=0 (69)

There is a singular point at f0f\rightarrow 0, where the equation becomes

r2At+ω2At=0\partial_{r}^{2}A_{t}+\omega^{2}A_{t}=0 (70)

with solution At(r,ω,k)eiωrA_{t}(r,\omega,k)\sim e^{-i\omega r}. We have picked the in-falling mode on this boundary. The ansatz

At(r,ω,k)=eiωrF(r,ω,k)A_{t}(r,\omega,k)=e^{-i\omega r}F(r,\omega,k) (71)

yields an equation for FF,

F′′2iλω^Frln[Rd2(ω^2k^2f)](Fiλω^F)+λ2(ω^2k^2f)F=0,F^{\prime\prime}-2i\lambda\hat{\omega}F^{\prime}-\partial_{r}\ln[R^{d-2}(\hat{\omega}^{2}-\hat{k}^{2}f)](F^{\prime}-i\lambda\hat{\omega}F)+\lambda^{2}(\hat{\omega}^{2}-\hat{k}^{2}f)F=0, (72)

where (ω,k)=(λω^,λk^)(\omega,k)=(\lambda\hat{\omega},\lambda\hat{k}) and λ1\lambda\ll 1.

The solution FF should have an expansion in the form F=F0+λF1+F=F_{0}+\lambda F_{1}+\cdots. The leading F0F_{0} satisfies

F0′′rln[Rd2(ω^2k^2f)]F0=0,F0=C0+C10r𝑑rRd2(ω^2k^2f).\begin{split}F_{0}^{\prime\prime}-\partial_{r}\ln[R^{d-2}(\hat{\omega}^{2}-\hat{k}^{2}f)]F_{0}^{\prime}=0,\\ \implies F_{0}=C_{0}+C_{1}\int_{0}^{r}dr^{\prime}R^{\prime d-2}(\hat{\omega}^{2}-\hat{k}^{2}f).\end{split} (73)

F0F_{0} goes like C1ω^2rC_{1}\hat{\omega}^{2}r as rr\rightarrow-\infty, so a regular solution should have C1=0C_{1}=0. Similarly, the first order term F1F_{1} should satisfy

F1′′2iω^F0rln[Rd2(ω^2k^2f)](F1iω^F0)=0.F_{1}^{\prime\prime}-2i\hat{\omega}F_{0}^{\prime}-\partial_{r}\ln[R^{d-2}(\hat{\omega}^{2}-\hat{k}^{2}f)](F_{1}^{\prime}-i\hat{\omega}F_{0})=0. (74)

The integration constant can be fixed by requiring regularity at horizon, then one obtains

F1=iω^C0r0r𝑑r[1Rd2(1k^2ω^2)f].F_{1}=i\hat{\omega}C_{0}\int_{r_{0}}^{r}dr^{\prime}[1-R^{\prime d-2}(1-\frac{\hat{k}^{2}}{\hat{\omega}^{2}})f]. (75)

To first order in λ\lambda, we find

At(r,ω,k)=C0{1+iωr0r𝑑r[1Rd2(1k^2ω^2)f]}.A_{t}(r,\omega,k)=C_{0}\{1+i\omega\int_{r_{0}}^{r}dr^{\prime}[1-R^{\prime d-2}(1-\frac{\hat{k}^{2}}{\hat{\omega}^{2}})f]\}. (76)

Appendix B Details of the OTOC calculation

Start from the inner product,

(A1,A2)=𝑑pddxddk(2π)dddk(2π)d(kk)ppDk21pDk21eip[2+ΔONet12μ|xx12|]ei(kk)x=ddxddk(2π)dddk(2π)d(kk)Γ[D(k2+k2)][2+ΔONet12μ|xx12|]D(k2+k2)ei(kk)x.\begin{split}&(A_{1},A_{2})\\ &=\int dp\int d^{d}\vec{x}\int\frac{d^{d}k}{(2\pi)^{d}}\int\frac{d^{d}k^{\prime}}{(2\pi)^{d}}(\vec{k}\cdot\vec{k^{\prime}})pp^{Dk^{2}-1}p^{Dk^{\prime 2}-1}e^{-ip\left[2+\frac{\Delta_{O}}{N}e^{t_{12}-\mu|\vec{x}-\vec{x}_{12}|}\right]}e^{i(\vec{k^{\prime}}-\vec{k})\cdot\vec{x}}\\ &=\int d^{d}\vec{x}\int\frac{d^{d}k}{(2\pi)^{d}}\int\frac{d^{d}k^{\prime}}{(2\pi)^{d}}(\vec{k}\cdot\vec{k^{\prime}})\Gamma[D(k^{2}+k^{\prime 2})]\left[2+\frac{\Delta_{O}}{N}e^{t_{12}-\mu|\vec{x}-\vec{x}_{12}|}\right]^{-D(k^{2}+k^{\prime 2})}e^{i(\vec{k^{\prime}}-\vec{k})\cdot\vec{x}}.\\ \end{split} (77)

As in the main text, we will just keep the leading order dependence in kk for the gamma function. We change the integration variables to K=k+k2K=\frac{k+k^{\prime}}{2} and κ=kk2\kappa=\frac{k-k^{\prime}}{2}. This gives

(A1,A2)ddxddK(2π)dddκ(2π)d2dK2κ22D(K2+κ2)[2+ΔONet12μ|xx12|]2D(K2+κ2)e2iκx=ddx(4π)d[dDd+1E(lng,|x|22D)12Dd+11(lng)de|x|22Dlng],\begin{split}(A_{1},A_{2})\sim&\int d^{d}\vec{x}\int\frac{d^{d}K}{(2\pi)^{d}}\int\frac{d^{d}\kappa}{(2\pi)^{d}}2^{d}\frac{K^{2}-\kappa^{2}}{2D(K^{2}+\kappa^{2})}\left[2+\frac{\Delta_{O}}{N}e^{t_{12}-\mu|\vec{x}-\vec{x}_{12}|}\right]^{-2D(K^{2}+\kappa^{2})}e^{-2i\kappa\cdot\vec{x}}\\ =&\int\frac{d^{d}x}{(4\pi)^{d}}\left[\frac{d}{D^{d+1}}E(\ln{g},\frac{|\vec{x}|^{2}}{2D})-\frac{1}{2D^{d+1}}\frac{1}{(\ln{g})^{d}}e^{-\frac{|\vec{x}|^{2}}{2D\ln g}}\right],\end{split} (78)

where gg and EE are defined as

g=2+ΔONet12μ|xx12|,E(z,a)=z𝑑y1yd+1eay.\begin{split}g=2+\frac{\Delta_{O}}{N}e^{t_{12}-\mu|\vec{x}-\vec{x}_{12}|},\\ E(z,a)=\int_{z}^{\infty}dy\frac{1}{y^{d+1}}e^{-\frac{a}{y}}.\end{split} (79)

Since both of the two terms contain e|x|22Dlnge^{-\frac{|\vec{x}|^{2}}{2D\ln g}}, we expect the integral to receive its dominant contribution from |x|0|x|\sim 0. Integrating x\vec{x} over this saddle point gives a factor of (2Dlng)d2(2D\ln g)^{\frac{d}{2}}. Therefore, we finally obtain

(A1,A2)1[ln(2+Δ𝒪Ne2πβtμ|x12|)]d2.(A_{1},A_{2})\propto\frac{1}{[\ln{(2+\frac{\Delta_{\mathcal{O}}}{N}e^{\frac{2\pi}{\beta}t-\mu|x_{12}|})}]^{\frac{d}{2}}}. (80)

In fact, the saddle point approximation in last step is only valid for very small diffusion constant DD and for not too large values of the function g(x)g(x). Thus it is necessary to discuss the late and early time limits separately from the above treatment. Looking back at Eq. (78), in the large t12t_{12} limit, t12LnN+|x12|vBt_{12}\gg LnN+\frac{|\vec{x}_{12}|}{v_{B}}. We can expand the function lngt12(1|x|vBt12)\ln{g}\sim t_{12}(1-\frac{|\vec{x}|}{v_{B}t_{12}}), for |x|<cvBt|x|<cv_{B}t, where cc is some finite constant smaller than 11. Then the integral over xx can be evaluated as

ddx1(lng)αe|x|22Dlng,=|x|<cvBtddx1t12α(1|x|t12)αe|x|22Dt12[1+O(|x|t12))]+|x|>cvBtddx1(lng)αe|x|22Dlng.\begin{split}&\int d^{d}\vec{x}\frac{1}{(\ln g)^{\alpha}}e^{-\frac{|x|^{2}}{2D\ln{g}}},\\ =&\int^{|x|<cv_{B}t}d^{d}\vec{x}\frac{1}{t_{12}^{\alpha}(1-\frac{|x|}{t_{12}})^{\alpha}}e^{-\frac{|x|^{2}}{2Dt_{12}}[1+O(\frac{|x|}{t_{12}}))]}+\int_{|x|>cv_{B}t}d^{d}\vec{x}\frac{1}{(\ln g)^{\alpha}}e^{-\frac{|x|^{2}}{2D\ln{g}}}.\end{split} (81)

For the first part, the change of variable to xx2Dt12x\rightarrow\frac{x}{\sqrt{2Dt_{12}}} gives

|x|<cvB2Dtddxt12d2α(1+O(|x|t12))e|x|2(1+O(|x|t12))t12d2α(1+O(t1212)).\int^{|x|<c\frac{v_{B}}{\sqrt{2D}}\sqrt{t}}d^{d}\vec{x}\ t_{12}^{\frac{d}{2}-\alpha}\ (1+O(\frac{|x|}{\sqrt{t_{12}}}))e^{-|x|^{2}(1+O(\frac{|x|}{\sqrt{t_{12}}}))}\sim t_{12}^{\frac{d}{2}-\alpha}(1+O(t_{12}^{-\frac{1}{2}})). (82)

The second part is bounded by

|x|>cvBtddx1(ln2)αe|x|22Dt12O(evB2t12D).\int_{|x|>cv_{B}t}d^{d}\vec{x}\frac{1}{(\ln{2})^{\alpha}}e^{-\frac{|x|^{2}}{2Dt_{12}}}\sim O(e^{-\frac{v_{B}^{2}t_{12}}{D}}). (83)

From these results, the late time amplitude indeed decays in a power law manner, and is consistent with the result Eq. (80).

(A1,A2)1|t12|d2.(A_{1},A_{2})\sim\frac{1}{|t_{12}|^{\frac{d}{2}}}. (84)

On the other hand, when t12|x21|vBlnNt_{12}-\frac{|\vec{x}_{21}|}{v_{B}}\ll\ln{N}, we expand lngln2+Δ𝒪2Net12|xx12|vB\ln{g}\sim\ln{2}+\frac{\Delta_{\mathcal{O}}}{2N}e^{t_{12}-\frac{|\vec{x}-\vec{x}_{12}|}{v_{B}}}, as well as

E(lng,a)E(ln2,a)+Δ𝒪2Net12|xx12|vBddzE(z,a)|z=ln2,E(ln2,a)12Net12|xx12|vB1(ln2)d+1ealn2.\begin{split}E(\ln{g},a)\sim&E(\ln{2},a)+\frac{\Delta_{\mathcal{O}}}{2N}e^{t_{12}-\frac{|\vec{x}-\vec{x}_{12}|}{v_{B}}}\frac{d}{dz}E(z,a)|_{z=\ln{2}},\\ \sim&E(\ln{2},a)-\frac{1}{2N}e^{t_{12}-\frac{|\vec{x}-\vec{x}_{12}|}{v_{B}}}\frac{1}{(\ln{2})^{d+1}}e^{-\frac{a}{\ln{2}}}.\end{split} (85)

The leading order deviation is

(A1,A2)1(ln2)d2[112Nd2ln2et12ddx~23(1+|x|2d)e|x~x~12/D|vB/D|x~|2]\begin{split}(A_{1},A_{2})\sim\frac{1}{(\ln{2})^{\frac{d}{2}}}\left[1-\frac{1}{2N}\frac{\frac{d}{2}}{\ln{2}}e^{t_{12}}\int d^{d}\tilde{x}\frac{2}{3}\left(1+\frac{|x|^{2}}{d}\right)e^{-\frac{|\tilde{x}-{\tilde{x}_{12}/\sqrt{D}}|}{v_{B}/\sqrt{D}}-|\tilde{x}|^{2}}\right]\end{split} (86)

This matches with the result Eq. (80), when expanding around small values of DD, because the integral in Eq. (86) is approximated by e|x12|vB+e|x12|2De^{-\frac{|x_{12}|}{v_{B}}}+e^{-\frac{|x_{12}|^{2}}{D}}. We can see that the velocity of the wave-front is still given by vBv_{B}. For completeness, we give the exact result of this integral in 1d,

e|x12|vB+D4vB2erf(D2vB|x12|D)(12+D12vB2)(D6vB+13|x12|D)e|x12|2D.e^{-\frac{|x_{12}|}{v_{B}}+\frac{D}{4v_{B}^{2}}}\text{erf}\left(\frac{\sqrt{D}}{2v_{B}}-\frac{|x_{12}|}{\sqrt{D}}\right)\left(\frac{1}{2}+\frac{D}{12v_{B}^{2}}\right)-\left(\frac{\sqrt{D}}{6v_{B}}+\frac{1}{3}\frac{|x_{12}|}{\sqrt{D}}\right)e^{-\frac{|x_{12}|^{2}}{D}}. (87)

Appendix C OTOCs of sound mode operators

In this section, we evaluate the OTOC between a sound mode operator (eg. TttT_{tt}, Txx+TyyT_{xx}+T_{yy}) and a scalar operator with large conformal dimension Δ\Delta. For this purpose, we first solve the sound mode equation in a symmetric gauge to second order of ω\omega and kk. By doing this, we obtain the dispersion relation as in [46] and the near horizon form of the wave function. Unlike in [46], we apply a gauge fixing condition that preserves boundary spatial rotational symmetry.

If the boundary source respects rotational symmetry (for example, consider a boundary insertion of TttT_{tt} or i=1dTii\sum_{i=1}^{d}T_{ii}), we expect a bulk configuration satisfying hti=hri=0h_{ti}=h_{ri}=0 and hijh_{ij} proportional to identity matrix, for i,j{1,,d}i,j\in\{1,\cdots,d\}. Without loss of generality, we will take d=2d=2 in the following. Then the non-zero components are htth_{tt},htrh_{tr}, hrrh_{rr} and hxx=hyyh_{xx}=h_{yy}. They satisfy a set of differential equations. Using the tortoise coordinate r=dRf(R)r=-\int\frac{dR}{f(R)}, and the Fourier decomposition hMN(r,t,x)=𝑑ω𝑑khMN(r,ω,k)eiωt+ikxh_{MN}(r,t,x)=\int d\omega dkh_{MN}(r,\omega,k)e^{-i\omega t+ikx}, these equations are written as

i(f+3)Rωhxx+k2R2htr+2iR2ωhxx2iRωhrr=0,-i(f+3)R\omega h_{\text{xx}}+k^{2}R^{2}h_{\text{tr}}+2iR^{2}\omega h_{\text{xx}}^{\prime}-2iR\omega h_{\text{rr}}=0, (88)
kR2ωhrrf+ikR2htrfkR2ωhxx=0,-\frac{kR^{2}\omega h_{\text{rr}}}{f}+\frac{ikR^{2}h_{\text{tr}}^{\prime}}{f}-kR^{2}\omega h_{\text{xx}}=0, (89)
kR(hrrhtt)f=0,\frac{kR\left(h_{\text{rr}}-h_{\text{tt}}\right)}{f}=0, (90)
2f2hxxR+(f+3)hrr2R(f+3)htt2Rfhxx+iωhtr+htt=0,\begin{split}\frac{2f^{2}h_{\text{xx}}}{R}+\frac{(f+3)h_{\text{rr}}}{2R}-\frac{(f+3)h_{\text{tt}}}{2R}-fh_{\text{xx}}^{\prime}+i\omega h_{\text{tr}}+h_{\text{tt}}^{\prime}=0,\end{split} (91)
(f+k2R2+3)hrrR2+(3fR2+k2)htt+(fk26fR2+ω2)hxxhrrR2iωhtrRhttR+hxx′′=0,\begin{split}-\frac{\left(f+k^{2}R^{2}+3\right)h_{\text{rr}}}{R^{2}}+\left(\frac{3-f}{R^{2}}+k^{2}\right)h_{\text{tt}}+\left(-fk^{2}-\frac{6f}{R^{2}}+\omega^{2}\right)h_{\text{xx}}-\frac{h_{\text{rr}}^{\prime}}{R}-\frac{2i\omega h_{\text{tr}}}{R}-\frac{h_{\text{tt}}^{\prime}}{R}+h_{\text{xx}}^{\prime\prime}=0,\end{split} (92)
htt′′+(7f9)htt2R+(f3)fhxxR(f3)hrr2R+2iωhtr+=0,\begin{split}h_{\text{tt}}^{\prime\prime}+\frac{(7f-9)h_{\text{tt}}^{\prime}}{2R}+\frac{(f-3)fh_{\text{xx}}^{\prime}}{R}-\frac{(f-3)h_{\text{rr}}^{\prime}}{2R}+2i\omega h_{\text{tr}}^{\prime}+\cdots=0,\end{split} (93)
htt′′2fhxx′′+3(f3)htt2R+3f(f+1)hxxR+3(f+1)hrr2R+2iωhtr+=0.h_{\text{tt}}^{\prime\prime}-2fh_{\text{xx}}^{\prime\prime}+\frac{3(f-3)h_{\text{tt}}^{\prime}}{2R}+\frac{3f(f+1)h_{\text{xx}}^{\prime}}{R}+\frac{3(f+1)h_{\text{rr}}^{\prime}}{2R}+2i\omega h_{\text{tr}}^{\prime}+\cdots=0. (94)

These seven equations are not independent. They reduce to three independent first order differential equations together with an algebraic equation, Eq. (90). Then the last three equations, Eq. (92)-(94), give an algebraic constraint,

ωhxx(r)(3f22f(k2R2+6)+4R2ω2+9)+ωhtt(r)(6f+2k2R2+6)iRhtr(r)((f3)k2+4ω2)=0.\omega h_{xx}(r)\left(3f^{2}-2f\left(k^{2}R^{2}+6\right)+4R^{2}\omega^{2}+9\right)+\omega h_{tt}(r)\left(-6f+2k^{2}R^{2}+6\right)-iRh_{tr}(r)\left((f-3)k^{2}+4\omega^{2}\right)=0. (95)

There are two independent solutions, with out-going and in-falling conditions near the horizon. To see this, make the substitution limrhμν(r)=eνrFμν\lim_{r\rightarrow-\infty}h_{\mu\nu}(r)=e^{\nu r}F_{\mu\nu} to the equations and take the limit R1R\rightarrow 1. The equations become

ν(FxxFtrFtt)=(32ik22ω100iω0iω0)(FxxFtrFtt)\nu\left(\begin{array}[]{c}F_{xx}\\ F_{tr}\\ F_{tt}\end{array}\right)=\left(\begin{array}[]{ccc}\frac{3}{2}&\frac{ik^{2}}{2\omega}&1\\ 0&0&-i\omega\\ 0&-i\omega&0\end{array}\right)\left(\begin{array}[]{c}F_{xx}\\ F_{tr}\\ F_{tt}\end{array}\right) (96)

There are three eigenvalues, (32,iω,iω)(\frac{3}{2},i\omega,-i\omega), corresponding to a spurious solution, out-going, and in-falling solutions, respectively. The eigenvalue 32\frac{3}{2} is discarded, since the corresponding eigenvector is not compatible with the constraint Eq. (95). The eigenvector of the in-falling solution tells us that

(FxxFtrFtt)=C(ω,k)(k22iωω(2ω3i)11).\left(\begin{array}[]{c}F_{xx}\\ F_{tr}\\ F_{tt}\end{array}\right)=C(\omega,k)\left(\begin{array}[]{c}-\frac{k^{2}-2i\omega}{\omega(2\omega-3i)}\\ 1\\ 1\end{array}\right). (97)

One can check that the gauge condition fixes the gauge completely. As a result, the in-falling solution is unique. To second order in momentum, we find the solution for hxxh_{xx}

hxx(r,ω,k)=C(ω,k)eiωr[23R+λcx1R𝑑Ri(k2f2ω2(1R2))3R2fω+λ2hxx(2)+O(λ3)]hxx(2)=1Rcx2R𝑑R[k2f2ω29R2fLn(f3)+4(k2ω2)k2R39R2f](4ω29k23)rω2r23\begin{split}h_{xx}(r,\omega,k)=C(\omega,k)e^{-i\omega r}[-\frac{2}{3R}+\lambda\int^{R}_{c_{x}^{1}}dR^{\prime}\frac{i(k^{2}f-2\omega^{2}(1-R^{\prime 2}))}{3R^{\prime 2}f\omega}+\lambda^{2}h_{xx}^{(2)}+O(\lambda^{3})]\\ h^{(2)}_{xx}=\frac{1}{R}\int^{R}_{c_{x}^{2}}dR^{\prime}[\frac{k^{2}f-2\omega^{2}}{9R^{\prime 2}f}Ln(\frac{f}{3})+\frac{4(k^{2}-\omega^{2})-k^{2}R^{\prime 3}}{9R^{\prime 2}f}]-\left(\frac{4\omega^{2}}{9}-\frac{k^{2}}{3}\right)r-\frac{\omega^{2}r^{2}}{3}\end{split} (98)

The integration constants cx1c_{x}^{1} and cx2c_{x}^{2} are fixed by requiring that the rr\rightarrow-\infty limit of hxxh_{xx} matches with Eq. (97).

The solution for htth_{tt} is

htt(r.ω,k)=C(ω,k)eiωr[13R2+23R+λ2+R3Rct1RdR3iωR4(2+R3)2f+λ2htt(2)+O(λ3)],\begin{split}h_{tt}(r.\omega,k)=C(\omega,k)e^{-i\omega r}[\frac{1}{3}R^{2}+\frac{2}{3R}+\lambda\frac{2+R^{3}}{R}\int^{R}_{c_{t}^{1}}dR^{\prime}\frac{3i\omega R^{\prime 4}}{(2+R^{\prime 3})^{2}f}+\lambda^{2}h^{(2)}_{tt}+O(\lambda^{3})],\end{split} (99)

where htt(2)h_{tt}^{(2)} is a complicated function. Again, the integration constants can be chosen according to Eq. (97). Finally, solution for htrh_{tr} is

htr(ω,k)=C(ω,k)eiωr[1iλω1R𝑑R1R2f+λ2(iω𝑑Rhtt(1)+fhxx(1)f+12ω2r2)+O(λ3)].h_{tr}(\omega,k)=C(\omega,k)e^{-i\omega r}[1-i\lambda\omega\int^{R}_{1}dR^{\prime}\frac{1-R^{\prime 2}}{f}+\lambda^{2}(-i\omega\int dR^{\prime}\frac{h_{tt}^{(1)}+fh_{xx}^{(1)}}{f}+\frac{1}{2}\omega^{2}r^{2})+O(\lambda^{3})]. (100)

Close to the boundary (r0r\rightarrow 0), httO(1r)h_{tt}\sim O(\frac{1}{r}), and hxxh_{xx} has the asymptotic form

hxx(1+iω3Ln(3))(2ω2k2)+4iω3(k2ω2)3iωr2+O(1r).h_{xx}\rightarrow\frac{(1+\frac{i\omega}{3}Ln(3))(2\omega^{2}-k^{2})+\frac{4i\omega}{3}(k^{2}-\omega^{2})}{-3i\omega r^{2}}+O(\frac{1}{r}). (101)

Therefore, for the boundary souce hxx0(ω,k)=hyy0(ω,k)=1h^{0}_{xx}(\omega,k)=h^{0}_{yy}(\omega,k)=1, we obtain the overall constant C(ω,k)=3iω(1+iω3Ln(3))(2ω2k2)+4iω3(k2ω2)C(\omega,k)=\frac{-3i\omega}{(1+\frac{i\omega}{3}Ln(3))(2\omega^{2}-k^{2})+\frac{4i\omega}{3}(k^{2}-\omega^{2})}. The near horizon limit of all the components is also clear. Due to rotational symmetry, the xx-axis can be any direction. So we have the following ansatz for the wave function, with the correct sound pole,

htt(r,t,x)=hrr(r,t,x)𝑑ωd2k32iω(13R3+23R)(ω212k2)+iω3k2eiω(t+r)+ikx,h_{tt}(r,t,\vec{x})=h_{rr}(r,t,\vec{x})\sim\int d\omega d^{2}\vec{k}\frac{-\frac{3}{2}i\omega(\frac{1}{3}R^{3}+\frac{2}{3R})}{(\omega^{2}-\frac{1}{2}k^{2})+\frac{i\omega}{3}k^{2}}e^{-i\omega(t+r)+i\vec{k}\cdot\vec{x}}, (102)
hxx(r,t,x)𝑑ωd2k1Riω(ω212k2)+iω3k2eiω(t+r)+ikx,h_{xx}(r,t,\vec{x})\sim\int d\omega d^{2}\vec{k}\frac{1}{R}\frac{i\omega}{(\omega^{2}-\frac{1}{2}k^{2})+\frac{i\omega}{3}k^{2}}e^{-i\omega(t+r)+i\vec{k}\cdot\vec{x}}, (103)
htr(r,t,x)𝑑ωd2k32iω(ω212k2)+iω3k2eiω(t+r)+ikx.h_{tr}(r,t,\vec{x})\sim\int d\omega d^{2}\vec{k}\frac{-\frac{3}{2}i\omega}{(\omega^{2}-\frac{1}{2}k^{2})+\frac{i\omega}{3}k^{2}}e^{-i\omega(t+r)+i\vec{k}\cdot\vec{x}}. (104)

Using this, we can estimate the late time tail of the sound mode OTOC, given that the inner product contains a term

γ𝑑vnv(h1xx(v)vh2xx(v)h2xx(v)vh1xx(v)),\int\sqrt{\gamma}dvn^{v}({h_{1}}_{xx}^{*}(v)\partial_{v}{h_{2}}_{xx}(v)-{h_{2}}_{xx}(v)\partial_{v}{h_{1}^{*}}_{xx}(v)), (105)

where h2xx(v)=h1xx(vh){h_{2}}_{xx}(v)={h_{1}}_{xx}(v-h) is a solution to the linearized Einstein equation on the shockwave background. The calculation is slightly different from the previous one due to the linear in kk term in the sound pole dispersion. In the end, it becomes the following integral

(h1,h2)ddxddk(2π)dddk(2π)ddp2πppDk21cos[vskln(p)]pDk21cos[vskLn(p)]G(p)eΔNet12μ|xx12|ei(kk)x,\begin{split}&(h_{1},h_{2})\\ \propto&\int d^{d}\vec{x}\int\frac{d^{d}\vec{k}}{(2\pi)^{d}}\frac{d^{d}\vec{k^{\prime}}}{(2\pi)^{d}}\int\frac{dp}{2\pi}pp^{Dk^{2}-1}\cos[v_{s}k\ln(p)]p^{Dk^{\prime 2}-1}\cos[v_{s}k^{\prime}Ln(p)]G(p)e^{-\frac{\Delta}{N}e^{t_{12}-\mu|\vec{x}-\vec{x}_{12}|}}e^{-i(\vec{k}-\vec{k^{\prime}})\cdot\vec{x}},\end{split} (106)

where we have introduced an unknown cutoff factor G(p)G(p) to regulate the large momentum behavior. Similar to the method in Section 3, one defines s=ln(p)s=-\ln(p) and performs the integral over the transverse momentum first. Then the inner product can be written as

ddx0+𝑑s1sd+1(e(|x|vss)24Ds+e(|x|+vss)24Ds)2eiΔNet12s|xx12|vBG(s),𝑑Ωd0+𝑑s1sd2+1eiΔNet12s|vssn^x12|vBG(s).\begin{split}&\int d^{d}\vec{x}\int_{0}^{+\infty}ds\frac{1}{s^{d+1}}(e^{-\frac{(|\vec{x}|-v_{s}s)^{2}}{4Ds}}+e^{-\frac{(|\vec{x}|+v_{s}s)^{2}}{4Ds}})^{2}e^{-i\frac{\Delta}{N}e^{t_{12}-s-\frac{|\vec{x}-\vec{x}_{12}|}{v_{B}}}}G(s),\\ \sim&\int d\Omega_{d}\int_{0}^{+\infty}ds\frac{1}{s^{\frac{d}{2}+1}}e^{-i\frac{\Delta}{N}e^{t_{12}-s-\frac{|v_{s}s\hat{n}-\vec{x}_{12}|}{v_{B}}}}G(s).\end{split} (107)

In the final, we performed the integral over |x||\vec{x}| assuming that it receives its dominant contribution around |x|vss|\vec{x}|\sim v_{s}s. The factor G(s)G(s) regulates small ss region. When t12t_{12} is large, the integral in ss becomes significant only when s>t12s>t_{12}. So we conclude that the late time OTOC has a power law tail.

It’s also interesting to discuss the early time regime, where we can expand the integrand in 1N\frac{1}{N}, and obtain

OTOC𝑑Ωd0+𝑑s1sd2+1G(s)(1iΔNet12s|vssn^x12|vB+)\text{OTOC}\sim\int d\Omega_{d}\int_{0}^{+\infty}ds\frac{1}{s^{\frac{d}{2}+1}}G(s)\left(1-\frac{i\Delta}{N}e^{t_{12}-s-\frac{|v_{s}s\hat{n}-\vec{x}_{12}|}{v_{B}}}+\cdots\right) (108)

We need to analyze the integral over ss. Denote the angle between n^\hat{n} and x12\vec{x}_{12} by θ\theta. The exponential reaches its maximum at s=x12vs(cosθsinθtanφ)s_{*}=\frac{x_{12}}{v_{s}}(\cos\theta-\sin\theta\tan\varphi), with φ=arcsinvBvs\varphi=\arcsin\frac{v_{B}}{v_{s}}. So for vB>vsv_{B}>v_{s}, or cosθ<vBvs\cos\theta<\frac{v_{B}}{v_{s}}, then s=0s_{*}=0, and we conclude that the information still scrambles at the speed vBv_{B}. On the other hand, for cosθ>vBvs\cos\theta>\frac{v_{B}}{v_{s}}, we expand s=s+ls=s_{*}+l and approximate the exponential factor as

et12s|vssn^x12|vBet12x12vs(cosθ+sinθcotφ)evscos3φ2x12sinθsinφl2.e^{t_{12}-s-\frac{|v_{s}s\hat{n}-\vec{x}_{12}|}{v_{B}}}\approx e^{t_{12}-\frac{x_{12}}{v_{s}}(\cos\theta+\sin\theta\cot\varphi)}e^{-\frac{v_{s}\cos^{3}\varphi}{2x_{12}\sin\theta\sin\varphi}l^{2}}. (109)

After integrating over ll, the O(1N)O(\frac{1}{N}) term becomes 333Since ss_{*} can be very large, this result is not sensitive to the regulator G(s)G(s). However, the constant term does depend on it, which will change the O(1N)O(\frac{1}{N}) term’s prefactor after normalization.

1N(x12vs)d+12et12x12vs(cosθ+sinθcotφ).\sim\frac{1}{N}(\frac{x_{12}}{v_{s}})^{-\frac{d+1}{2}}e^{t_{12}-\frac{x_{12}}{v_{s}}(\cos\theta+\sin\theta\cot\varphi)}. (110)

From this expression, we learn that when vs>vBv_{s}>v_{B}, a portion of the information, corresponding to solid angle θ0\theta_{0}, can scramble at a speed vscosθ0+sinθ0cotφ>vB\frac{v_{s}}{\cos\theta_{0}+\sin\theta_{0}\cot\varphi}>v_{B}, with cosθ0<sinφ=vBvs\cos\theta_{0}<\sin\varphi=\frac{v_{B}}{v_{s}}. For θ0\theta_{0} sufficiently small, the information spreading speed is close to speed of sound.

Appendix D Non-linear corrections

In this section, we consider the leading non-linear correction to the photon’s propogator. The correction is from graviton dressing, as shown in Fig. 5. Expanding the Einstein-Maxwell action, one obtains a gauge-gauge-graviton vertex of the following form,

1gc2dd+2xAμν[g(Fρνhρμ+Fμρhρν12Fμνhρρ)].\frac{1}{g_{c}^{2}}\int d^{d+2}xA_{\mu}\partial_{\nu}[\sqrt{-g}(F^{\rho\nu}h^{\mu}_{\rho}+F^{\mu\rho}h^{\nu}_{\rho}-\frac{1}{2}F^{\mu\nu}h^{\rho}_{\rho})]. (111)

Following [47], we consider the gravitational dressing in the near horizon region, and only include the interaction between the photon and the diffusive mode of the graviton. In other words, we only keep htxh_{tx} and hrxh_{rx} non-zero. Many terms in Eq. (111) are suppressed by small ω\omega and kk, so the leading order term involving AtA_{t} is

1gc2dd+2xggttgrrrAtFrxhtx.\frac{1}{g_{c}^{2}}\int d^{d+2}x\sqrt{-g}g^{tt}g^{rr}\partial_{r}A_{t}F_{rx}h^{x}_{t}. (112)
{feynman}\vertextt\vertex\vertex\vertextt\vertex\vertexFxrF_{xr}\vertexhtxh_{tx}\diagram
Figure 5: gravitational dressing to photon’s wave function

To be consistent with the main text, we still use the gauge Ax=0A_{x}=0. To find the bulk correlators, we have to solve the Maxwell-Einstein equation, Eq. (12), with a source term such that

At=dd+2xGtt(rr)Jt(r),Ar=dd+2xGrr(rr)Jr(r),\begin{split}A_{t}=\int d^{d+2}\vec{x}\ G_{tt}(\vec{r}-\vec{r}^{\prime})J^{t}(\vec{r}^{\prime}),\\ A_{r}=\int d^{d+2}\vec{x}\ G_{rr}(\vec{r}-\vec{r}^{\prime})J^{r}(\vec{r}^{\prime}),\end{split} (113)

where JtJ^{t} and JrJ^{r} are 4-vectors that satisfy

tJt+rJr+xJx=0.\partial_{t}J^{t}+\partial_{r}J^{r}+\partial_{x}J^{x}=0. (114)

To obtain GttG_{tt}, we require Jr=0J^{r}=0, and Jt(r,ω,k)=δ(rr)J^{t}(r,\omega,k)=\delta(r-r^{\prime}). Then Jx(r,ω,k)=ωkδ(rr)J^{x}(r,\omega,k)=\frac{\omega}{k}\delta(r-r^{\prime}). One can thenderive the following equation,

r2At+rln(1Rd2(ω2k2f))rAt+(ω2k2f)At=(ω2k2f)Rd2k2δ(rr).\partial^{2}_{r}A_{t}+\partial_{r}\ln\left(\frac{1}{R^{d-2}(\omega^{2}-k^{2}f)}\right)\partial_{r}A_{t}+(\omega^{2}-k^{2}f)A_{t}=\frac{(\omega^{2}-k^{2}f)R^{d-2}}{k^{2}}\delta(r-r^{\prime}). (115)

Applying the in-falling condition at the horizon and a Neumann boundary condition on the boundary, we obtain an approximate solution by expanding in small ω\omega and kk. Moreover, if we focus on the near horizon region, the solution takes a simple form,

Gtt(ω,k,r,r)ω2k2iωDk2(1+O(ωr)),Gtx,tx(ω,k,r,r)ω2k2iωDTk2(1+O(ωr)).\begin{split}&G_{tt}(\omega,k,r,r^{\prime})\sim\frac{\frac{\omega^{2}}{k^{2}}}{i\omega-Dk^{2}}(1+O(\omega r)),\\ &G_{tx,tx}(\omega,k,r,r^{\prime})\sim\frac{\frac{\omega^{2}}{k^{2}}}{i\omega-D_{T}k^{2}}(1+O(\omega r)).\\ \end{split} (116)

Similarly, to solve for GrrG_{rr}, we use a source such that Jt=0J_{t}=0, and Jr(r,ω,k)=δ(rr)J_{r}(r,\omega,k)=\delta(r-r^{\prime}). So we have Jx(r,ω,k)=1ikδ(rr)J^{x}(r,\omega,k)=\frac{1}{-ik}\delta(r-r^{\prime}), as well as the equation

r2A~r+rLog(Rd2)rA~r+(ω2k2f)A~r=ω2k2δ(rr),\partial^{2}_{r}\tilde{A}_{r}+\partial_{r}Log(R^{d-2})\partial_{r}\tilde{A}_{r}+(\omega^{2}-k^{2}f)\tilde{A}_{r}=\frac{\omega^{2}}{k^{2}}\delta(r-r^{\prime}), (117)

where A~r\tilde{A}_{r} contains a contact term and is defined as 1Rd2Ar+1k2δ(rr)\frac{1}{R^{d-2}}A_{r}+\frac{1}{k^{2}}\delta(r-r^{\prime}). In the near horizon region, one can also find that

Grr(r,r,ω.k)ω2k2iωDk2(1+O(ωr)).G_{rr}(r,r^{\prime},\omega.k)\sim\frac{\frac{\omega^{2}}{k^{2}}}{i\omega-Dk^{2}}(1+O(\omega r)). (118)

To simplify the calculation, we replace ω\omega by its value at the pole and set ω2k2\frac{\omega^{2}}{k^{2}} to Dk2Dk^{2}. Then we evaluate the bubble diagram by summing over imaginary frequencies and continuing to real frequency in the end,

Σtt(iωnω+i0+,k)=1Nddk(2π)dk2Tn𝒢rr(iωn,k)𝒢xt,xt(iωniωn,kk)|ıωnω+i0+1Nddk(2π)ddω2πk2[Grr(ω,k)ωGtx,tx(ωω,kk)+Grr(ω,k)Gtx,tx(ωω,kk)ωω]cNk2ω[iω+Dmk2]d21,\begin{split}&\Sigma_{tt}(i\omega_{n}\rightarrow\omega+i0^{+},k)=\frac{1}{N}\int\frac{d^{d}k^{\prime}}{(2\pi)^{d}}k^{\prime 2}T\sum_{n}\mathcal{G}_{rr}(i\omega^{\prime}_{n},k^{\prime})\mathcal{G}_{xt,xt}(i\omega_{n}-i\omega_{n}^{\prime},k-k^{\prime})|_{\i\omega_{n}\rightarrow\omega+i0^{+}}\\ \approx&\frac{1}{N}\int\frac{d^{d}k^{\prime}}{(2\pi)^{d}}\int\frac{d\omega^{\prime}}{2\pi}k^{\prime 2}[\frac{\Im{G_{rr}(\omega^{\prime},k^{\prime})}}{\omega^{\prime}}G_{tx,tx}(\omega-\omega^{\prime},k-k^{\prime})+G_{rr}(\omega^{\prime},k^{\prime})\frac{\Im G_{tx,tx}(\omega-\omega^{\prime},k-k^{\prime})}{\omega-\omega^{\prime}}]\\ \sim&\frac{c}{N}k^{2}\omega[-i\omega+D_{m}k^{2}]^{\frac{d}{2}-1},\end{split} (119)

where Dm=DDTD+DTD_{m}=\frac{DD_{T}}{D+D_{T}} is a mixed diffusion constant. The loop correction creates a branch cut along iω<Dmk2-i\omega<-D_{m}k^{2}, as expected by considering the on-shell condition of the two internal states. Then we suppose that the wave function in the near horizon region also receives a correction in the denominator, of the form

Atωω+iDk2cNk4ω[iω+Dmk2]d21.A_{t}\sim\frac{\omega}{\omega+iDk^{2}-\frac{c}{N}k^{4}\omega[-i\omega+D_{m}k^{2}]^{\frac{d}{2}-1}}. (120)

The branch cut structure is similar to that considered in [48]. Close to the line iω<Dmk2-i\omega<-D_{m}k^{2}, the pole is split into two poles, at ω=iDk2±αN|k|d+4\omega=-iDk^{2}\pm\frac{\alpha}{N}|k|^{d+4}. So the modification to real time functions is sub-leading in 1/|t|1/|t|. When going to the real time, we need to add a integral along a contour that circulates the branch cut. This integral is proportional to

Dmk2+𝑑sck4Ns(sDmk2)d21est(sDk2)2+c2k8s2N2(sDmk2)d2.\begin{split}&\int_{D_{m}k^{2}}^{+\infty}ds\frac{c\frac{k^{4}}{N}s(s-D_{m}k^{2})^{\frac{d}{2}-1}e^{-st}}{(s-Dk^{2})^{2}+c^{2}\frac{k^{8}s^{2}}{N^{2}}(s-D_{m}k^{2})^{d-2}}.\\ \end{split} (121)

The integrand is like a Lorentzian function, so we can estimate it by multiplying its peak height and width, which is again eDk2t(1+O(k2))e^{-Dk^{2}t}(1+O(k^{2})). So we conclude that the loop correction doesn’t change the conclusion in the main text.

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