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aainstitutetext: School of Physical Sciences, University of Chinese Academy of Sciences, Beijing 100049, Chinabbinstitutetext: School of Physics and Astronomy, Beijing Normal University, Beijing 100875, Chinaccinstitutetext: Key Laboratory of Multiscale Spin Physics, Ministry of Education, Beijing Normal University, Beijing 100875, China

Dynamical black hole entropy beyond general relativity from the Einstein frame

Delong Kong [email protected] a    Yu Tian [email protected] b,c    Hongbao Zhang [email protected] b,c    Jinan Zhao [email protected]
Abstract

Recently Hollands, Wald and Zhang proposed a new formula for the entropy of a dynamical black hole for an arbitrary theory of gravity obtained from a diffeomorphism covariant Lagrangian via the Noether charge methodHollands:2024vbe . We present an alternative, pedagogical derivation of the dynamical black hole entropy for f(R)f(R) gravity as well as canonical scalar-tensor theory by means of conformal transformations. First, in general relativity we generalize Visser and Yan’s pedagogical proof of the non-stationary physical process first law to black holes that may not be in vacuum, and give a pedagogical derivation of the second-order behavior of the dynamical black hole entropy for vacuum perturbations by considering the second-order variation of the Raychaudhuri equation. Second, we apply the derivation for general relativity to theories in the Einstein frames, and then recast the conclusions in their original frames. We show that the dynamical black hole entropy formulae of these theories satisfy both the non-stationary physical process first law and the non-stationary comparison first law via the Einstein frame. We further study the second-order behavior of the dynamical black hole entropy for vacuum perturbations, and observe that the second law is obeyed at second order in those theories. Using the Einstein frame, we also determine the relationship between the dynamical black hole entropy and the Wald entropy of the generalized apparent horizon in the original frame.

Keywords:
Black Holes, Classical Theories of Gravity

1 Introduction

The discovery of the laws of black hole thermodynamics is one of the great achievements of fundamental physicsBardeen:1973gs ; Bekenstein:1973ur ; Hawking:1975vcx . These laws combine gravity, quantum theory and thermodynamics within one stunning framework. Moreover, they provide some of the deepest insights on the fundamental nature of the quantum theory of gravity. For general relativity (GR), the black hole entropy SS is given by the Bekenstein-Hawking formulaBekenstein:1973ur ; Hawking:1975vcx

SBH=A4G,S_{\text{BH}}=\frac{A}{4G}, (1)

where AA is the area of the event horizon and GG is Newton’s constant. While for an arbitrary theory of gravity obtained from a diffeomorphism covariant Lagrangian, the entropy of a stationary black hole at the bifurcation surface \mathcal{B} is given by the Wald entropy, which is defined as the Noether charge and for the f(Riemann)f(\text{Riemann}) theories of gravity it is written asWald:1993nt ; Iyer:1994ys

SWald=8πdALRuvuv,S_{\text{Wald}}=-8\pi\int_{\mathcal{B}}\mathrm{d}A\ \frac{\partial L}{\partial R_{uvuv}}, (2)

where vv is the future-directed affine parameter of the null generator of the future horizon, uu denotes the affine null distance away from the horizon and is also future-directed. Furthermore, Iyer and Wald proposed a formula SIyer-WaldS_{\text{Iyer-Wald}} for dynamical black hole entropy on an arbitrary cross-section 𝒞\mathcal{C} of the horizon by expanding the Wald entropy in fields and their derivatives, and keeping the terms that depend only on boost-invariant fieldsIyer:1994ys . However, the second law of black hole mechanics does not seem to hold for SIyer-WaldS_{\text{Iyer-Wald}}. And that proposed dynamical entropy formula is not field redefinition invariant. Moreover, the Noether charge method used to derive the black hole entropy is subjected to a number of ambiguities for non-stationary black holes, identified by Jacobson, Kang and Myers (JKM)Jacobson:1993vj . Wall derived a second law for higher curvature gravity in a perturbative context, and resolved some ambiguities in Wald’s Noether charge methodWall:2015raa . For f(Riemann)f(\text{Riemann}) gravity the Wall entropy is given by

SWall=8π𝒞(v)dA(LRuvuv42LRuiujRvkvlKij(u)Kkl(v)).S_{\text{Wall}}=-8\pi\int_{\mathcal{C}(v)}\mathrm{d}A\left(\frac{\partial L}{\partial R_{uvuv}}-4\frac{\partial^{2}L}{\partial R_{uiuj}\partial R_{vkvl}}K_{ij(u)}K_{kl(v)}\right). (3)

Where Kij(a)K_{ij(a)} is the extrinsic curvature of the horizon in the aa direction. At the bifurcation surface both SIyer-WaldS_{\text{Iyer-Wald}} and SWallS_{\text{Wall}} reduce to SWaldS_{\text{Wald}}, and they are equal to SBHS_{\text{BH}} for general relativity.

Although the second law for SBHS_{\text{BH}} and the linearized second law for SWallS_{\text{Wall}} hold for non-stationary perturbations, this is not the case for the first law. The first law often does not hold for non-stationary perturbations of a stationary black hole, and if it does, the black hole entropy cannot be evaluated at an arbitrary cross-section of the event horizon of the perturbed non-stationary black holeVisser:2024pwz . Recently, Hollands, Wald and Zhang proposed a strategy to overcome these two limitationsHollands:2024vbe . They derived the first law by applying the Noether charge method to non-stationary perturbations of a stationary black hole background, and introduced a new program to the definition of dynamical black hole entropy valid to leading order, on the basis of the validity of a local, “physical process version” of the first law of black hole mechanics. Visser and Yan generalized and improved their work in a number of ways, and gave a more pedagogical proof of the physical process first law for black holes in general relativityVisser:2024pwz .

Next let us review the key results of Hollands:2024vbe for the dynamical black hole entropy and the non-stationary first law. For a non-stationary dynamical black hole, the entropy SS is no longer equal to the Bekenstein-Hawking entropy for GR or to the Wall entropy for higher curvature gravity. The formula for dynamical black holes differs from the usual Noether charge formula by a non-trivial dynamical correction term. For general relativity, the dynamical black hole entropy was defined as

Sdyn=(1vddv)SBH,S_{\text{dyn}}=\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)S_{\text{BH}}, (4)

where vv is the future-directed affine null parameter along the future horizon, and it is equal to 0 at the bifurcation surface \mathcal{B}. Notably, the derivative term is invariant under the scaling transformation of the affine parameter va(xi)vv\to a(x^{i})v, where xix^{i} are codimension-2 spatial coordinates on the horizon. It was also shown that, to leading order in perturbation theory, the formula of dynamical black hole entropy for general relativity is equal to the Bekenstein-Hawking entropy of the apparent horizon. Furthermore, the dynamical black hole entropy was generalized to higher curvature gravity asHollands:2024vbe

Sdyn=(1vddv)SWall.S_{\text{dyn}}=\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)S_{\text{Wall}}. (5)

By applying the Noether charge method to non-stationary perturbations, Hollands, Wald and Zhang have shown that their formula for dynamical black hole entropy satisfies both the non-stationary comparison first law and the non-stationary physical process first law. The non-stationary comparison version of the first law for an arbitrary horizon cross-section compares two vacuum black hole geometries

κ2πδSdyn[𝒞(v)]=δMΩδJ,\frac{\kappa}{2\pi}\delta S_{\text{dyn}}\left[\mathcal{C}(v)\right]=\delta M-\Omega_{\mathcal{H}}\delta J, (6)

where MM and JJ are the mass and angular momentum of the black hole, respectively. Ω\Omega_{\mathcal{H}} is the angular velocity of the horizon. And κ\kappa denotes the surface gravity of the black hole. For vacuum perturbations of a stationary black hole, the dynamical entropy is “time independent” to first order, i.e., δSdyn[𝒞(v)]=δSdyn[]\delta S_{\text{dyn}}[\mathcal{C}(v)]=\delta S_{\text{dyn}}[\mathcal{B}], where 𝒞(v)\mathcal{C}(v) is an arbitrary cross-section. In order to study the non-trivial time variation of black hole entropy, we may unseal an external stress-energy, δTab\delta T_{ab}, in the first-order perturbation. For perturbations sourced by external matter fields, the non-stationary physical process first law reads111Note that in the traditional treatments of the physical process first law, the black hole starts and ends in a stationary stateGao:2001ut ; Poisson:2009pwt .

κ2πΔδSdyn=v1v2dv𝒞(v)dAκvδTvv=ΔδMΩΔδJ,\frac{\kappa}{2\pi}\Delta\delta S_{\text{dyn}}=\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \kappa v\delta T_{vv}=\Delta\delta M-\Omega_{\mathcal{H}}\Delta\delta J, (7)

where Δ\Delta denotes the difference between two cross-sections 𝒞(v1)\mathcal{C}(v_{1}) and 𝒞(v2)\mathcal{C}(v_{2}), and δ\delta stands for the first-order perturbation around the stationary background. As a corollary of the physical process first law, the second law holds for the dynamical black hole entropy to first order as long as the stress-energy tensor satisfies the null energy condition δTvv0\delta T_{vv}\geq 0. While for vacuum perturbations we have to pay attention to second order in perturbation theory to study the leading-order change of the dynamical black hole entropy. And for vacuum perturbations the second law is obeyed at second order in general relativity since the “modified canonical energy flux” is positive for GR. However, in more general theories of gravity the “modified canonical energy flux” is not necessarily positive, and the second law presumably would not hold in more general theories of gravity for vacuum perturbations.

In this paper we present an alternative, pedagogical proof of both the non-stationary physical process first law and the non-stationary comparison first law for the f(R)f(R) gravity as well as the canonical scalar-tensor theory via conformal transformations. To begin with, we generalize Visser and Yan’s pedagogical derivation of the physical process first law for GR to black holes that may not be in vacuum. We also present a pedagogical deviation of the second-order behavior of SdynS_{\text{dyn}} for vacuum perturbations in GR by studying the second variation of the Raychaudhuri equation. Since conformal transformations preserve the causal structures of spacetimes, and the conformal factors that put theories into the Einstein frames are independent of the Killing time τ\tau in the stationary spacetimes, the spacetimes given by conformal transformations are stationary black hole solutions to the Einstein equation. We are capable of applying the proof of the first law for GR to theories in the Einstein frames, and then recast them in their original frames. As the perturbations are non-stationary, the gauge conditions for perturbations that fix the affine parameter vEv^{E} in the Einstein frame will not necessarily fix the affine parameter vv in the original frame. However, those gauge conditions do not restrict the way we perturb the stationary black hole background. Instead, they tell us how to identify spacetime points in the two slightly different spacetimes. We show that the switching from vEv^{E}-identification to vv-identification leads to second-order corrections, and the first laws are invariant to first order under the re-identification of spacetime points. For vacuum perturbations we further study the second-order behavior of the dynamical black hole entropy, and observe that the second law holds at second order both in the Einstein frames and in the original frames. Using the Einstein frame we also determine the relationship between the dynamical black hole entropy of the cross-section and the Wald entropy of the generalized apparent horizon in the original frame, which was not given before.

The rest of the paper is organized as follows. In section 2 we introduce the geometric setup and impose gauge conditions on perturbations. In Section 3 we generalize Visser and Yan’s pedagogical proof of the physical process first law for GR to non-vacuum solutions, and study the second-order behavior of the dynamical black hole entropy for vacuum perturbations. In Sections 4 and 5 we present the proof of both the physical process first law and the comparison first law for those theories, study the second-order behavior of the dynamical black hole entropy for vacuum perturbations, and determine the relationship between the dynamical black hole entropy and the Wald entropy of the generalized apparent horizon in the original frame. Section 6 is devoted to the summary of the paper and some discussions. In Appendix A we calculate the modified canonical energy flux for f(R)f(R) gravity via the covariant phase space formalism, and give a non-trivial check of the second-order behavior of SdynS_{\text{dyn}} for vacuum perturbations.

We will mainly follow the notation and conventions of Wald:1984rg . Throughout this paper, we set c==kB=1c=\hbar=k_{B}=1 while keep Newton’s constant GDG_{D} explicit.

2 Stationary black hole background and gauge conditions for perturbations

In this section we introduce the geometry of the stationary black hole background and impose gauge conditions on non-stationary perturbations used to study the first law. Our geometric setup mainly follows that of Visser:2024pwz .

+\mathcal{H}^{+}\mathcal{H}^{-}kak^{a}lal^{a}\mathcal{B}\ 𝒞(v)\mathcal{C}(v)ξa\xi^{a}
Figure 1: The stationary black hole background

Consider a stationary DD-dimensional stationary black hole background geometry (M,gab)(M,g_{ab}). We assume that the black hole spacetime is asymptotic flat and electrically neutral. The event horizon of this black hole coincides with the bifurcate Killing Horizon \mathcal{H}. We label the future horizon by +\mathcal{H}^{+}, the past horizon by \mathcal{H}^{-}, and the bifurcation surface by \mathcal{B}. The Killing field normal to the Killing horizon is denoted by ξa\xi^{a}, and it is a Killing symmetry of the metric gabg_{ab} as well as the matter fields ϕ\phi. i.e.,

ξgab=0,ξϕ=0.\mathcal{L}_{\xi}g_{ab}=0,\quad\mathcal{L}_{\xi}\phi=0. (8)

We are mainly interested in the part of +\mathcal{H}^{+} that lies to the future of \mathcal{B}. We can always erect a set of null zweibein bases (ka,la)(k^{a},l^{a}) on +\mathcal{H}^{+}, where kak^{a} is the future directed null normal to +\mathcal{H}^{+} and it is affinely parameterized as ka=+(v)ak^{a}\overset{\mathcal{H}^{+}}{=}(\partial_{v})^{a} with vv being set to 0 on \mathcal{B}, lal^{a} is an (future-directed) ingoing auxiliary null vector field and kala=1k^{a}l_{a}=-1 holds on the horizon. We can also extend lal^{a} off the horizon by solving lbbla=0l^{b}\nabla_{b}l^{a}=0 and denote the affine null distance away from +\mathcal{H}^{+} by uu to identify la=(u)al^{a}=(\partial_{u})^{a}. Finally, we can extend kak^{a} off the horizon such that it commutes with lal^{a}, i.e., [k,l]a=0\left[k,l\right]^{a}=0. Since ξbbξa=+κξa\xi^{b}\nabla_{b}\xi^{a}\overset{\mathcal{H}^{+}}{=}\kappa\xi^{a} and kbbka=+0k^{b}\nabla_{b}k^{a}\overset{\mathcal{H}^{+}}{=}0, we can scale kak^{a} properly such that

ξa=(τ)a=+Ceκτka=κvka,\xi^{a}=(\partial_{\tau})^{a}\overset{\mathcal{H}^{+}}{=}Ce^{\kappa\tau}k^{a}=\kappa vk^{a}, (9)

where CC is a constant. We can also decompose the metric on +\mathcal{H}^{+} as

gab=+kalblakb+γab,g_{ab}\overset{\mathcal{H}^{+}}{=}-k_{a}l_{b}-l_{a}k_{b}+\gamma_{ab}, (10)

where γab\gamma_{ab} is the intrinsic codimension-2 spatial metric of the cross-section 𝒞(v)\mathcal{C}(v) satisfying γab=γ(ab)\gamma_{ab}=\gamma_{(ab)} and γabka=+γabla=+0\gamma_{ab}k^{a}\overset{\mathcal{H}^{+}}{=}\gamma_{ab}l^{a}\overset{\mathcal{H}^{+}}{=}0.

We would like to perturb the stationary black hole background gabgab+δgabg_{ab}\to g_{ab}+\delta g_{ab} and the matter fields ϕϕ+δϕ\phi\to\phi+\delta\phi to study the first law for non-stationary variations, where δgab,δϕ𝒪(ϵ)\delta g_{ab},\ \delta\phi\sim\mathcal{O}(\epsilon) are of first order in the perturbation. Since the stationary black hole spacetime and the perturbed spacetime are different, there exists certain gauge freedoms about how we should establish the coordinate systems in the perturbed geometry and how to identify spacetime points in the two slightly different spacetimes. In order to simplify the deviation of the first law, we impose the following gauge conditions on perturbationsVisser:2024pwz :

  1. 1.

    The event horizon of the perturbed black hole is identified with the Killing horizon of the background geometry. And +\mathcal{H}^{+} is still described by u=0u=0 and \mathcal{H}^{-} described by v=0v=0 after the perturbation.

  2. 2.

    kak^{a} and lal^{a} are fixed under the perturbation

    δka=0,δla=0.\delta k^{a}=0,\quad\delta l^{a}=0. (11)

    and kak^{a} remains null normal to +\mathcal{H}^{+} and lal^{a} remains null everywhere under the perturbation, which together with the condition δ(kala)=0\delta(k^{a}l_{a})=0 yields the following conditions

    kaδgab=+0,laδgab=0.k^{a}\delta g_{ab}\overset{\mathcal{H}^{+}}{=}0,\quad l^{a}\delta g_{ab}=0. (12)

    We further require that kak^{a} is still affinely parameterized on +\mathcal{H}^{+} and lal^{a} affinely parameterized everywhere after the perturbation

    δ(kbbka)=+0,δ(lbbla)=0.\delta(k^{b}\nabla_{b}k^{a})\overset{\mathcal{H}^{+}}{=}0,\quad\delta(l^{b}\nabla_{b}l^{a})=0. (13)
  3. 3.

    The Killing vector field ξa\xi^{a} remains null and tangent to the geodesic generators of the perturbed black hole. Combining with ξaδgab=0\xi^{a}\delta g_{ab}\overset{\mathcal{H}}{=}0 means that δξa\delta\xi^{a} is proportional to kak^{a} on +\mathcal{H}^{+} and to lal^{a} on \mathcal{H}^{-}.

The gauge condition 1 simply means that we compare the event horizon of the perturbed black hole and the Killing horizon of the stationary background. Condition 2 tells us how to establish the u,vu,v coordinate systems in the perturbed spacetimes. Moreover, we identify points with identical coordinates in the two slightly different spacetimes. These conditions do not mean that the Killing field should be fixed under the perturbation. If we allow the surface gravity κ\kappa to vary, ξa\xi^{a} will change in the perturbed geometry.

3 Dynamical black hole entropy in general relativity

In this section, we present the formula for dynamical black hole entropy based on the non-stationary physical process first law in GR. This derivation is completed by means of integrating the linearized Raychaudhuri equation on the horizon between two arbitrary cross-sections. A similar derivation was given in Visser:2024pwz for black hole solutions to the vacuum Einstein equation. While our deviation is less restrictive since we allow the metric to couple to matter fields via the Einstein equation in the stationary background. For vacuum perturbations we also provide a pedagogical derivation of the second-order behavior of the dynamical black hole entropy by considering the second-order variation of the Raychaudhuri equation. We also note that a similar deduction for vacuum perturbations was established in Rignon-Bret:2023fjq before us.

Let us consider the stationary black hole background and the perturbed geometry introduced in the last section. The Raychaudhuri equation for the congruence of null geodesics on the future horizon +\mathcal{H}^{+} reads

dθdv=1D2θ2σabσab+ωabωabRabkakb.\frac{\mathrm{d}\theta}{\mathrm{d}v}=-\frac{1}{D-2}\theta^{2}-\sigma_{ab}\sigma^{ab}+\omega_{ab}\omega^{ab}-R_{ab}k^{a}k^{b}. (14)

As the black hole background is stationary, the expansion θ\theta and shear tensor σab\sigma_{ab} vanish in the unperturbed spacetime geometry. What’s more, the rotation tensor ωab\omega_{ab} is equal to 0 since kak^{a} is hypersurface orthogonal. With the aid of the Einstein equation, the last term of (14) can be written as

Rabkakb=8πGD(Tab12Tgab)kakb=8πGDTabkakb.R_{ab}k^{a}k^{b}=8\pi G_{D}\left(T_{ab}-\frac{1}{2}Tg_{ab}\right)k^{a}k^{b}=8\pi G_{D}T_{ab}k^{a}k^{b}. (15)

Where GDG_{D} is the DD-dimensional Newton’s constant. As a corollary of the Raychaudhuri equation combined with the Einstein equation, TabkakbT_{ab}k^{a}k^{b} is equal to zero on the horizon in the stationary geometry. Otherwise the last term on the right hand side of (14) would not be zeroPoisson:2009pwt . Physically this condition can be interpreted as matter cannot be flowing across the event horizon. We multiply the Raychaudhuri equation on both sides by κv\kappa v, integrate it over the future horizon between cross-sections 𝒞(v1)\mathcal{C}(v_{1}) and 𝒞(v2)\mathcal{C}(v_{2}), and then vary this equation. Since dθdv\frac{\mathrm{d}\theta}{\mathrm{d}v} and TabkakbT_{ab}k^{a}k^{b} vanish in the unperturbed geometry, δ\delta acts only on θ\theta on the left-hand side and only on RabR_{ab} on the right-hand side, and the right-hand side is left with 8πGDκvδTabkakb8\pi G_{D}\kappa v\delta T_{ab}k^{a}k^{b} due to our gauge condition δgabkakb=0\delta g_{ab}k^{a}k^{b}=0. Recalling that ξa=κvka\xi^{a}=\kappa vk^{a} on the future horizon, to first order the result is

κv1v2dv𝒞(v)dAvdδθdv=8πGDv1v2dv𝒞(v)dAδTabξakb,\kappa\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ v\frac{\mathrm{d}\delta\theta}{\mathrm{d}v}=-8\pi G_{D}\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\xi^{a}k^{b}, (16)

where dA=dD2xγ(x,v)\mathrm{d}A=\mathrm{d}^{D-2}x\sqrt{\gamma(x,v)} is the area element of the cross-section 𝒞(v)\mathcal{C}(v). Let x=(x1,xD2)x=(x^{1},\cdots x^{D-2}) be a coordinate system on 𝒞(v1)\mathcal{C}(v_{1}), we can extend this coordinate system to an arbitrary cross-section by requiring that all points on each null geodesic share the same values of (x1,xD2)(x^{1},\cdots x^{D-2}). To exchange the order of integrals in (16), define the function 𝒜(x,v)\mathcal{A}(x,v) on +\mathcal{H}^{+} asFlanagan:1999jp

𝒜(x,v)=exp[v1vdv~θ(x,v~)].\mathcal{A}(x,v)=\exp\left[\int_{v_{1}}^{v}\mathrm{d}\tilde{v}\ \theta(x,\tilde{v})\right]. (17)

The integral on the left hand side of (16) can then be split into

v1v2dv𝒞(v)dAvdδθdv=𝒞(v1)dAv1v2dv𝒜(x,v)vdδθdv,\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ v\frac{\mathrm{d}\delta\theta}{\mathrm{d}v}=\int_{\mathcal{C}(v_{1})}\mathrm{d}A\int_{v_{1}}^{v_{2}}\mathrm{d}v\ \mathcal{A}(x,v)v\frac{\mathrm{d}\delta\theta}{\mathrm{d}v}, (18)

and it can be integrated by parts

𝒞(v1)dAv1v2dvvdδθdv=𝒞(v1)dA[vδθ]v1v2𝒞(v1)dAv1v2dvδθ,\int_{\mathcal{C}(v_{1})}\mathrm{d}A\int_{v_{1}}^{v_{2}}\mathrm{d}v\ v\frac{\mathrm{d}\delta\theta}{\mathrm{d}v}=\int_{\mathcal{C}(v_{1})}\mathrm{d}A\left[v\delta\theta\right]_{v_{1}}^{v_{2}}-\int_{\mathcal{C}(v_{1})}\mathrm{d}A\int_{v_{1}}^{v_{2}}\mathrm{d}v\ \delta\theta, (19)

where we have used the fact that 𝒜(x,v)=1\mathcal{A}(x,v)=1 in the stationary background. On the right-hand side of this equation, we may pull the variation δ\delta to the front of the integrals as θ\theta vanishes on the horizon of the unperturbed black hole background. And the second term on the right-hand side is

δ𝒞(v1)dAv1v2dvθ=δ𝒞(v1)dAv1v2dv𝒜(x,v)vlnγ(x,v)=δ𝒞(v1)dD2xγ(x,v1)v1v2dvγ(x,v)γ(x,v1)vγ(x,v)γ(x,v)=δ𝒞(v1)dD2x[γ(x,v2)γ(x,v1)]=ΔδA.\begin{split}\delta\int_{\mathcal{C}(v_{1})}\mathrm{d}A\int_{v_{1}}^{v_{2}}\mathrm{d}v\ \theta&=\delta\int_{\mathcal{C}(v_{1})}\mathrm{d}A\int_{v_{1}}^{v_{2}}\mathrm{d}v\ \mathcal{A}(x,v)\partial_{v}\ln\sqrt{\gamma(x,v)}\\ &=\delta\int_{\mathcal{C}(v_{1})}\mathrm{d}^{D-2}x\sqrt{\gamma(x,v_{1})}\int_{v_{1}}^{v_{2}}\mathrm{d}v\ \frac{\sqrt{\gamma(x,v)}}{\sqrt{\gamma(x,v_{1})}}\frac{\partial_{v}\sqrt{\gamma(x,v)}}{\sqrt{\gamma(x,v)}}\\ &=\delta\int_{\mathcal{C}(v_{1})}\mathrm{d}^{D-2}x\left[\sqrt{\gamma(x,v_{2})}-\sqrt{\gamma(x,v_{1})}\right]\\ &=\Delta\delta A.\end{split} (20)

As a result, the left part of (16) reads

κv1v2dv𝒞(v)dAvdδθdv=κΔδ(𝒞(v)dA(1vθ)).\kappa\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ v\frac{\mathrm{d}\delta\theta}{\mathrm{d}v}=-\kappa\Delta\delta\left(\int_{\mathcal{C}(v)}\mathrm{d}A\ (1-v\theta)\right). (21)

Thus we obtain the non-stationary physical process first law between two arbitrary cross-sections for GR

κ2πΔδSdyn=v1v2dv𝒞(v)dAδTabξakb,\frac{\kappa}{2\pi}\Delta\delta S_{\text{dyn}}=\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\xi^{a}k^{b}, (22)

where SdynS_{\text{dyn}} is the dynamical black hole entropy of the cross-section of the horizon

Sdyn[𝒞]=14GD𝒞(v)dA(1vθ)=(1vddv)SBH.S_{\text{dyn}}[\mathcal{C}]=\frac{1}{4G_{D}}\int_{\mathcal{C}(v)}\mathrm{d}A\left(1-v\theta\right)=\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)S_{\text{BH}}. (23)

The matter Killing energy flux between two cross-sections 𝒞(v1)\mathcal{C}(v_{1}) and 𝒞(v2)\mathcal{C}(v_{2}), relative to the Killing field ξa\xi^{a}, is defined as

ΔE=v1v2dv𝒞(v)dATabξakb.\Delta E=\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ T_{ab}\xi^{a}k^{b}. (24)

And Δ\Delta denotes the difference between 𝒞(v1)\mathcal{C}(v_{1}) and 𝒞(v2)\mathcal{C}(v_{2}). By the argument similar to (16), if we vary ΔE\Delta E, δ\delta acts only on TabT_{ab}. It was shown by Hawking that if a black hole is stationary, then it must be either static or axisymmetricHawking:1971vc . If the horizon Killing field is normalized as ξa=(t)a+Ω(θ)a\xi^{a}=\left(\partial_{t}\right)^{a}+\Omega_{\mathcal{H}}\left(\partial_{\theta}\right)^{a}, where (t)a\left(\partial_{t}\right)^{a} represents time translations at infinity, (θ)a\left(\partial_{\theta}\right)^{a} represents the rotational Killing vector and Ω\Omega_{\mathcal{H}} is the angular velocity of the black hole, then the mass and angular momentum transferred across the horizon arePoisson:2009pwt

ΔδMH=v1v2dv𝒞(v)dAδTab(t)akb,ΔδJH=v1v2dv𝒞(v)dAδTab(θ)akb.\begin{split}\Delta\delta M_{H}&=\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\left(\partial_{t}\right)^{a}k^{b},\\ \Delta\delta J_{H}&=-\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\left(\partial_{\theta}\right)^{a}k^{b}.\end{split} (25)

The matter Killing energy flux is then related to the change in mass and angular momentum of the black hole as222We emphasize that the mass and the angular momentum of the black hole are not equal to those of the spacetime if the black hole is not in vacuum. The matter distribution outside the black hole also contributes to the total mass and total angular momentum of the spacetime.

v1v2dv𝒞(v)dAδTabξakb=ΔδMHΩΔδJH.\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\xi^{a}k^{b}=\Delta\delta M_{H}-\Omega_{\mathcal{H}}\Delta\delta J_{H}. (26)

Therefore, the physical process first law reads

κ2πΔδSdyn=ΔδMHΩΔδJH.\frac{\kappa}{2\pi}\Delta\delta S_{\text{dyn}}=\Delta\delta M_{H}-\Omega_{\mathcal{H}}\Delta\delta J_{H}. (27)

As the first corollary of the physical process first law, if the perturbation of the stress-energy tensor satisfies the null energy condition δTabkakb0\delta T_{ab}k^{a}k^{b}\geq 0, for first-order perturbations sourced by external matter fields, the “linearized” second law holds for the dynamical black hole entropy

ΔδSdyn0.\Delta\delta S_{\text{dyn}}\geq 0. (28)

And as the second corollary, for source-free perturbations of a stationary black hole, the comparison first law holds between an arbitrary cross-section 𝒞(v)\mathcal{C}(v) and the spatial infinity i0i_{0}

κ2πδSdyn[𝒞(v)]=δMΩδJ,\frac{\kappa}{2\pi}\delta S_{\text{dyn}}[\mathcal{C}(v)]=\delta M-\Omega_{\mathcal{H}}\delta J, (29)

where MM and JJ are ADM definitions of the mass and angular momentum of the spacetime, respectively. This is because ΔδSdyn=0\Delta\delta S_{\text{dyn}}=0 for source-free perturbations δTab=0\delta T_{ab}=0, SdynS_{\text{dyn}} equals the usual Bekenstein-Hawking entropy at the bifurcation surface, and it has been proven that Bekenstein-Hawking entropy satisfies the comparison first law at the bifurcation surface. It is noteworthy that this relation still holds if matter fields are present as long as the combined Einstein-matter system admits a Hamiltonian formulationWald:1995yp ; Sudarsky:1992ty .

In the case of vacuum perturbations there are no external matter fields and δTab=0\delta T_{ab}=0. Then (22) indicates that the dynamical black hole entropy is a constant at first order in perturbation theory. So we have to keep track of the second order in perturbation theory to study the leading-order behavior of the dynamical black hole entropy. Hollands, Wald and Zhang obtained the leading-order behavior in that case based on the varied fundamental identity of the covariant phase space formalismHollands:2024vbe . In what follows we are going to present a different derivation of the second-order behavior of SdynS_{\text{dyn}} by considering the second variation of the Raychaudhuri equationRignon-Bret:2023fjq .

For vacuum perturbations, the first-order variation of (14) is

ddvδθ=δRabkakb=0.\frac{\mathrm{d}}{\mathrm{d}v}\delta\theta=\delta R_{ab}k^{a}k^{b}=0. (30)

Thus the perturbed expansion δθ\delta\theta is a constant along the null generators of +\mathcal{H}^{+}. Recalling that θ\theta vanishes at future infinity in the perturbed spacetime due to the teleological definition of the event horizon, the perturbed expansion δθ\delta\theta must vanish on +\mathcal{H}^{+}Hollands:2012sf . We then consider the second-order variation of (14) to obtain

ddvδ2θ=2δσabδσab.\frac{\mathrm{d}}{\mathrm{d}v}\delta^{2}\theta=-2\delta\sigma_{ab}\delta\sigma^{ab}. (31)

We multiply this equation on both sides by κv\kappa v, integrate over the future horizon between 𝒞(v1)\mathcal{C}(v_{1}) and 𝒞(v2)\mathcal{C}(v_{2}), and integrate the left hand side by parts in the same way shown above

κ𝒞(v1)dA[vδ2θ]v1v2κ𝒞(v1)dAv1v2dvδ2θ=2v1v2dv𝒞(v)dAκv(δσabδσab).\kappa\int_{\mathcal{C}(v_{1})}\mathrm{d}A\left[v\delta^{2}\theta\right]_{v_{1}}^{v_{2}}-\kappa\int_{\mathcal{C}(v_{1})}\mathrm{d}A\int_{v_{1}}^{v_{2}}\mathrm{d}v\ \delta^{2}\theta=-2\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \kappa v\left(\delta\sigma_{ab}\delta\sigma^{ab}\right). (32)

What’s more, on the left hand side of this equation we may pull δ2\delta^{2} to the front of the integrals as both θ\theta and δθ\delta\theta vanish. Finally the result is

κ2πΔδ2Sdyn=14πGDv1v2dv𝒞(v)dAκv(δσabδσab).\frac{\kappa}{2\pi}\Delta\delta^{2}S_{\text{dyn}}=\frac{1}{4\pi G_{D}}\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \kappa v\left(\delta\sigma_{ab}\delta\sigma^{ab}\right). (33)

Our result agrees with that derived by varying the fundamental identity of the covariant phase space formalismHollands:2024vbe . The term δσabδσab\delta\sigma_{ab}\delta\sigma^{ab} can be interpreted as the energy flux of the weak gravitational wavesAshtekar:2021kqj . Since δσabδσab0\delta\sigma_{ab}\delta\sigma^{ab}\geq 0, the second law holds at second order for vacuum perturbations of GR.

4 Dynamical black hole entropy in f(R)f(R) gravity

In this section we derive both the non-stationary physical process first law and the non-stationary comparison first law for f(R)f(R) gravity using the Einstein frame. Our results and and the dynamical black hole entropy formula for f(R)f(R) gravity agree with those derived by means of the Noether charge methodHollands:2024vbe ; Visser:2024pwz . For vacuum perturbations we also study the second-order behavior of the dynamical black hole entropy, and observe that the second law is obeyed both in the Einstein frame and in the original frame. What’s more, we determine the relationship between the dynamical black hole entropy of the cross-section 𝒞\mathcal{C} and the Wald entropy of the generalized apparent horizon 𝒯\mathcal{T} in the original frame.

4.1 The conformal transformation and the Einstein frame

The f(R)f(R) gravity is described by the action

If=116πGDdDxgf(R).I_{f}=\frac{1}{16\pi G_{D}}\int\mathrm{d}^{D}x\sqrt{-g}f(R). (34)

And in this paper, we assume that333We impose f(R)>0f^{\prime}(R)>0 to ensure that the effective gravitational coupling strength Geff=G/f(R)G_{\text{eff}}=G/f^{\prime}(R) for the f(R)f(R) theory is positiveSotiriou:2008rp ; Nojiri:2017ncd . On the other hand, if f′′(R)=0f^{\prime\prime}(R)=0, then f(R)f(R) is linear to RR, and the resulting theory is reduced to GR.

f(R)>0,f′′(R)0.f^{\prime}(R)>0,\quad f^{\prime\prime}(R)\neq 0. (35)

We invent an auxiliary scalar field φ\varphi to write the action (34) in an equivalent form

I~f=116πGDdDxg[f(φ)R+f(φ)φf(φ)],\tilde{I}_{f}=\frac{1}{16\pi G_{D}}\int\mathrm{d}^{D}x\sqrt{-g}\left[f^{\prime}(\varphi)R+f(\varphi)-\varphi f^{\prime}(\varphi)\right], (36)

because with the on-shell condition φ=R\varphi=R, this action reduces to the original one. To utilize the conclusions of the last section, we turn to the Einstein frame and redefine the scalar field as followsBarrow:1988xh ; Whitt:1984pd

gabE[f(φ)]2D2gab,ϕ116πGD2(D1)D2lnf(φ).g^{E}_{ab}\equiv\left[f^{\prime}(\varphi)\right]^{\frac{2}{D-2}}g_{ab},\quad\phi\equiv\frac{1}{\sqrt{16\pi G_{D}}}\sqrt{\frac{2\left(D-1\right)}{D-2}}\ln f^{\prime}(\varphi). (37)

As a result, the equivalent action (36) can be rewritten as

I~f=dDxgE[RE16πGD12gEabaϕbϕV(ϕ)],\tilde{I}_{f}=\int\mathrm{d}^{D}x\sqrt{-g^{E}}\left[\frac{R^{E}}{16\pi G_{D}}-\frac{1}{2}g_{E}^{ab}\partial_{a}\phi\partial_{b}\phi-V(\phi)\right], (38)

where

V(ϕ)116πGD[f(φ)]DD2(φf(φ)f(φ)).V(\phi)\equiv\frac{1}{16\pi G_{D}\left[f^{\prime}(\varphi)\right]^{\frac{D}{D-2}}}\left(\varphi f^{\prime}(\varphi)-f(\varphi)\right). (39)

Obviously, the action (38) is the Einstein-Hilbert action coupled to the canonical scalar field ϕ\phi with the potential V(ϕ)V(\phi).

Since the conformal transformation preserves the causal structure of the spacetime, and gabEg^{E}_{ab} is asymptotically flat as long as gabg_{ab} is asymptotically flat, the conformal transformation (37) of an asymptotically flat black hole spacetime remains an asymptotically flat black hole spacetime with the same event horizon, at least the conformal factor is regular on the horizonJacobson:1993pf ; Jacobson:1995uq . Moreover, the conformal factor ω=[f(φ)]1D2=[f(R)]1D2\omega=\left[f^{\prime}(\varphi)\right]^{\frac{1}{D-2}}=\left[f^{\prime}(R)\right]^{\frac{1}{D-2}} is independent of the Killing time τ\tau in the stationary black hole spacetime, so the conformal transformation (37) of a stationary black hole solution is still a stationary black hole solution, with the horizon Killing field given by ξa\xi^{a} up to a normalization factor. If the horizon Killing field ξa\xi^{a} is normalized as ξa=(t)a+Ω(θ)a\xi^{a}=(\partial_{t})^{a}+\Omega_{\mathcal{H}}(\partial_{\theta})^{a} with (t)a(\partial_{t})^{a} representing time translations at infinity in the original frame, we normalize ξEa=αξa\xi_{E}^{a}=\alpha\xi^{a} with the normalization constant α\alpha determined by

gabE(tE)a(tE)b|r=gabE[α(t)a][α(t)b]|r=[f(0)]2D2α2=1,\left.g^{E}_{ab}(\partial_{t^{E}})^{a}(\partial_{t^{E}})^{b}\right|_{r\to\infty}=\left.g^{E}_{ab}\left[\alpha(\partial_{t})^{a}\right]\left[\alpha(\partial_{t})^{b}\right]\right|_{r\to\infty}=-\left[f^{\prime}(0)\right]^{\frac{2}{D-2}}\alpha^{2}=-1, (40)

such that (tE)a=α(t)a=[f(0)]1D2(t)a(\partial_{t^{E}})^{a}=\alpha(\partial_{t})^{a}=\left[f^{\prime}(0)\right]^{-\frac{1}{D-2}}(\partial_{t})^{a} generates time translations at infinity in the Einstein frame. With the choice α=[f(0)]1D2\alpha=\left[f^{\prime}(0)\right]^{-\frac{1}{D-2}}, we can investigate the relation of the surface gravity of the black hole in the Einstein frame κE\kappa^{E} to that in the original frame κ\kappa. Notice that

aE(gbcEξEbξEc)=a(ω2α2gbcξbξc)=+ω2α2a(gbcξbξc)=+2ω2α2κgabξb=2κEgabEξEb.\begin{split}\nabla^{E}_{a}\left(g^{E}_{bc}\xi_{E}^{b}\xi_{E}^{c}\right)&=\nabla_{a}\left(\omega^{2}\alpha^{2}g_{bc}\xi^{b}\xi^{c}\right)\overset{\mathcal{H}^{+}}{=}\omega^{2}\alpha^{2}\nabla_{a}\left(g_{bc}\xi^{b}\xi^{c}\right)\\ &\overset{\mathcal{H}^{+}}{=}-2\omega^{2}\alpha^{2}\kappa g_{ab}\xi^{b}=-2\kappa^{E}g^{E}_{ab}\xi_{E}^{b}.\end{split} (41)

Therefore the relation between κE\kappa^{E} and κ\kappa reads κE=ακ=[f(0)]1D2κ\kappa^{E}=\alpha\kappa=\left[f^{\prime}(0)\right]^{-\frac{1}{D-2}}\kappa. After the conformal transformation, the null affine parameter vEv^{E} on the horizon in the Einstein frame is related to that in the original frame vv byWald:1984rg

dvEdv=c[fR(v,x)]2D2,\frac{\mathrm{d}v^{E}}{\mathrm{d}v}=c\left[f_{R}(v,x)\right]^{\frac{2}{D-2}}, (42)

where cc is an arbitrary constant and fR(v,x)f_{R}(v,x) is the value of f(φ)=f(R)f^{\prime}(\varphi)=f^{\prime}(R) at (v,x)(v,x) on the horizon. As a result,

vE=c0vdv[fR(v,x)]2D2.v^{E}=c\int_{0}^{v}\mathrm{d}v^{\prime}\left[f_{R}(v^{\prime},x)\right]^{\frac{2}{D-2}}. (43)

Since 0=τf(R)=κvvfR(v,x)0=\partial_{\tau}f^{\prime}(R)=\kappa v\partial_{v}f_{R}(v,x) in the stationary background, fR(v,x)f_{R}(v,x) does not depend on vv, so vEv^{E} is proportional to vv on the horizon of the stationary black hole.

4.2 The physical process first law

Since null geodesics are conformally invariant and the Einstein equation holds for gabEg^{E}_{ab} in the Einstein frame, the derivation of Sec.3 is still tenable for f(R)f(R) gravity in the Einstein frame. Let

𝒯ab=TabE+aϕbϕgabE[12gEcdcϕdϕ+V(ϕ)]\mathcal{T}_{ab}=T^{E}_{ab}+\partial_{a}\phi\partial_{b}\phi-g^{E}_{ab}\left[\frac{1}{2}g_{E}^{cd}\partial_{c}\phi\partial_{d}\phi+V(\phi)\right] (44)

denote the sum of the stress-energy tensor of the external matter fields in the Einstein frame TabE=2gEδSMδgEab=Tab/fR(v,x)T^{E}_{ab}=-\frac{2}{\sqrt{-g^{E}}}\frac{\delta S_{M}}{\delta g_{E}^{ab}}=T_{ab}/f_{R}(v,x) as well as that of the auxiliary scalar field. Notice that

δ𝒯abξEakEb=+δTabEξEakEb+2aϕ(bδϕ)ξEakEbδgabE[12gEcdcϕdϕ+V(ϕ)]ξEakEbgabEδ[12gEcdcϕdϕ+V(ϕ)]ξEakEb=+δTabEξEakEb,\begin{split}\delta\mathcal{T}_{ab}\xi_{E}^{a}k_{E}^{b}&\overset{\mathcal{H}^{+}}{=}\delta T^{E}_{ab}\xi_{E}^{a}k_{E}^{b}+2\partial_{a}\phi\left(\partial_{b}\delta\phi\right)\xi_{E}^{a}k_{E}^{b}\\ &-\delta g^{E}_{ab}\left[\frac{1}{2}g_{E}^{cd}\partial_{c}\phi\partial_{d}\phi+V(\phi)\right]\xi_{E}^{a}k_{E}^{b}\\ &-g^{E}_{ab}\delta\left[\frac{1}{2}g_{E}^{cd}\partial_{c}\phi\partial_{d}\phi+V(\phi)\right]\xi_{E}^{a}k_{E}^{b}\\ &\overset{\mathcal{H}^{+}}{=}\delta T^{E}_{ab}\xi_{E}^{a}k_{E}^{b},\end{split} (45)

where we have used the fact that kEaaϕ=0k_{E}^{a}\partial_{a}\phi=0 and gabEkakb|+=0\left.g^{E}_{ab}k^{a}k^{b}\right|_{\mathcal{H}^{+}}=0 in the stationary background as well as the gauge condition δgabkEakEb=+0\delta g_{ab}k_{E}^{a}k_{E}^{b}\overset{\mathcal{H}^{+}}{=}0 for the perturbations. Thus, only the variation of the external matter fields contributes to the first-order variation of 𝒯ab\mathcal{T}_{ab}. For perturbations satisfying the gauge conditions listed in Sec.2 that fix kEak_{E}^{a} on the horizon, the non-stationary physical process first law for f(R)f(R) gravity in the Einstein frame reads

κE2πΔδSdynE=v1Ev2EdvE𝒞(vE)dAEδTabEξEakEb,\frac{\kappa^{E}}{2\pi}\Delta\delta S^{E}_{\text{dyn}}=\int_{v^{E}_{1}}^{v^{E}_{2}}\mathrm{d}v^{E}\int_{\mathcal{C}(v^{E})}\mathrm{d}A^{E}\ \delta T^{E}_{ab}\xi_{E}^{a}k_{E}^{b}, (46)

where the dynamical black hole entropy formula for f(R)f(R) gravity in the Einstein frame is given by

SdynE[𝒞]=14GD(1vEddvE)𝒞(vE)dD2xγES^{E}_{\text{dyn}}[\mathcal{C}]=\frac{1}{4G_{D}}\left(1-v^{E}\frac{\mathrm{d}}{\mathrm{d}v^{E}}\right)\int_{\mathcal{C}(v^{E})}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}} (47)

with γE=γ[f(R)]2\gamma^{E}=\gamma\left[f^{\prime}(R)\right]^{2} representing the determinant of the induced metric on 𝒞(vE)\mathcal{C}(v^{E}) in the Einstein frame.

Next we would like to recast the physical process first law and the formula for the dynamical black hole entropy in the original frame. As the perturbation performed on the black hole is non-stationary, the gauge conditions that fix kEak_{E}^{a} will not generally fix kak^{a} in the original frame. Since for non-stationary perturbations, fR(x,v)f_{R}(x,v) is not necessary a constant along the null geodesics on +\mathcal{H}^{+} and vEv^{E} presumably would not be proportional to vv accordingly. While as mentioned in Section 2, the essence of those gauge conditions lies in how to identify spacetime points in two slightly different spacetimes. Those gauge conditions that fix kEak_{E}^{a} under the perturbations imply that we correspond points with the same vEv^{E} in the two spacetimes. To rewrite (46) and (47) in the original frame, in what follows we are going to compare spacetime points sharing the same vv on the horizon, and replace vEv^{E} with vv in the formula of SdynES^{E}_{\text{dyn}}.

Without loss of generality, in the following discussion we set vE=vv^{E}=v in the stationary background, and perform the conformal transformation (37) on the perturbed geometry gab+δgabg_{ab}+\delta g_{ab} to obtain the non-stationary black hole solution in the Einstein frame. Then vE=v+δV(x,v)v^{E}=v+\delta V(x,v) on the horizon according to (43) in the perturbed geometry, where δV(x,v)\delta V(x,v) is a correction function derived from expanding the conformal factor ω2=[fR(x,v)]2D2\omega^{2}=\left[f_{R}(x,v)\right]^{\frac{2}{D-2}} with respect to the non-stationary perturbation of the metric, and it is of first order in perturbation theory. To begin with, let F(v,x)F(v,x) represent a quantity on the horizon, such as the entropy SdynS_{\text{dyn}} or the component of the stress-energy tensor Tvv(v,x)T_{vv}(v,x), which is stationary in the background, and let F~(v,x)\tilde{F}(v,x) denote the corresponding quantity in the perturbed spacetime, then δF(v,x)=F~(v,x)F(v,x)\delta F(v,x)=\tilde{F}(v,x)-F(v,x) does not change to first order as we switch from vEv^{E}-identification to vv-identification, because

δvEFδvF=F~(v+δV,x)F~(v,x)vF~δV=𝒪(ϵ2),\delta_{v^{E}}F-\delta_{v}F=\tilde{F}(v+\delta V,x)-\tilde{F}(v,x)\sim\partial_{v}\tilde{F}\ \delta V=\mathcal{O}(\epsilon^{2}), (48)

where δv\delta_{v} stands for the comparison between points with the same vv in the stationary background and in the perturbed spacetime, and the same connotation holds for δvE\delta_{v^{E}}. We have also used that vF~\partial_{v}\tilde{F} is of first order in the perturbed spacetime as FF is stationary in the unperturbed background. Therefore (46) does not change to first order under the re-identification of spacetime points. In addition, although the difference δV\delta V between vv and vEv^{E} leads to first-order corrections to the integral over vv and to the null generator kak^{a} in the perturbed geometry, the right hand side of (46) will not change to first order if we replace kak^{a} by kEak_{E}^{a} and replace v1Ev2EdvE\int_{v^{E}_{1}}^{v^{E}_{2}}\mathrm{d}v^{E} by v1v2dv\int_{v_{1}}^{v_{2}}\mathrm{d}v, since δTabE\delta T^{E}_{ab} is a first-order small quantity and this substitution leads to second-order corrections. Moreover, in the perturbed geometry,

SdynE=14GD(1vEdvdvEddv)𝒞dD2xγE=14GD[1(v+δV)(1dδVdvE)ddv]𝒞dD2xγE=14GD(1vddv)𝒞dD2xγE+𝒪(ϵ2),\begin{split}S^{E}_{\text{dyn}}&=\frac{1}{4G_{D}}\left(1-v^{E}\frac{\mathrm{d}v}{\mathrm{d}v^{E}}\frac{\mathrm{d}}{\mathrm{d}v}\right)\int_{\mathcal{C}}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}}\\ &=\frac{1}{4G_{D}}\left[1-\left(v+\delta V\right)\left(1-\frac{\mathrm{d}\delta V}{\mathrm{d}v^{E}}\right)\frac{\mathrm{d}}{\mathrm{d}v}\right]\int_{\mathcal{C}}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}}\\ &=\frac{1}{4G_{D}}\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)\int_{\mathcal{C}}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}}+\mathcal{O}(\epsilon^{2}),\end{split} (49)

where we have used ddv𝒞dD2xγE𝒪(ϵ)\frac{\mathrm{d}}{\mathrm{d}v}\int_{\mathcal{C}}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}}\sim\mathcal{O}(\epsilon) in the third line. Thus replacing vEv^{E} with vv in (47) leads to second-order corrections. For perturbations left kak^{a} invariant on the horizon, we rewrite (46) in the original frame as

κ2πΔδSdyn=v1v2dv𝒞(v)dAδTabξakb,\frac{\kappa}{2\pi}\Delta\delta S_{\text{dyn}}=\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\xi^{a}k^{b}, (50)

where SdynS_{\text{dyn}} is given by

Sdyn[𝒞]=14GD(1vddv)𝒞(v)dD2xγf(R).S_{\text{dyn}}[\mathcal{C}]=\frac{1}{4G_{D}}\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)\int_{\mathcal{C}(v)}\mathrm{d}^{D-2}x\sqrt{\gamma}f^{\prime}(R). (51)

Our results agree with those obtained by means of the Noether charge methodHollands:2024vbe ; Visser:2024pwz . Moreover, if the stress-energy tensor of the external matter field satisfies the null energy condition δTabkakb0\delta T_{ab}k^{a}k^{b}\geq 0, the dynamical black hole entropy will obey the linearized second law ΔδSdyn0\Delta\delta S_{\text{dyn}}\geq 0 under the perturbation.

4.3 The comparison first law

The conformal transformation (37) can also be used to derive the non-stationary comparison first law for f(R)f(R) gravity. As shown above, the variation of the auxiliary scalar field does not contribute to the first-order variation of 𝒯ab\mathcal{T}_{ab}. For source-free perturbations of the stationary black hole δTabE=0\delta T^{E}_{ab}=0, in the Einstein frame we write down the comparison first law for an arbitrary cross-section (29) as

κE2πδSdynE[𝒞(vE)]=δMEΩδJE.\frac{\kappa^{E}}{2\pi}\delta S^{E}_{\text{dyn}}[\mathcal{C}(v^{E})]=\delta M^{E}-\Omega_{\mathcal{H}}\delta J^{E}. (52)

Since the asymptotic forms of gabg_{ab} and gabEg^{E}_{ab} agree up to a normalization factor, the mass and angular momenta of the two spacetimes agree up to a normalization factor according to the Iyer-Wald definitionsJacobson:1995uq ; Iyer:1994ys . And the angular velocities are in agreement as ξEaξa\xi_{E}^{a}\propto\xi^{a}. One can determine the relationship between MEM^{E} and MM as ME=αMM^{E}=\alpha M since the time translations at infinity are related as (tE)a=α(t)a(\partial_{t^{E}})^{a}=\alpha(\partial_{t})^{a}, and similarly we have JE=αJJ^{E}=\alpha J. Notice that κE=ακ\kappa^{E}=\alpha\kappa, δSdyn\delta S_{\text{dyn}} does not change to first order as we switch from vEv^{E}-identification to vv-identification, and SdynES^{E}_{\text{dyn}} remains unchanged to first order if we use vv instead of vEv^{E} in the formula. The comparison first law for an arbitrary cross-section is translated into the claim in the original frame as

κ2πδSdyn[𝒞(v)]=δMΩδJ.\frac{\kappa}{2\pi}\delta S_{\text{dyn}}[\mathcal{C}(v)]=\delta M-\Omega_{\mathcal{H}}\delta J. (53)

4.4 The second law for vacuum perturbations

For vacuum perturbations we have no external matter fields and δTab=0\delta T_{ab}=0, so the dynamical black hole entropy is invariant to first order. In order to study the non-trivial leading-order behavior of SdynS_{\text{dyn}}, we have to pay attention to the second order in perturbation theory. The first-order variation of the Raychaudhuri equation in the Einstein frame reads

ddvEδθE=0.\frac{\mathrm{d}}{\mathrm{d}v^{E}}\delta\theta^{E}=0. (54)

Because θE\theta^{E} vanishes asymptotically at late times, δθE=0\delta\theta^{E}=0 holds on +\mathcal{H}^{+}. Vary the Raychaudhuri equation combined with the Einstein equation twice to obtain444Notice that the stress-energy tensor of the auxiliary scalar field contributes to the second-order variation of 𝒯ab\mathcal{T}_{ab}.

ddvEδ2θE=2δσabEδσEab16πGD(kEaaδϕ)2.\frac{\mathrm{d}}{\mathrm{d}v^{E}}\delta^{2}\theta^{E}=-2\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}-16\pi G_{D}\left(k_{E}^{a}\partial_{a}\delta\phi\right)^{2}. (55)

And then integrating this equation on +\mathcal{H}^{+} between 𝒞(v1E)\mathcal{C}(v^{E}_{1}) and 𝒞(v2E)\mathcal{C}(v^{E}_{2}) returns

κE2πΔδ2SdynE=14πGDv1Ev2EdvE𝒞(vE)dAEκEvE[δσabEδσEab+8πGD(kEaaδϕ)2].\frac{\kappa^{E}}{2\pi}\Delta\delta^{2}S^{E}_{\text{dyn}}=\frac{1}{4\pi G_{D}}\int_{v^{E}_{1}}^{v^{E}_{2}}\mathrm{d}v^{E}\int_{\mathcal{C}(v^{E})}\mathrm{d}A^{E}\ \kappa^{E}v^{E}\left[\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}+8\pi G_{D}\left(k_{E}^{a}\partial_{a}\delta\phi\right)^{2}\right]. (56)

Since δσabEδσEab0\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}\geq 0 and (kEaaδϕ)20\left(k_{E}^{a}\partial_{a}\delta\phi\right)^{2}\geq 0, for vacuum perturbations, the dynamical black hole entropy satisfies the second law at the second order in the Einstein frame. In what follows we would like to explore the second-order behavior of the dynamical black hole entropy for vacuum perturbations in the original frame based on this equation.

First, (56) is invariant to second order in the perturbation theory as we decide to compare spacetime points sharing the same vv rather than vEv^{E} on the horizon. Since by the argument similar to that of (48), switching from vEv^{E}-identification to vv-identification for δSdyn\delta S_{\text{dyn}} and δ2Sdyn\delta^{2}S_{\text{dyn}} leads to third-order corrections as vSdyn𝒪(ϵ2)\partial_{v}S_{\text{dyn}}\sim\mathcal{O}(\epsilon^{2}), and altering the identification of spacetime points also leads to third-order corrections on the right hand side of (56). Moreover, for vacuum perturbations SdynES^{E}_{\text{dyn}} is invariant to second order if we replace vEv^{E} with vv in the formula. As SdynES^{E}_{\text{dyn}} is a constant to first order under the vacuum perturbations, in the perturbed spacetime

(1vEddvE)SBHE=C+𝒪(ϵ2),\left(1-v^{E}\frac{\mathrm{d}}{\mathrm{d}v^{E}}\right)S^{E}_{\text{BH}}=C+\mathcal{O}(\epsilon^{2}), (57)

where SBHE=14GD𝒞dD2xγES^{E}_{\text{BH}}=\frac{1}{4G_{D}}\int_{\mathcal{C}}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}} is the Bekenstein-Hawking entropy in the Einstein frame and CC is a constant. Requiring that SBHES^{E}_{\text{BH}} remains finite at future infinity vEv^{E}\to\infty in the perturbed spacetime leads to the conclusion that

SBHE=C+𝒪(ϵ2)S^{E}_{\text{BH}}=C+\mathcal{O}(\epsilon^{2}) (58)

Thus ddvESBHE\frac{\mathrm{d}}{\mathrm{d}v^{E}}S^{E}_{\text{BH}} is of second order for vacuum perturbations, and replacing vEv^{E} with vv in the expression of SdynES^{E}_{\text{dyn}} leads to third-order corrections.

Next, we wish to rewrite (56) in the original frame. Notice that δθE=+0\delta\theta^{E}\overset{\mathcal{H}^{+}}{=}0 for vacuum perturbations in the Einstein frame. In the original frame we have

δvln[γf(R)]=f(R)vδγ+γf′′(R)vδRγf(R)=δθ+f′′(R)f(R)vδR=+0.\begin{split}\delta\partial_{v}\ln\left[\sqrt{\gamma}f^{\prime}(R)\right]=\frac{f^{\prime}(R)\partial_{v}\delta\sqrt{\gamma}+\sqrt{\gamma}f^{\prime\prime}(R)\partial_{v}\delta R}{\sqrt{\gamma}f^{\prime}(R)}=\delta\theta+\frac{f^{\prime\prime}(R)}{f^{\prime}(R)}\partial_{v}\delta R\overset{\mathcal{H}^{+}}{=}0.\end{split} (59)

As a result, to first order δσabE\delta\sigma^{E}_{ab} in the original frame reads

δσabE=12kEδγabE1D2δθEγab=12[f(φ)]2D2kδγab+1D2[f(φ)]2D2f′′(φ)f(φ)γabkδφ=[f(φ)]2D2[12kδγab1D2δθγab]=[f(φ)]2D2δσab,\begin{split}\delta\sigma^{E}_{ab}&=\frac{1}{2}\mathcal{L}_{k^{E}}\delta\gamma^{E}_{ab}-\frac{1}{D-2}\delta\theta^{E}\gamma_{ab}\\ &=\frac{1}{2}\left[f^{\prime}(\varphi)\right]^{\frac{2}{D-2}}\mathcal{L}_{k}\delta\gamma_{ab}+\frac{1}{D-2}\left[f^{\prime}(\varphi)\right]^{\frac{2}{D-2}}\frac{f^{\prime\prime}(\varphi)}{f^{\prime}(\varphi)}\gamma_{ab}\mathcal{L}_{k}\delta\varphi\\ &=\left[f^{\prime}(\varphi)\right]^{\frac{2}{D-2}}\left[\frac{1}{2}\mathcal{L}_{k}\delta\gamma_{ab}-\frac{1}{D-2}\delta\theta\gamma_{ab}\right]\\ &=\left[f^{\prime}(\varphi)\right]^{\frac{2}{D-2}}\delta\sigma_{ab},\end{split} (60)

where the second equality follows from δθE=+0\delta\theta^{E}\overset{\mathcal{H}^{+}}{=}0 as well as γabE=[f(φ)]2D2γab\gamma^{E}_{ab}=\left[f^{\prime}(\varphi)\right]^{\frac{2}{D-2}}\gamma_{ab}, and the third follows from δθ=+f′′(R)f(R)vδR=f′′(φ)f(φ)kδφ\delta\theta\overset{\mathcal{H}^{+}}{=}-\frac{f^{\prime\prime}(R)}{f^{\prime}(R)}\partial_{v}\delta R=-\frac{f^{\prime\prime}(\varphi)}{f^{\prime}(\varphi)}\mathcal{L}_{k}\delta\varphi. We also emphasize that k\mathcal{L}_{k} only acts on δγab\delta\gamma_{ab} and δφ\delta\varphi as they are non-stationary. Thus

δσabEδσEab=γEacγEbdδσabEδσcdE=γEacγEbd[f(φ)]4D2δσabδσcd=γacγbdδσabδσcd=δσabδσab.\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}=\gamma_{E}^{ac}\gamma_{E}^{bd}\delta\sigma^{E}_{ab}\delta\sigma^{E}_{cd}=\gamma_{E}^{ac}\gamma_{E}^{bd}\left[f^{\prime}(\varphi)\right]^{\frac{4}{D-2}}\delta\sigma_{ab}\delta\sigma_{cd}=\gamma^{ac}\gamma^{bd}\delta\sigma_{ab}\delta\sigma_{cd}=\delta\sigma_{ab}\delta\sigma^{ab}. (61)

Furthermore,

δϕ=116πGD2(D1)D2δlnf(φ)=116πGD2(D1)D2f′′(R)f(R)δR,\delta\phi=\frac{1}{\sqrt{16\pi G_{D}}}\sqrt{\frac{2(D-1)}{D-2}}\delta\ln f^{\prime}(\varphi)=\frac{1}{\sqrt{16\pi G_{D}}}\sqrt{\frac{2(D-1)}{D-2}}\frac{f^{\prime\prime}(R)}{f^{\prime}(R)}\delta R, (62)

so (kEaaϕ)2(k_{E}^{a}\partial_{a}\phi)^{2} in the original frame reads

(kEaaϕ)2=D18πGD(D2)(f′′(R)f(R))2(vδR)2=D18πGD(D2)(δθ)2.(k_{E}^{a}\partial_{a}\phi)^{2}=\frac{D-1}{8\pi G_{D}(D-2)}\left(\frac{f^{\prime\prime}(R)}{f^{\prime}(R)}\right)^{2}\left(\partial_{v}\delta R\right)^{2}=\frac{D-1}{8\pi G_{D}(D-2)}\left(\delta\theta\right)^{2}. (63)

Gathering all of the results obtained above, we rewrite (56) in the original frame as

κ2πΔδ2Sdyn=14πGDv1v2dv𝒞(v)dAκvf(R)[δσabδσab+D1D2(δθ)2].\frac{\kappa}{2\pi}\Delta\delta^{2}S_{\text{dyn}}=\frac{1}{4\pi G_{D}}\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \kappa vf^{\prime}(R)\left[\delta\sigma_{ab}\delta\sigma^{ab}+\frac{D-1}{D-2}\left(\delta\theta\right)^{2}\right]. (64)

This result aligns with the outcome obtained by calculating the modified canonical energy flux for f(R)f(R) gravity, which is shown in Appendix A. As f(R)>0f^{\prime}(R)>0, δσabδσab0\delta\sigma_{ab}\delta\sigma^{ab}\geq 0 and (δθ)20(\delta\theta)^{2}\geq 0, we may also verify the second law for vacuum perturbations at second order in the original frame.

4.5 Relation to the Wald entropy of the generalized apparent horizon

If the derivative of the Wall entropy with respect to the affine parameter dSWall/dv\mathrm{d}S_{\text{Wall}}/\mathrm{d}v is positive, which follows from the second law of black hole thermodynamicsJacobson:1995uq ; Wall:2015raa , it suggests that dynamical black hole entropy is associated to the entropy of a surface inside the black hole. Although the location of the apparent horizon associated with the prescribed cross-section 𝒞(v)\mathcal{C}(v) is ambiguous as it depends on the choice of the simultaneous surface, for perturbations of a stationary black hole with bifurcate Killing horizon, the notion of the area of an apparent horizon corresponding to cross-section 𝒞(v)\mathcal{C}(v) is well defined to first orderHollands:2024vbe . And it was shown in the appendix A of Hollands:2024vbe that the dynamical black hole entropy is equal to the area entropy of the apparent horizon to first order in GR. Visser and Yan also provided a more pedagogical proof of this claim using Gaussian null coordinates (GNC) systemVisser:2024pwz . Their proof can be applied to f(R)f(R) gravity in the Einstein frame since it’s only a geometric fact. And in the Einstein frame this relation reads

SdynE=14GD(1vEddvE)A[𝒞(vE)]=A[𝒯E(vE)]4GD,S^{E}_{\text{dyn}}=\frac{1}{4G_{D}}\left(1-v^{E}\frac{\mathrm{d}}{\mathrm{d}v^{E}}\right)A\left[\mathcal{C}(v^{E})\right]=\frac{A\left[\mathcal{T}^{E}(v^{E})\right]}{4G_{D}}, (65)

where 𝒯E(vE)\mathcal{T}^{E}(v^{E}) is a constantvE-v^{E} surface of the apparent horizon in the Einstein frame 𝒜E\mathcal{A}^{E}, which is determined by the condition that the outgoing null expansion vanishes

θλE=λElnγE=0,\theta_{\lambda^{E}}=\frac{\partial}{\partial{\lambda^{E}}}\ln\sqrt{\gamma^{E}}=0, (66)

where λE\lambda^{E} is the affine parameter of the (future directed) outgoing null normal k~Ea\tilde{k}_{E}^{a} to 𝒯E(vE)\mathcal{T}^{E}(v^{E}), A[𝒞(vE)]A\left[\mathcal{C}(v^{E})\right] is the area of the horizon cross-section in the Einstein frame, and A[𝒯E(vE)]A\left[{\mathcal{T}^{E}}(v^{E})\right] is the area of 𝒯E(vE)\mathcal{T}^{E}(v^{E}). We wish to recast this relation in the original frame. As conformal transformations preserve orthogonality as well as the null property, the condition that locates the apparent horizon 𝒯E(vE)\mathcal{T}^{E}(v^{E}) in the Einstein frame (66) is translated into

1c[f(R)]2D2λln[γf(R)]=0\frac{1}{c\left[f^{\prime}(R)\right]^{\frac{2}{D-2}}}\frac{\partial}{\partial\lambda}\ln\left[\sqrt{\gamma}f^{\prime}(R)\right]=0 (67)

in the original frame, where cc is a constant and λ\lambda is the affine parameter of the outgoing null normal in the original frame. The generalized expansion for f(R)f(R) gravity in the original frame is defined asMatsuda:2020yvl

Θλ=λln[γf(R)].\Theta_{\lambda}=\frac{\partial}{\partial\lambda}\ln\left[\sqrt{\gamma}f^{\prime}(R)\right]. (68)

Then the constantvE-v^{E} surface of the apparent horizon in the Einstein frame 𝒯E(vE)\mathcal{T}^{E}(v^{E}) is translated into the constantv-v surface of the generalized apparent horizon 𝒯(v)\mathcal{T}(v) in the original frame, which is defined as the D2D-2 dimensional section with vanishing outgoing generalized expansion. As we have shown above, SdynS_{\text{dyn}} is invariant to first order if we replace vEv^{E} with vv in its formula. Therefore, the relation (65) in the original frame is rewritten as

Sdyn=14GD(1vddv)𝒞(v)dD2xγf(R)=14GD𝒯(v)dD2xγf(R).S_{\text{dyn}}=\frac{1}{4G_{D}}\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)\int_{\mathcal{C}(v)}\mathrm{d}^{D-2}x\sqrt{\gamma}f^{\prime}(R)=\frac{1}{4G_{D}}\int_{\mathcal{T}(v)}\mathrm{d}^{D-2}x\sqrt{\gamma}f^{\prime}(R). (69)

Thus the dynamical black hole entropy is equal to the Wald entropy of the generalized apparent horizon in the original frame of f(R)f(R) gravity.

5 Dynamical black hole entropy in canonical scalar-tensor theory

In this section we apply the methodology of the previous section to the canonical scalar-tensor theory. Firstly we derive both the physical process first law and the comparison first law for the canonical scalar-tensor theory. Secondly we study the second-order behavior of the dynamical black hole entropy for vacuum perturbations in the Einstein frame, and then convert it to the expression in the original frame. Finally we determine the relationship between the dynamical black hole entropy of the cross-section and the Wald entropy of the generalized apparent horizon in the original frame.

5.1 The conformal transformation and the Einstein frame

The canonical scalar-tensor theory is described by the action

Ist=116πGDdDxg[F(φ)R12gabaφbφU(φ)].I_{\text{st}}=\frac{1}{16\pi G_{D}}\int\mathrm{d}^{D}x\sqrt{-g}\left[F(\varphi)R-\frac{1}{2}g^{ab}\partial_{a}\varphi\partial_{b}\varphi-U(\varphi)\right]. (70)

And we assume that F(φ)>0F(\varphi)>0 to avoid tensor ghostsMatsuda:2020yvl . We turn to the Einstein frame and redefine the scalar field asDicke:1961gz

gabE=[F(φ)]2D2gab,ϕ=116πGDdφ~F(φ~)1+2(D1)D2[F(φ~)F(φ~)]2.g^{E}_{ab}=\left[F(\varphi)\right]^{\frac{2}{D-2}}g_{ab},\quad\phi=\frac{1}{\sqrt{16\pi G_{D}}}\int\mathrm{d}\tilde{\varphi}\ \sqrt{F(\tilde{\varphi})^{-1}+\frac{2(D-1)}{D-2}\left[\frac{F^{\prime}(\tilde{\varphi})}{F(\tilde{\varphi})}\right]^{2}}. (71)

Then the action can be rewritten as

Ist=dDxgE[RE16πGD12gEabaϕbϕV(ϕ)],I_{\text{st}}=\int\mathrm{d}^{D}x\sqrt{-g^{E}}\left[\frac{R^{E}}{16\pi G_{D}}-\frac{1}{2}g_{E}^{ab}\partial_{a}\phi\partial_{b}\phi-V(\phi)\right], (72)

where

V(ϕ)=116πGD[F(φ)]DD2U(φ).V(\phi)=\frac{1}{16\pi G_{D}}\left[F(\varphi)\right]^{-\frac{D}{D-2}}U(\varphi). (73)

And for an asymptotically flat stationary black hole solution to the scalar-tensor theory, the spacetime given by (71) remains an asymptotic flat stationary black hole with the same event horizon. Without loss of generality we assume φ\varphi tends to be a constant at spatial infinity. So the surface gravities of the two black hole spacetimes are related as κE=ακ\kappa^{E}=\alpha\kappa with α\alpha representing the value of [F(φ)]1D2\left[F(\varphi)\right]^{-\frac{1}{D-2}} at infinity.

5.2 The physical process first law

The derivation of the physical process first law for scalar-tensor theory is similar to the previous situation for f(R)f(R) gravity. First, for the perturbations left kEak_{E}^{a} invariant, we write down the non-stationary physical process first law in the Einstein frame as

κE2πΔδSdynE=v1Ev2EdvE𝒞(vE)dAEδTabEξEakEb,\frac{\kappa^{E}}{2\pi}\Delta\delta S^{E}_{\text{dyn}}=\int_{v^{E}_{1}}^{v^{E}_{2}}\mathrm{d}v^{E}\int_{\mathcal{C}(v^{E})}\mathrm{d}A^{E}\ \delta T^{E}_{ab}\xi_{E}^{a}k_{E}^{b}, (74)

where

SdynE[𝒞]=14GD(1vEddvE)𝒞(vE)dD2xγE.S^{E}_{\text{dyn}}[\mathcal{C}]=\frac{1}{4G_{D}}\left(1-v^{E}\frac{\mathrm{d}}{\mathrm{d}v^{E}}\right)\int_{\mathcal{C}(v^{E})}\mathrm{d}^{D-2}x\sqrt{\gamma^{E}}. (75)

Then we would like to recast this equation in the original frame. By the arguments similar to the last section, switching from vEv^{E}-identification to vv-identification leads to second-order corrections. And for perturbations left kak^{a} invariant, we recast (74) in the original frame as

κ2πΔδSdyn=v1v2dv𝒞(v)dAδTabξakb,\frac{\kappa}{2\pi}\Delta\delta S_{\text{dyn}}=\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \delta T_{ab}\xi^{a}k^{b}, (76)

where

Sdyn[𝒞]=14GD(1vddv)𝒞(v)dD2xγF(φ).S_{\text{dyn}}[\mathcal{C}]=\frac{1}{4G_{D}}\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)\int_{\mathcal{C}(v)}\mathrm{d}^{D-2}x\sqrt{\gamma}F(\varphi). (77)

5.3 The comparison first law

Next, the derivation of the comparison first law for scalar-tensor theory is straightforward. For source-free perturbations δTabE=0\delta T^{E}_{ab}=0 we write the comparison first law (29) in the Einstein frame as

κE2πδSdynE[𝒞(vE)]=δMEΩδJE.\frac{\kappa^{E}}{2\pi}\delta S^{E}_{\text{dyn}}[\mathcal{C}(v^{E})]=\delta M^{E}-\Omega_{\mathcal{H}}\delta J^{E}. (78)

Then as κE=ακ\kappa^{E}=\alpha\kappa, ME=αMM^{E}=\alpha M and JE=αJJ^{E}=\alpha J with α\alpha representing the inverse of the conformal factor at infinity, we obtain the comparison first law in the original frame

κ2πδSdyn[𝒞(v)]=δMΩδJ.\frac{\kappa}{2\pi}\delta S_{\text{dyn}}[\mathcal{C}(v)]=\delta M-\Omega_{\mathcal{H}}\delta J. (79)

5.4 The second law for vacuum perturbations

If external matter fields are absent, for vacuum perturbations δTabE=0\delta T^{E}_{ab}=0 if follows immediately that the dynamical black hole entropy is a constant to first order. So we have to pay attention to the second-order behavior to study the non-trivial change of the dynamical black hole entropy. The first-order variation of the Raychaudhuri equation implies that δθE\delta\theta^{E} is 0 along the horizon. We consider the second-order variation of the Raychaudhuri equation

ddvEδ2θE=2δσabEδσEab16πGD(kEaaδϕ)2,\frac{\mathrm{d}}{\mathrm{d}v^{E}}\delta^{2}\theta^{E}=-2\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}-16\pi G_{D}\left(k_{E}^{a}\partial_{a}\delta\phi\right)^{2}, (80)

and then integrate it on the horizon between two arbitrary cross-sections to obtain

κE2πΔδ2SdynE=14πGDv1Ev2EdvE𝒞(vE)dAEκEvE[δσabEδσEab+8πGD(kEaaδϕ)2].\frac{\kappa^{E}}{2\pi}\Delta\delta^{2}S^{E}_{\text{dyn}}=\frac{1}{4\pi G_{D}}\int_{v^{E}_{1}}^{v^{E}_{2}}\mathrm{d}v^{E}\int_{\mathcal{C}(v^{E})}\mathrm{d}A^{E}\ \kappa^{E}v^{E}\left[\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}+8\pi G_{D}\left(k_{E}^{a}\partial_{a}\delta\phi\right)^{2}\right]. (81)

As δσabEδσEab0\delta\sigma^{E}_{ab}\delta\sigma_{E}^{ab}\geq 0 and (kEaaδϕ)20\left(k_{E}^{a}\partial_{a}\delta\phi\right)^{2}\geq 0, the second law holds at second order for vacuum perturbations in the Einstein frame. Next we are going to rewrite this equation in the original frame.

By the arguments similar to those in the previous section, (81) is invariant to second order as we recast it in the original frame and switch from vEv^{E}-identification to vv-identification on the horizon. Notice that δθE=+0\delta\theta^{E}\overset{\mathcal{H}^{+}}{=}0 in the Einstein frame. In the original frame we obtain

δvln[γF(φ)]=δθ+F(φ)F(φ)vδφ=+0.\delta\partial_{v}\ln\left[\sqrt{\gamma}F(\varphi)\right]=\delta\theta+\frac{F^{\prime}(\varphi)}{F(\varphi)}\partial_{v}\delta\varphi\overset{\mathcal{H}^{+}}{=}0. (82)

As a result,

δσabE=12kEδγabE=[F(φ)]2D2[12kδγab+1D2γabF(φ)F(φ)kδφ]=[F(φ)]2D2[12kδγab1D2δθγab]=[F(φ)]2D2δσab(ϵ2).\begin{split}\delta\sigma^{E}_{ab}&=\frac{1}{2}\mathcal{L}_{k^{E}}\delta\gamma^{E}_{ab}\\ &=\left[F(\varphi)\right]^{\frac{2}{D-2}}\left[\frac{1}{2}\mathcal{L}_{k}\delta\gamma_{ab}+\frac{1}{D-2}\gamma_{ab}\frac{F^{\prime}(\varphi)}{F(\varphi)}\mathcal{L}_{k}\delta\varphi\right]\\ &=\left[F(\varphi)\right]^{\frac{2}{D-2}}\left[\frac{1}{2}\mathcal{L}_{k}\delta\gamma_{ab}-\frac{1}{D-2}\delta\theta\gamma_{ab}\right]\\ &=\left[F(\varphi)\right]^{\frac{2}{D-2}}\delta\sigma_{ab}(\epsilon^{2}).\end{split} (83)

Furthermore,

kEaaδϕ=dϕdφvδφ=116πGDF(φ)1+2(D1)D2[F(φ)F(φ)]2vδφ.k_{E}^{a}\partial_{a}\delta\phi=\frac{\mathrm{d}\phi}{\mathrm{d}\varphi}\partial_{v}\delta\varphi=\frac{1}{\sqrt{16\pi G_{D}}}\sqrt{F(\varphi)^{-1}+\frac{2(D-1)}{D-2}\left[\frac{F^{\prime}(\varphi)}{F(\varphi)}\right]^{2}}\partial_{v}\delta\varphi. (84)

Thus (81) in the original frame reads

κ2πΔδ2Sdyn=14πGDv1v2dv𝒞(v)dAκvF(φ)[δσabδσab+D1D2(δθ)2+12F(φ)(kaaδφ)2].\frac{\kappa}{2\pi}\Delta\delta^{2}S_{\text{dyn}}=\frac{1}{4\pi G_{D}}\int_{v_{1}}^{v_{2}}\mathrm{d}v\int_{\mathcal{C}(v)}\mathrm{d}A\ \kappa vF(\varphi)\left[\delta\sigma_{ab}\delta\sigma^{ab}+\frac{D-1}{D-2}\left(\delta\theta\right)^{2}+\frac{1}{2F(\varphi)}\left(k^{a}\partial_{a}\delta\varphi\right)^{2}\right]. (85)

Since F(φ)>0F(\varphi)>0, δσabδσab\delta\sigma_{ab}\delta\sigma^{ab}, (δθ)2\left(\delta\theta\right)^{2} and (kaaδφ)2\left(k^{a}\partial_{a}\delta\varphi\right)^{2} are nonnegative, the second law holds at second order for vacuum perturbations in the original frame.

5.5 Relation to the Wald entropy of the generalized apparent horizon

Finally we would like to determine the relation between the dynamical black hole entropy of 𝒞(v)\mathcal{C}(v) and the entropy of the generalized apparent horizon inside the black hole. The starting point is the relation to the Bekenstein-Hawking entropy of the apparent horizon in the Einstein frame

SdynE=14GD(1vEddvE)A[𝒞(vE)]=A[𝒯E(vE)]4GD.S^{E}_{\text{dyn}}=\frac{1}{4G_{D}}\left(1-v^{E}\frac{\mathrm{d}}{\mathrm{d}v^{E}}\right)A\left[\mathcal{C}(v^{E})\right]=\frac{A\left[\mathcal{T}^{E}(v^{E})\right]}{4G_{D}}. (86)

We would like to recast this relation in the original frame. Define the generalized expansion for canonical scalar-tensor theory asMatsuda:2020yvl

Θλ=λln[γF(φ)],\Theta_{\lambda}=\frac{\partial}{\partial\lambda}\ln\left[\sqrt{\gamma}F(\varphi)\right], (87)

where λ\lambda is the affine parameter of the null geodesics in the original frame. We define the generalized apparent horizon for the black hole spacetime of the canonical scalar-tensor theory as the section 𝒯\mathcal{T} with vanishing outgoing generalized expansion. Relation (86) is translated into

Sdyn=14GD(1vddv)𝒞(v)dD2xγF(φ)=14GD𝒯(v)dD2xγF(φ).S_{\text{dyn}}=\frac{1}{4G_{D}}\left(1-v\frac{\mathrm{d}}{\mathrm{d}v}\right)\int_{\mathcal{C}(v)}\mathrm{d}^{D-2}x\sqrt{\gamma}F(\varphi)=\frac{1}{4G_{D}}\int_{\mathcal{T}(v)}\mathrm{d}^{D-2}x\sqrt{\gamma}F(\varphi). (88)

Thus in the original frame the dynamical black hole entropy is equal to the Wald entropy of the generalized apparent horizon for canonical scalar-tensor theory.

6 Conclusion and discussion

In this paper we first generalize the pedagogical proof of the non-stationary physical process first law to non-vacuum black holes, and give a pedagogical deduction of the second-order behavior for SdynS_{\text{dyn}} under the vacuum perturbations in GR. We then derive both the non-stationary physical process first law and the non-stationary comparison first law for f(R)f(R) gravity as well as canonical scalar-tensor theory by means of conformal transformations. Our formulae for dynamical black hole entropy agree with those derived by the Noether charge method. We further study the second-order behavior of SdynS_{\text{dyn}} for vacuum perturbations in those theories, and find that second law is obeyed both in the Einstein frames and in the original frames. Moreover, we determine the relationship between the dynamical black hole entropy and the Wald entropy of the generalized apparent horizon in the original frame.

However, our methodology can be applied only to theories that can be put into the Einstein frames via conformal transformations. While there are also many theories of gravity cannot be put into the Einstein frame. One of the future works is to present a more pedagogical proof of the physical process first law and the comparison first law for theories such as Lovelock gravity. So far our arguments for dynamical black hole entropy only dwell on the classical level. It would be important to investigate at the semi-classical level whether the entropy of the Hawking radiation of a black hole will obtain a dynamical correction term after the non-stationary perturbation.

Acknowledgements.
This work is partly supported by the National Key Research and Development Program of China with Grant No. 2021YFC2203001 as well as the National Natural Science Foundation of China with Grant Nos. 12075026, 12035016, 12361141825 and 12375058.

Appendix A The modified canonical energy flux for f(R)f(R) gravity

In this appendix we calculate the modified canonical energy flux for f(R)f(R) gravity using the covariant phase space formalism. To simplify the calculations, we shall follow the gauge conditions of Hollands:2024vbe that take ξa\xi^{a} to be fixed under the variation. And the gauge conditions on δgab\delta g_{ab} at the event horizon reads:

ξaδgab=+0,a(ξbξcδgbc)=+0,\xi^{a}\delta g_{ab}\overset{\mathcal{H}^{+}}{=}0,\quad\nabla_{a}(\xi^{b}\xi^{c}\delta g_{bc})\overset{\mathcal{H}^{+}}{=}0, (89)

which are less relaxed than the gauge conditions in Sec.2.

A.1 The covariant phase space formalism and the fundamental identity

First let us briefly review the covariant phase space formalism. Consider an arbitrary diffeomorphism covariant theory of gravity in nn-dimensions derived from a Lagrangian nn-form 𝑳\boldsymbol{L}, then the variation of the Lagrangian can always be expressed as

δ𝑳=𝑬δϕ+dδ𝜽,\delta\boldsymbol{L}=\boldsymbol{E}\delta\phi+\mathrm{d}\delta\boldsymbol{\theta}, (90)

where ϕ\phi is the collection of dynamical fields such as metric gabg_{ab} and other matter fields, 𝑬\boldsymbol{E} is the equation of motion locally constructed out of ϕ\phi, and the symplectic potential (n1)(n-1)-form 𝜽(ϕ,δϕ)\boldsymbol{\theta}(\phi,\delta\phi) is locally constructed out of ϕ\phi, δϕ\delta\phi and their derivatives and is linear in δϕ\delta\phi. The symplectic current (n1)(n-1)-form is obtained from 𝜽\boldsymbol{\theta} via555Here we assume that the field variations δ1ϕ\delta_{1}\phi and δ2ϕ\delta_{2}\phi arise from a two-parameter variation ϕ(λ1,λ2)\phi(\lambda_{1},\lambda_{2}) and thus commute.

𝝎(ϕ;δ1ϕ,δ2ϕ)=δ1𝜽(ϕ,δ2ϕ)δ2𝜽(ϕ,δ1ϕ).\boldsymbol{\omega}(\phi;\delta_{1}\phi,\delta_{2}\phi)=\delta_{1}\boldsymbol{\theta}(\phi,\delta_{2}\phi)-\delta_{2}\boldsymbol{\theta}(\phi,\delta_{1}\phi). (91)

Let χa\chi^{a} be an arbitrary vector field which is also the infinitesimal generator of a diffeomorphism, then the associated Noether current (n1)(n-1)-form 𝑱\boldsymbol{J} is defined by

𝑱(ϕ)=𝜽(ϕ,χϕ)χ𝑳(ϕ),\boldsymbol{J}(\phi)=\boldsymbol{\theta}(\phi,\mathcal{L}_{\chi}\phi)-\chi\cdot\boldsymbol{L}(\phi), (92)

where the notation \cdot denotes the contraction of a vector field with the first index of a differential form. It was shown that the Noether current can also be written in the formIyer:1995kg ; Seifert:2006kv

𝑱=d𝑸[χ]+χa𝑪a.\boldsymbol{J}=\mathrm{d}\boldsymbol{Q}[\chi]+\chi^{a}\boldsymbol{C}_{a}. (93)

Here, the (n2)(n-2)-form 𝑸\boldsymbol{Q} is referred to as the “Noether charge”Iyer:1994ys and the dual vector valued (n1)(n-1)-form 𝑪a\boldsymbol{C}_{a} vanishes when the equations of motion are satisfied. Taking the first variation of (92) (taking the vector field χa\chi^{a} to be fixed) and using (90) and (91), we obtain

δ𝑱(ϕ)=χ[𝑬(ϕ)δϕ]+𝝎(ϕ;δϕ,χϕ)+d[χ𝜽(ϕ,δϕ)].\delta\boldsymbol{J}(\phi)=-\chi\cdot\left[\boldsymbol{E}(\phi)\delta\phi\right]+\boldsymbol{\omega}(\phi;\delta\phi,\mathcal{L}_{\chi}\phi)+\mathrm{d}\left[\chi\cdot\boldsymbol{\theta}(\phi,\delta\phi)\right]. (94)

Considering the variation of (93), we obtain the fundamental identity according toHollands:2012sf

𝝎(ϕ;δϕ,χϕ)=χ[𝑬(ϕ)δϕ]+χaδ𝑪a(ϕ)+d[δ𝑸[χ]χ𝜽(ϕ,δϕ)].\boldsymbol{\omega}(\phi;\delta\phi,\mathcal{L}_{\chi}\phi)=\chi\cdot\left[\boldsymbol{E}(\phi)\delta\phi\right]+\chi^{a}\delta\boldsymbol{C}_{a}(\phi)+\mathrm{d}\left[\delta\boldsymbol{Q}[\chi]-\chi\cdot\boldsymbol{\theta}(\phi,\delta\phi)\right]. (95)

For the case where χa\chi^{a} is a Killing field of the background ϕ\phi such that χϕ=0\mathcal{L}_{\chi}\phi=0, we vary the fundamental identity (95) to yield666Note that here the symbol χδ\mathcal{L}_{\chi}\delta is seen as “one” variation, which means that 𝝎(ϕ;δϕ,χδϕ)=δ𝜽(ϕ,χδϕ)(χδ)𝜽(ϕ,δ1ϕ).\boldsymbol{\omega}(\phi;\delta\phi,\mathcal{L}_{\chi}\delta\phi)=\delta\boldsymbol{\theta}(\phi,\mathcal{L}_{\chi}\delta\phi)-(\mathcal{L}_{\chi}\delta)\boldsymbol{\theta}(\phi,\delta_{1}\phi). (96) For instance, writing 𝜽(ϕ,δϕ)=𝑫δϕ\boldsymbol{\theta}(\phi,\delta\phi)=\boldsymbol{D}\delta\phi formally, where 𝑫\boldsymbol{D} is a linear operator valued (n1)(n-1)-form acting on δϕ\delta\phi constructed out of ϕ\phi, its derivatives, and the covariant derivative with respect to the stationary metric gabg_{ab}. If we see χδ\mathcal{L}_{\chi}\delta as “one” variation, we will get (χδ)𝜽(ϕ,δϕ)=(χδ𝑫)δϕ+𝑫(χδ2ϕ),(\mathcal{L}_{\chi}\delta)\boldsymbol{\theta}(\phi,\delta\phi)=(\mathcal{L}_{\chi}\delta\boldsymbol{D})\delta\phi+\boldsymbol{D}(\mathcal{L}_{\chi}\delta^{2}\phi), (97) and if we see χδ\mathcal{L}_{\chi}\delta as two subsequent variation, we will get χ(δ𝜽(ϕ,δϕ))=(χδ𝑫)δϕ+δ𝑫(χδϕ)+𝑫(χδ2ϕ),\mathcal{L}_{\chi}(\delta\boldsymbol{\theta}(\phi,\delta\phi))=(\mathcal{L}_{\chi}\delta\boldsymbol{D})\delta\phi+\delta\boldsymbol{D}(\mathcal{L}_{\chi}\delta\phi)+\boldsymbol{D}(\mathcal{L}_{\chi}\delta^{2}\phi), (98) where δ𝑫\delta\boldsymbol{D} constructed out of ϕ\phi, δϕ\delta\phi, their derivatives, and the variation of the Christoffel symbols.

𝝎(ϕ;δϕ,χδϕ)=χ[δ𝑬(ϕ)δϕ]+χ[𝑬(ϕ)δ2ϕ]+χaδ2𝑪a(ϕ)+d[δ2𝑸[χ]χδ𝜽(ϕ,δϕ)].\boldsymbol{\omega}(\phi;\delta\phi,\mathcal{L}_{\chi}\delta\phi)=\chi\cdot\left[\delta\boldsymbol{E}(\phi)\delta\phi\right]+\chi\cdot\left[\boldsymbol{E}(\phi)\delta^{2}\phi\right]+\chi^{a}\delta^{2}\boldsymbol{C}_{a}(\phi)+\mathrm{d}\left[\delta^{2}\boldsymbol{Q}[\chi]-\chi\cdot\delta\boldsymbol{\theta}(\phi,\delta\phi)\right]. (99)

A.2 The second-order behavior of SdynS_{\text{dyn}} for vacuum perturbations

Now let’s consider the pure gravity theory in which matter fields are absent in the Lagrangian. For vacuum perturbations, we have no external matter sources, δTab=0\delta T_{ab}=0, and (50) states that there is no change of dynamical black hole entropy with respect to affine time at first order, ΔδSdyn=0\Delta\delta S_{\text{dyn}}=0. Thus we must go to second order in perturbation theory to obtain the leading-order dynamical behavior of the black hold entropy. By (99) and setting χa=ξa\chi^{a}=\xi^{a}, in the case that the vacuum equations of motion hold, we obtainHollands:2024vbe

𝝎(g;δg,ξδg)+d[ξδ𝜽(g,δg)ξδ2𝑩(g)]=d[δ2𝑸[ξ]ξδ2𝑩(g)]=κ2πdδ2𝑺dyn(g),\boldsymbol{\omega}(g;\delta g,\mathcal{L}_{\xi}\delta g)+\mathrm{d}\left[\xi\cdot\delta\boldsymbol{\theta}(g,\delta g)-\xi\cdot\delta^{2}\boldsymbol{B}_{\mathcal{H}}(g)\right]=\mathrm{d}\left[\delta^{2}\boldsymbol{Q}[\xi]-\xi\cdot\delta^{2}\boldsymbol{B}_{\mathcal{H}}(g)\right]=\frac{\kappa}{2\pi}\mathrm{d}\delta^{2}\boldsymbol{S}_{\text{dyn}}(g), (100)

where 𝑩\boldsymbol{B}_{\mathcal{H}} satisfying 𝜽=+δ𝑩\boldsymbol{\theta}\overset{\mathcal{H}^{+}}{=}\delta\boldsymbol{B}_{\mathcal{H}} is defined on \mathcal{H} according to the theorem 1 of Hollands:2024vbe , and it has the following form

𝑩=ϵ(n1)i=0mT~(i)b1bicd(b1bi)ξgcd,\boldsymbol{B}_{\mathcal{H}}=\boldsymbol{\epsilon}^{(n-1)}\sum_{i=0}^{m}\tilde{T}_{(i)}^{b_{1}\cdots b_{i}cd}\nabla_{(b_{1}}\cdots\nabla_{b_{i})}\mathcal{L}_{\xi}g_{cd}, (101)

where the tensors T~(i)b1bicd=T~(i)(b1bi)(cd)\tilde{T}_{(i)}^{b_{1}\cdots b_{i}cd}=\tilde{T}_{(i)}^{(b_{1}\cdots b_{i})(cd)} are smooth on \mathcal{H} and are locally and covariantly constructed from the metric, curvature, covariant derivatives of the curvature as well as ξa\xi^{a} and NaN^{a}, with ξa\xi^{a} and NaN^{a} appearing only algebraically777The vector field NaN^{a} is introduced byHollands:2024vbe aξb=+2κN[aξb],NaNa=+0,Naξa=+1.\nabla_{a}\xi_{b}\overset{\mathcal{H}^{+}}{=}2\kappa N_{[a}\xi_{b]},\quad N^{a}N_{a}\overset{\mathcal{H}^{+}}{=}0,\quad N^{a}\xi_{a}\overset{\mathcal{H}^{+}}{=}1. (102) . And the entropy (n2)(n-2)-form 𝑺dyn\boldsymbol{S}_{\text{dyn}} is defined on \mathcal{H} by

𝑺dyn2πκ(𝑸[ξ]ξ𝑩).\boldsymbol{S}_{\text{dyn}}\equiv\frac{2\pi}{\kappa}(\boldsymbol{Q}[\xi]-\xi\cdot\boldsymbol{B}_{\mathcal{H}}). (103)

Integrating (100) between two cross-sections on the horizon, we find that

κ2πΔδ2Sdyn=12𝒆G(g;δg,δg),\frac{\kappa}{2\pi}\Delta\delta^{2}S_{\text{dyn}}=\int_{\mathcal{H}_{12}}\boldsymbol{e}_{G}(g;\delta g,\delta g), (104)

where the modified canonical energy flux (n1)(n-1)-form 𝒆G\boldsymbol{e}_{G} is defined by

𝒆G(g;δg,δg)𝝎(g;δg,ξδg)+d[ξδ𝜽(g,δg)ξδ2𝑩(g)].\boldsymbol{e}_{G}(g;\delta g,\delta g)\equiv\boldsymbol{\omega}(g;\delta g,\mathcal{L}_{\xi}\delta g)+\mathrm{d}\left[\xi\cdot\delta\boldsymbol{\theta}(g,\delta g)-\xi\cdot\delta^{2}\boldsymbol{B}_{\mathcal{H}}(g)\right]. (105)

From (104), one can immediately deduce that in the case of vacuum perturbations, the second law of black hole thermodynamics holds at second order if and only if the modified canonical energy flux 𝒆G\boldsymbol{e}_{G} is non-negative everywhere on the horizon.

Next we are going to show that 𝒆G\boldsymbol{e}_{G} is quadratic in δgab\delta g_{ab} and does not depend on δ2gab\delta^{2}g_{ab}. Again, we formally write 𝜽(g,δg)=𝑫δg\boldsymbol{\theta}(g,\delta g)=\boldsymbol{D}\delta g and 𝑩(g)=𝑪ξg\boldsymbol{B}_{\mathcal{H}}(g)=\boldsymbol{C}\mathcal{L}_{\xi}g by (101), then 𝜽=+δ𝑩\boldsymbol{\theta}\overset{\mathcal{H}^{+}}{=}\delta\boldsymbol{B}_{\mathcal{H}} implies that 𝑫=+𝑪ξ\boldsymbol{D}\overset{\mathcal{H}^{+}}{=}\boldsymbol{C}\mathcal{L}_{\xi}. Thus

𝝎(g;δg,ξδg)=δ𝜽(g;ξδg)ξδ𝜽(g;δg)=δ𝑫(ξδg)(ξδ𝑫)δg,δ𝜽(g;δg)=δ𝑫δg+𝑫δ2g=+δ𝑫δg+𝑪ξδ2g,δ2𝑩=δ(δ𝑪ξg+𝑪ξδg)=2δ𝑪ξδg+𝑪ξδ2g.\begin{split}\boldsymbol{\omega}(g;\delta g,\mathcal{L}_{\xi}\delta g)&=\delta\boldsymbol{\theta}(g;\mathcal{L}_{\xi}\delta g)-\mathcal{L}_{\xi}\delta\boldsymbol{\theta}(g;\delta g)=\delta\boldsymbol{D}(\mathcal{L}_{\xi}\delta g)-(\mathcal{L}_{\xi}\delta\boldsymbol{D})\delta g,\\ \delta\boldsymbol{\theta}(g;\delta g)&=\delta\boldsymbol{D}\delta g+\boldsymbol{D}\delta^{2}g\overset{\mathcal{H}^{+}}{=}\delta\boldsymbol{D}\delta g+\boldsymbol{C}\mathcal{L}_{\xi}\delta^{2}g,\\ \delta^{2}\boldsymbol{B}_{\mathcal{H}}&=\delta(\delta\boldsymbol{C}\mathcal{L}_{\xi}g+\boldsymbol{C}\mathcal{L}_{\xi}\delta g)=2\delta\boldsymbol{C}\mathcal{L}_{\xi}\delta g+\boldsymbol{C}\mathcal{L}_{\xi}\delta^{2}g.\end{split} (106)

Notice that for an (n1)(n-1)-form 𝒑\boldsymbol{p} the pullback of ξd𝒑\xi\cdot\mathrm{d}\boldsymbol{p} to the horizon vanishes. By Cartan’s magic formula

d(ξ𝒑)=+d(ξ𝒑)+ξd𝒑=ξ𝒑,\mathrm{d}(\xi\cdot\boldsymbol{p})\overset{\mathcal{H}^{+}}{=}\mathrm{d}(\xi\cdot\boldsymbol{p})+\xi\cdot\mathrm{d}\boldsymbol{p}=\mathcal{L}_{\xi}\boldsymbol{p}, (107)

we have

𝒆G(g;δg,δg)𝝎(g;δg,ξδg)+d[ξδ𝜽(g,δg)ξδ2𝑩(g)]=+δ𝑫(ξδg)(ξδ𝑫)δg+ξ(δ𝑫δg2δ𝑪ξδg)=2δ𝑫(ξδg)ξ(2δ𝑪ξδg).\begin{split}\boldsymbol{e}_{G}(g;\delta g,\delta g)&\equiv\boldsymbol{\omega}(g;\delta g,\mathcal{L}_{\xi}\delta g)+\mathrm{d}[\xi\cdot\delta\boldsymbol{\theta}(g,\delta g)-\xi\cdot\delta^{2}\boldsymbol{B}_{\mathcal{H}}(g)]\\ &\overset{\mathcal{H}^{+}}{=}\delta\boldsymbol{D}(\mathcal{L}_{\xi}\delta g)-(\mathcal{L}_{\xi}\delta\boldsymbol{D})\delta g+\mathcal{L}_{\xi}(\delta\boldsymbol{D}\delta g-2\delta\boldsymbol{C}\mathcal{L}_{\xi}\delta g)\\ &=2\delta\boldsymbol{D}(\mathcal{L}_{\xi}\delta g)-\mathcal{L}_{\xi}(2\delta\boldsymbol{C}\mathcal{L}_{\xi}\delta g).\end{split} (108)

Thus we have shown that 𝒆G\boldsymbol{e}_{G} actually does not depend on δ2gab\delta^{2}g_{ab}, and to calculate 𝒆G\boldsymbol{e}_{G} in practice, we need only to calculate δ𝜽(g;ξδg)\delta\boldsymbol{\theta}(g;\mathcal{L}_{\xi}\delta g) and δ2𝑩\delta^{2}\boldsymbol{B}_{\mathcal{H}} and take their parts which are quadratic in δgab\delta g_{ab} by comparing (106) and (108).

Consider the f(R)f(R) gravity, whose Lagrangian is given by

𝑳a1an=116πGDf(R)ϵa1an.\boldsymbol{L}_{a_{1}\cdots a_{n}}=\frac{1}{16\pi G_{D}}f(R)\boldsymbol{\epsilon}_{a_{1}\cdots a_{n}}. (109)

The equation of motion is

Eab=116πGD(12gabffRRab+abfRgabfR)=0,E_{ab}=\frac{1}{16\pi G_{D}}\left(\frac{1}{2}g_{ab}f-\frac{\partial f}{\partial R}R_{ab}+\nabla_{a}\nabla_{b}\frac{\partial f}{\partial R}-g_{ab}\square\frac{\partial f}{\partial R}\right)=0, (110)

where =gabab\square=g^{ab}\nabla_{a}\nabla_{b}. The symplectic potential is

𝜽(g;δg)a1an1=116πGD(gmcgbdgmdgbc)(fRddfR)δgbcϵma1an1\boldsymbol{\theta}(g;\delta g)_{a_{1}\cdots a_{n-1}}=\frac{1}{16\pi G_{D}}(g^{mc}g^{bd}-g^{md}g^{bc})(\frac{\partial f}{\partial R}\nabla_{d}-\nabla_{d}\frac{\partial f}{\partial R})\delta g_{bc}\boldsymbol{\epsilon}_{ma_{1}\cdots a_{n-1}} (111)

and

𝑩a1an1=+116πGDξmNd(gmcgbdgmdgbc)fRξgbcϵ(n1).\boldsymbol{B}_{\mathcal{H}a_{1}\cdots a_{n-1}}\overset{\mathcal{H}^{+}}{=}-\frac{1}{16\pi G_{D}}\xi_{m}N_{d}(g^{mc}g^{bd}-g^{md}g^{bc})\frac{\partial f}{\partial R}\mathcal{L}_{\xi}g_{bc}\boldsymbol{\epsilon}^{(n-1)}. (112)

According to the aforementioned argument, since (omit the terms containing δ2gab\delta^{2}g_{ab})

δ𝜽(g;ξδg)=+116πGD[(12fgefδgef+f′′δR)gbcξξδgbcfgbegcfδgefξξδgbc12fgbegcfξδgbcξδgeff′′ξδRgbcξδgbc]ϵ(n1),\begin{split}\delta\boldsymbol{\theta}(g;\mathcal{L}_{\xi}\delta g)\overset{\mathcal{H}^{+}}{=}\frac{1}{16\pi G_{D}}&\left[\left(\frac{1}{2}f^{\prime}g^{ef}\delta g_{ef}+f^{\prime\prime}\delta R\right)g^{bc}\mathcal{L}_{\xi}\mathcal{L}_{\xi}\delta g_{bc}-f^{\prime}g^{be}g^{cf}\delta g_{ef}\mathcal{L}_{\xi}\mathcal{L}_{\xi}\delta g_{bc}\right.\\ &\left.-\frac{1}{2}f^{\prime}g^{be}g^{cf}\mathcal{L}_{\xi}\delta g_{bc}\mathcal{L}_{\xi}\delta g_{ef}-f^{\prime\prime}\mathcal{L}_{\xi}\delta Rg^{bc}\mathcal{L}_{\xi}\delta g_{bc}\right]\boldsymbol{\epsilon}^{(n-1)},\end{split} (113)

and (also omit the terms containing δ2gab\delta^{2}g_{ab})

δ2𝑩=+116πGD(fgefδgefgbcξδgbc2fgbegcfδgefξδgbc+2f′′δRgbcξδgbc)ϵ(n1),\delta^{2}\boldsymbol{B}_{\mathcal{H}}\overset{\mathcal{H}^{+}}{=}\frac{1}{16\pi G_{D}}\left(f^{\prime}g^{ef}\delta g_{ef}g^{bc}\mathcal{L}_{\xi}\delta g_{bc}-2f^{\prime}g^{be}g^{cf}\delta g_{ef}\mathcal{L}_{\xi}\delta g_{bc}+2f^{\prime\prime}\delta Rg^{bc}\mathcal{L}_{\xi}\delta g_{bc}\right)\boldsymbol{\epsilon}^{(n-1)}, (114)

therefore the modified canonical energy flux is given by

𝒆G=+14πGD(κv)2[f(R)(δσabδσabD3D2(δθ)2)2f′′(R)kδRδθ]ϵ(n1),\boldsymbol{e}_{G}\overset{\mathcal{H}^{+}}{=}\frac{1}{4\pi G_{D}}(\kappa v)^{2}\left[f^{\prime}(R)\left(\delta\sigma_{ab}\delta\sigma^{ab}-\frac{D-3}{D-2}(\delta\theta)^{2}\right)-2f^{\prime\prime}(R)\mathcal{L}_{k}\delta R\delta\theta\right]\boldsymbol{\epsilon}^{(n-1)}, (115)

where vv is the affine parameter of the null generator kak^{a} of the future horizon, σab=12kγab1D2θγab\sigma_{ab}=\frac{1}{2}\mathcal{L}_{k}\gamma_{ab}-\frac{1}{D-2}\theta\gamma_{ab} is the shear and θ=vlnγ\theta=\partial_{v}\ln\sqrt{\gamma} is the expansion of the generators of the horizon with respect to vv as mentioned before.

For the vacuum perturbation, the linearized equation of motion is satisfied δEab=0\delta E_{ab}=0, so that on the entire horizon, we have

0=δEabξaξb=+(κv)216πGDddv(fδθ+f′′kδR).0=\delta E_{ab}\xi^{a}\xi^{b}\overset{\mathcal{H}^{+}}{=}\frac{\left(\kappa v\right)^{2}}{16\pi G_{D}}\frac{\mathrm{d}}{\mathrm{d}v}\left(f^{\prime}\delta\theta+f^{\prime\prime}\mathcal{L}_{k}\delta R\right). (116)

Suppose that at the late time limit, the spacetime returns to stationary, i.e. limv(fδθ+f′′kδR)=0\lim_{v\rightarrow\infty}(f^{\prime}\delta\theta+f^{\prime\prime}\mathcal{L}_{k}\delta R)=0, then with the above linearized equation of motion, we get

fδθ+f′′kδR=+0.f^{\prime}\delta\theta+f^{\prime\prime}\mathcal{L}_{k}\delta R\overset{\mathcal{H}^{+}}{=}0. (117)

Finally, we get the modified canonical energy flux for f(R)f(R) gravity

𝒆G=+14πGD(κv)2f(R)[δσabδσab+D1D2(δθ)2]ϵ(n1),\boldsymbol{e}_{G}\overset{\mathcal{H}^{+}}{=}\frac{1}{4\pi G_{D}}\left(\kappa v\right)^{2}f^{\prime}(R)\left[\delta\sigma_{ab}\delta\sigma^{ab}+\frac{D-1}{D-2}(\delta\theta)^{2}\right]\boldsymbol{\epsilon}^{(n-1)}, (118)

and so that

κ2πΔδ2Sdyn=14πGDτ1τ2dτC(τ)𝑑A(κv)2f(R)[δσabδσab+D1D2(δθ)2]=14πGDv1v2𝑑vC(v)dAκvf(R)[δσabδσab+D1D2(δθ)2].\begin{split}\frac{\kappa}{2\pi}\Delta\delta^{2}S_{\text{dyn}}&=\frac{1}{4\pi G_{D}}\int_{\tau_{1}}^{\tau_{2}}\mathrm{d}\tau\int_{C(\tau)}dA\left(\kappa v\right)^{2}f^{\prime}(R)\left[\delta\sigma_{ab}\delta\sigma^{ab}+\frac{D-1}{D-2}(\delta\theta)^{2}\right]\\ &=\frac{1}{4\pi G_{D}}\int_{v_{1}}^{v_{2}}dv\int_{C(v)}\mathrm{d}A\ \kappa vf^{\prime}(R)\left[\delta\sigma_{ab}\delta\sigma^{ab}+\frac{D-1}{D-2}(\delta\theta)^{2}\right].\end{split} (119)

where τ\tau is the Killing parameter for the null Killing generator ξa\xi^{a}, and the Killing parameter τ\tau is related to the affine parameter vv by v=Cκeκτv=\frac{C}{\kappa}e^{\kappa\tau}, which implies that dv=κvdτ\mathrm{d}v=\kappa v\mathrm{d}\tau. (119) gives the same result as (64), and this provides a non-trivial check for our conclusion obtained via the Einstein frame.

References