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aainstitutetext: Department of Mathematics and Haifa Research Center for Theoretical Physics and Astrophysics, University of Haifa, Haifa 31905, Israelbbinstitutetext: Department of Physics, Technion, Haifa 32000, Israelccinstitutetext: Department of Physics, Utah State University, 4415 Old Main Hill Road, UT 84322, USAddinstitutetext: Instituto de Física Teórica UAM/CSIC, Universidad Autónoma de Madrid, Cantoblanco, 28049 Madrid, Spaineeinstitutetext: Joseph Henry Laboratories, Princeton University, Princeton, NJ 08544, USA

Electro-Magnetic Energy Extraction from Rotating Black Holes in AdS

Nele Callebaut c,d    Maria J. Rodriguez e    and Herman Verlinde nele_calleba@technion.ac.il majo.rodriguez.b@gmail.com verlinde@princeton.edu
Abstract

Force-Free Electrodynamics for black holes in Anti de Sitter is considered. We present new, energy extracting solutions of Force-Free Electrodynamics in Anti de Sitter - Near Horizon Extremal Kerr and Super-Entropic Near Horizon Extremal Kerr geometries. The relevant equations of motion are derived from an action for force-free plasma surrounding spinning black holes with generic asymptotics. We consider the energy flux of electrodynamic fields in rotating frames to argue that the correct measure for energy extraction is the energy flux measured by a rotating observer in the near horizon region. We illustrate this procedure by application to near horizon solutions in Kerr, AdS-Kerr and BTZ.

1 Introduction

It is widely believed that astrophysical black holes are typically surrounded by magnetospheres composed of an electromagnetic plasma that is force-free to a good approximation. In Blandford:1977ds , Blandford and Znajek used a model of force-free electrodynamics (FFE) for the plasma surrounding a spinning black hole to suggest a mechanism for energy extraction from the black hole. They argued that rotational energy escapes via plasma currents along magnetic field lines that thread the horizon. The Blandford Znajek (BZ) process is considered to provide the basic picture behind astrophysical observations of jets, e.g. in active galactic nuclei and quasars. For more recent discussions on the consistency of the BZ mechanism, see Grignani:2018ntq ; Grignani:2019dqc ; Armas:2020mio .

The FFE solution discussed in the original paper Blandford:1977ds is an approximate analytical solution for a slowly rotating Kerr black hole. Despite a lot of work on numerical as well as analytical solutions (1973MichelCurtis ; 1976Blandford ; Menon:2005mg ; Tanabe:2008wm ; Brennan:2013kea ; Gralla:2015vta , see also Gralla:2014yja and references therein), it remains a challenge to find a physically realistic, exact and energy extracting solution of the FFE equations in a Kerr black hole background.

One successful strategy for generating families of solutions has been to exploit the enhanced amount of symmetry in the near-horizon region of an extremal, i.e. maximally spinning, Kerr black hole Lupsasca:2014pfa ; Lupsasca:2014hua ; Zhang:2014pla . In this paper we will continue this effort by proposing a previously overlooked symmetric ansatz for the electromagnetic field strength of the plasma. We discuss in detail the corresponding energy outflux. By making use of a toy model of a rotating electromagnetic configuration, we argue the correct measure for energy extraction is the outflux measured by a rotating observer in the near-horizon geometry, corresponding to an observer at rest in Kerr. The new symmetric ansatz has the main advantage (over previous energy-extracting, symmetric FFE solutions Zhang:2014pla ) that it gives rise to an energy outflux at the boundary of the near-horizon region, as measured by a Kerr observer, that is finite.

The FFE solutions that can be produced with the new ansatz in the Near Horizon Extremal Kerr geometry – known as NHEK – do not obey the assumed physical boundary conditions presented in this paper. However, when we generalize the background to the Near Horizon Extremal AdS-Kerr geometry – introduced later as AdS-NHEK or SE-NHEK for super-entropic Near Horizon Extremal AdS-Kerr – we do find such a solution. For the background in question the topology is in fact that of a cylinder and this metric therefore provides a close resemblance to our toy model of a rotating conducting cylinder.

The generalization to AdS-Kerr was motivated by the discovery in Jacobson:2017xam of an exotic application of the BZ process that does not involve the presence of plasma, realized in a BTZ background. While not immediately relevant astrophysically, the study of FFE in AdS backgrounds may prove useful for obtaining a better understanding of remaining conceptual questions regarding the BZ process, such as where and how the negative energy originates. Indeed we hope the presented toy model and FFE solutions in near-horizon AdS-Kerr may contribute to this goal in the future.

The toy model and new symmetric log ansatz in NHEK were first presented in the unpublished ThesisLibby . In this paper we additionally apply these ideas in the context of AdS-Kerr black holes.

The paper is organized as follows. We begin in section 2 with a review where we explain how a 2-dimensional (2D) action naturally describes toroidal force-free plasma systems surrounding a spinning black hole. At this stage we already assume a system that is toroidally invariant and therefore effectively 2-dimensional. We present in section 3 all the near-horizon geometries of spinning black holes that we will be using in the paper. Next, in section 4, we apply the technique of imposing the extra scaling symmetry of the near-horizon regions on the field strength of the plasma. This gives rise to the scaling ansatz in 4.1.1 and the new log ansatz in 4.1.2. These ansatze fix the analytic behavior of the field strength as a function of the radius rr of the background. The scaling ansatz is known in the literature for NHEK. We employ the same scaling ansatz in AdS-NHEK and SE-NHEK to find a new scaling solution of FFE. The log ansatz, to our knowledge, is new in all three backgrounds.

Making use of the ansatze, the problem reduces to solving an ODE for a function Φ(θ)\Phi(\theta) describing the dependence of the field strength on the polar angle. This is the part that will be treated numerically. The numerical problem is to solve the EOM summarized in section 4.2 with physical boundary conditions provided in section 4.3.

Before presenting the numerical solutions, in section 5 we consider the energy flux of electrodynamic fields in rotating frames, making use of a ‘toy model’, to explain how the fluxes at the boundary of the near-horizon throats connect with non-rotating observers outside the throat. We argue it is the latter observer’s flux that determines whether a near-horizon solution is energy extracting. The main results of this section are equation (5.15) for the energy flux in the toy model, equation (5.29) for the Kerr energy flux and (5.40) for the AdS-Kerr energy flux. The general relation (5.48) highlights the equivalence with the toy model. These formulas are applied to our energy-extracting semi-analytical solutions in section 6. The energy extraction is also discussed in section 5.5 for the full BTZ solution of Jacobson:2017xam . This provides a check on the proposed procedure for obtaining the flux outside the near-horizon throat.

Finally we present a scaling solution in NHEK, a scaling solution in AdS-NHEK and a log solution in SE-NHEK, with their corresponding Poynting fluxes, in Figures 2-4. Final remarks are discussed in section 7. Some mathematical details of our analysis have been relegated to Appendices A-D.

We adopt the metric signature (,+,+,+)(-,+,+,+), the units c=G=1c=G=1, and orientation of dtdϕdrdθdt\wedge d\phi\wedge dr\wedge d\theta for defining the Hodge dual \star.

2 Action for force-free plasma in black holes

In this section we review the set-up of the problem, hereby setting our notation. In particular, we will make use of an available action principle for the description of a force-free plasma in black holes. This has several advantages in general, such as allowing for the easy identification of conserved quantities through Noether’s theorem.

As first studied by Blandford and Znajek Blandford:1977ds , the equations for the force-free plasma around rotating black holes (described by a fixed background metric gμνg_{\mu\nu}) consists of Maxwell’s equations

μFνμ\displaystyle\nabla_{\mu}F^{\nu\mu} =\displaystyle= Jν,\displaystyle J^{\nu}\,, (2.1)
[μFσν]\displaystyle\nabla_{[\mu}F_{\sigma\nu]} =\displaystyle= 0,\displaystyle 0\,, (2.2)

and the force-free electromagnetic (FFE) condition

FμνJν=0,F_{\mu\nu}J^{\nu}=0\,, (2.3)

with source current JνJ_{\nu} and field strength FμνF_{\mu\nu}. Solutions to these equations involve finding a field strength FμνF_{\mu\nu} that generates a current JμJ^{\mu} through (2.1), and satisfies the FFE constraint (2.3). The Bianchi identity (2.2) follows straightforwardly by writing the field strength as Fμν=μAννAμF_{\mu\nu}=\partial_{\mu}A_{\nu}-\partial_{\nu}A_{\mu} in terms of the gauge field AμA_{\mu}.

The criterion for the FFE condition (2.3) to hold is that in local inertial frames the matter source contribution TμνmatterT^{matter}_{\mu\nu} becomes negligible. The stress tensor can therefore be defined as

Tμν=TμνEM+TμνmatterTμνEM,T_{\mu\nu}=T^{EM}_{\mu\nu}+T^{matter}_{\mu\nu}\approx T_{\mu\nu}^{EM}\,, (2.4)

where TμνEMT_{\mu\nu}^{EM} is the contribution from the electric and magnetic field.111The correspondence with the force-free condition (2.3)(\ref{eq:ffe}) follows directly from stress-energy conservation μTμν=0\nabla_{\mu}T^{\mu\nu}=0, combined with νTμνEM=FμνJν\nabla^{\nu}T^{EM}_{\mu\nu}=-F_{\mu\nu}J^{\nu} from Maxwell’s equations. In this FFE regime, the Einstein-Maxwell action for the interaction between the charged matter and the gauge field AμA_{\mu} must be nearly independent of gμνg_{\mu\nu}, hence

𝒮[g,A]𝒮[A]=g(14FμνFμν+AμJμ)𝑑t𝑑ϕ𝑑r𝑑θ.\mathcal{S}[g,A]\rightarrow\mathcal{S}[A]=\int\sqrt{-g}\left(-\frac{1}{4}F_{\mu\nu}F^{\mu\nu}+A_{\mu}J^{\mu}\right)dt\,d\phi\,dr\,d\theta\,. (2.5)

Maxwell’s inhomogeneous equations (2.1)(\ref{eom}) follow as the Euler-Lagrange equations of this action.

In general, the above system of equations (2.1)-(2.3) is highly nonlinear and can only be solved numerically. However, in toroidal spacetimes the symmetries can be exploited to simplify the analysis and obtain semi-analytical solutions Lupsasca:2014pfa ; Lupsasca:2014hua ; Zhang:2014pla . Here, by toroidal spacetimes we mean curved spacetimes that can be described by a coordinate system (t,ϕ,r,θ)(t,\phi,r,\theta) in which the metric is independent of time tt and angle ϕ\phi. The coordinates (t,ϕ)(t,\phi) are then referred to as toroidal coordinates xα,βx^{\alpha,\beta}, and (r,θ)(r,\theta) as poloidal coordinates xa,bx^{a,b}. The line-element of such a spacetime with a block-diagonal metric (gaα=0g_{a\alpha}=0), independent of time tt and angle ϕ\phi (tgμν=ϕgμν\partial_{t}g_{\mu\nu}=\partial_{\phi}g_{\mu\nu}=0) takes the form

ds2(gT)αβdxαdxβ+(gP)abdxadxb,ds^{2}\equiv(g_{T})_{\alpha\beta}\,dx^{\alpha}dx^{\beta}+(g_{P})_{ab}\,dx^{a}dx^{b}\,, (2.6)

with toroidal metric gTg_{T} and poloidal metric gPg_{P}.

Typically the dynamics around a black hole will capture the black hole’s symmetries. It is natural then to impose the same toroidal symmetry of the background metric on the solutions for the field strength. As we now argue, this will allow to reduce the 4D problem to a well-defined action in the two poloidal coordinates.

We assume a stationary and axisymmetric solution, characterized by a field strength with non-zero components

Fμa(xa)0.\displaystyle F_{\mu a}(x^{a})\neq 0\,. (2.7)

The analysis of the conditions on FμaF_{\mu a} imposed by the FFE equations is most clear in form notation, with the field strength defined as a two-form F=12FμνdxμdxνF=\frac{1}{2}F_{\mu\nu}dx^{\mu}\wedge dx^{\nu}. See e.g. Jacobson:2017xam for a quick review of differential forms in the context of force-free electrodynamics. In this notation, the equations (2.1)-(2.2) are written respectively as

dF\displaystyle d\star F =\displaystyle= J\displaystyle\star J\, (2.8)
dF\displaystyle dF =\displaystyle= 0\displaystyle 0\, (2.9)

for the 2-form field strength F=dAF=dA in terms of the 1-form gauge field AA, with \star the Hodge dual and \wedge the wedge product. Introducing the notation AT=AαdxαA_{T}=A_{\alpha}dx^{\alpha} for the toroidal contribution and AP=AadxaA_{P}=A_{a}dx^{a} for the poloidal contribution to the gauge field, we can write

A=Aμdxμ=AT+AP\displaystyle A=A_{\mu}dx^{\mu}=A_{T}+A_{P} (2.10)

and

F=dAtdt+dAϕdϕ+dAP.\displaystyle F=dA_{t}\wedge dt+dA_{\phi}\wedge d\phi+dA_{P}\,\,. (2.11)

Similarly, the 1-form current JJ is

J=JP+JT.\displaystyle J=J_{P}+J_{T}\,\,. (2.12)

In the expression for the field strength, dd is the differential operator in 4D, with dA=μAdxμdA=\partial_{\mu}A\,dx^{\mu}. Imposing toroidal invariance comes down to reinterpreting the differential operator dd as a 2D differential operator in the poloidal metric gPg_{P}. That is, dA=aAdxadA=\partial_{a}A\,dx^{a}. The toroidal invariance is therefore implicitly present in the expressions through the interpretation of dd.

The toroidal component of the FFE equation (2.3) can be written in form notation as

dATJP=0.\displaystyle dA_{T}\wedge*J_{P}=0\,\,. (2.13)

Here, we use * to refer to the star operator in the poloidal metric, to be distinguished from the star operator \star in the full 4D spacetime (as used in Maxwell’s equation). Its action is defined as JP=Jadxa=Jaϵbadxb*J_{P}=J_{a}*dx^{a}=J_{a}\epsilon^{a}_{\phantom{a}b}dx^{b}. Maxwell’s equation implies conservation of current dJ=0d\star J=0 (in 4D). For the toroidally invariant solution this further implies dJP=0d*J_{P}=0 (in 2D), which allows to introduce a 0-form current II by writing JP*J_{P} as a total derivative

JP=d(IgT).\displaystyle*J_{P}=d\left(\frac{I}{\sqrt{-g_{T}}}\right)\,\,. (2.14)

The interpretation of II is that it is proportional to the integrated polar current through a ‘spherical cap’ SS, stretching over a time interval Δt\Delta t, azimuthal angle interval Δϕ=2π\Delta\phi=2\pi and range θ<θ0\theta<\theta_{0} at constant radius rr, which by Stokes’ theorem is given by

SJ\displaystyle\int_{S}\star J =CgT(IgT)𝑑t𝑑ϕ=(2πΔt)I\displaystyle=\int_{C}\sqrt{-g_{T}}\,\left(\frac{I}{\sqrt{-g_{T}}}\right)\,dt\,d\phi=\,(2\pi\Delta t)\,I (2.15)

with CC (along tt and ϕ\phi) the boundary of the 3D surface SS. Following Gralla:2014yja , we will refer to II as the polar current.

We can parametrize the field strength in terms of the polar current II. By Maxwell’s equations and again Stokes’ theorem, the integrated polar current SJ\int_{S}\star J is also equal to SdF=CF=CdAP\int_{S}d\star F=\int_{C}\star F=\int_{C}\star dA_{P}, so that dAP=Idtdϕ\star dA_{P}=I\,dt\wedge d\phi or

dAP=IgTgPdrdθ\displaystyle dA_{P}=\frac{I}{\sqrt{-g_{T}}}\sqrt{g_{P}}\,dr\wedge d\theta (2.16)

in equation (2.11).

The FFE equation (2.13) with (2.14) imposes the conditions

dAtdI=0anddAϕdI=0.\displaystyle dA_{t}\wedge dI=0\quad\text{and}\quad dA_{\phi}\wedge dI=0. (2.17)

These conditions fix different terms of the field strength to be related to each other by

dAt=ωFdAϕ\displaystyle dA_{t}=-\,\omega_{F}\,dA_{\phi} (2.18)

and

dI\displaystyle dI =fdAϕorI=I(Aϕ).\displaystyle=fdA_{\phi}\quad\text{or}\quad I=I(A_{\phi})\,. (2.19)

The field strength thus has to be of the form

F=dAϕ(dϕωFdt)+gPgTIdrdθ\displaystyle F=dA_{\phi}\wedge\left(d\phi-\omega_{F}dt\right)+\frac{\sqrt{g_{P}}}{\sqrt{-g_{T}}}\,I\,dr\wedge d\theta\, (2.20)

where ωF\omega_{F} is the angular velocity of the EM fields, and both ωF\omega_{F} and the polar current II are functions of AϕA_{\phi}.

As shown originally in Uchida2:1997 , plugging this expression for the field strength into the action (2.21) yields an effective 2D action

𝒮[A]𝒮eff[A]=12(|dϕωFdt|2|dAϕ|2+I2gT)gPgT𝑑r𝑑θ,\displaystyle\mathcal{S}[A]\rightarrow\mathcal{S}^{eff}[A]=-\frac{1}{2}\int\left(\left|d\phi-\omega_{F}dt\right|^{2}|dA_{\phi}|^{2}+\frac{I^{2}}{g_{T}}\right)\sqrt{g_{P}}\sqrt{-g_{T}}\,dr\,d\theta\,, (2.21)

with the notation |X|2=gabXaXb|X|^{2}=g^{ab}X_{a}X_{b} for a 1-form XX. The integration over tt and ϕ\phi only produces overall volume factors. This action is a generalization of the Scharlemann-Wagoner action for pulsars WS to curved space-times. Similar results can be obtained from the Einstein-Maxwell action for a field strength of the form (2.20) with the force-free condition enforced through the use of a Lagrange multiplier term Thompson:1998ss ; Buniy:2013sca . Caution has to be taken in the process of eliminating APA_{P} from the action using I(Aϕ)I(A_{\phi}) Uchida2:1997 .

The problem is now reduced to solving the remaining FFE equation, also called the stream equation, for the toroidal gauge field Aϕ(xa)A_{\phi}(x^{a}). It is obtained as the Euler-Lagrange equation of the action 𝒮eff[A]=𝑑r𝑑θ\mathcal{S}^{eff}[A]=\int\mathcal{L}\,drd\theta, given by

a((aAϕ))Aϕ=0.\partial_{a}\left(\frac{\partial\mathcal{L}}{\partial(\partial_{a}A_{\phi})}\right)-\frac{\partial\mathcal{L}}{\partial A_{\phi}}=0\,. (2.22)

In the ensuing analysis we will find the action, derive the stream equation and solve this equation for specific choices of the rotating background metrics.

General rotating black hole metric

To illustrate the simplicity of this 2D force-free action (2.21), one can take a general stationary and axisymmetric block-diagonal metric

ds2=α2dt2+ω¯2(dϕ+ωdt)2+(gP)abdxadxb(a,b=r,θ).ds^{2}=-\alpha^{2}dt^{2}+\bar{\omega}^{2}(d\phi+\omega\,dt)^{2}+(g_{P})_{ab}\,dx^{a}dx^{b}\qquad(a,b=r,\theta)\,. (2.23)

Considering a field strength (per construction compatible with the background symmetries) of the form

F=dAϕ(dϕωFdt)+gPαω¯Idrdθ\displaystyle\begin{split}F&=dA_{\phi}\wedge\left(d\phi-\omega_{F}dt\right)+\frac{\sqrt{g_{P}}}{\alpha\bar{\omega}}\,I\,dr\wedge d\theta\,\end{split} (2.24)

with functions ωF(Aϕ)\omega_{F}(A_{\phi}) and I(Aϕ)I(A_{\phi}), leads to the 2D poloidal system given by

𝒮[A]=12gP𝑑r𝑑θ(𝒞|dAϕ|2I(Aϕ)2αω¯)\displaystyle\mathcal{S}[A]=-\frac{1}{2}\int\sqrt{g_{P}}\,dr\,d\theta\left(\mathcal{C}|dA_{\phi}|^{2}-\frac{I(A_{\phi})^{2}}{\alpha\bar{\omega}}\right) (2.25)

with

𝒞=αω¯ω¯α(ωF+ω)2.\displaystyle\mathcal{C}=\frac{\alpha}{\bar{\omega}}-\frac{\bar{\omega}}{\alpha}(\omega_{F}+\omega)^{2}\,\,. (2.26)

3 Near Horizon geometries

Rather than analyzing the 2D poloidal problem directly in the Kerr black hole geometry, it has proved advantageous to concentrate specifically on the near-horizon regions, which are described by a decoupled metric. These metrics possess a higher amount of symmetry than the black hole geometry they are derived from through a scaling limit. It is this high amount of symmetry that can be exploited in finding ansatze for symmetric, semi-analytic FFE solutions. This approach has been successfully applied in the near horizon of extremal Kerr or NHEK geometry, in the sense that energy-extracting solutions have been obtained Lupsasca:2014hua ; Lupsasca:2014pfa ; Zhang:2014pla . (However, we will comment on an unphysical feature of such solutions in the discussion of the energy flux.) We generalize the search for energy-extracting FFE solutions to include near-horizon geometries of AdS-Kerr black holes. Indeed, a 3D version of such a solution was presented in Jacobson:2017xam for the BTZ black hole. For previous work on the BZ process in AdS-Kerr, see Wang:2014vza .

In this section we collect the near horizon geometries that we will consider in this paper, each of the general rotating form (2.23): NHEK, AdS-NHEK, SE-NHEK, and near horizon extremal BTZ, which we will refer to as NHEBTZ. They are obtained from scaling limits of the respective black hole geometries. These limits are summarized in appendix A. The action and stream equation associated to these specific near horizon geometries are also described.

3.1 Near Horizon Extreme geometries

In this paper we are interested in the region very near the horizon of extreme Kerr and AdS-Kerr. These regions are described by the so-called Near-Horizon Extreme geometries defined by

ds2=Γ(θ)[r2dt2+dr2r2+α(θ)2dθ2+γ(θ)2(dϕ+krdt)2],\displaystyle ds^{2}=\Gamma(\theta)\left[-r^{2}dt^{2}+\frac{dr^{2}}{r^{2}}+\alpha(\theta)^{2}d\theta^{2}+\gamma(\theta)^{2}(d\phi+k\,r\,dt)^{2}\right]\,, (3.1)

and characterized in each case by specific functions Γ(θ),α(θ),γ(θ)\Gamma(\theta),\alpha(\theta),\gamma(\theta) and parameter kk. A separate discussion of each geometry is given in the next subsections.

3.1.1 Near Horizon Extreme Kerr

The line element of the so-called Near-Horizon Extreme Kerr (NHEK) geometry Bardeen:1999px is of the form (3.1) with

Γ(θ)=M2(1+cos2θ),α(θ)2=1,γ(θ)=Λ(θ)=2sinθ1+cos2θ,k=1\displaystyle\Gamma(\theta)=M^{2}\left(1+\cos^{2}\theta\right)\,,\qquad\alpha(\theta)^{2}=1\,,\qquad\gamma(\theta)=\Lambda(\theta)=\frac{2\sin\theta}{1+\cos^{2}\theta}\,,\qquad k=1 (3.2)

and metric determinant g=ΛΓ2\sqrt{-g}=\Lambda\,\Gamma^{2}. It is the decoupled near horizon limit of extremal Kerr and co-rotates with the extremal Kerr metric at the angular velocity of the horizon ΩHext=12M\Omega_{H}^{ext}=\frac{1}{2M}, see equation (A.2).

In contrast with the original Kerr metric, the NHEK geometry is not asymptotically flat; the metric contains an AdS2 factor in the (r,t)(r,t) directions and correspondingly an 𝖲𝖫(2,)\mathsf{SL}(2,\mathbb{R}) isometry. The full isometry group is 𝖲𝖫(2,)×𝖴(1)\mathsf{SL}(2,\mathbb{R})\times\mathsf{U}(1). The 𝖴(1)\mathsf{U}(1) rotational symmetry is generated by the Killing vector field

W0=ϕ\displaystyle W_{0}=\,\partial_{\phi} (3.3)

and the 𝖲𝖫(2,)\mathsf{SL}(2,\mathbb{R}) symmetry by the Killing vector fields

H0\displaystyle H_{0} =ttrr,\displaystyle=t\,\partial_{t}-r\,\partial_{r}\,, (3.4)
H+\displaystyle H_{+} =2t,\displaystyle=\sqrt{2}\,\partial_{t}\,, (3.5)
H\displaystyle H_{-} =2[12(t2+1r2)ttrr1rϕ].\displaystyle=\sqrt{2}\left[\frac{1}{2}\left(t^{2}+\frac{1}{r^{2}}\right)\,\partial_{t}-t\,r\,\partial_{r}-\frac{1}{r}\,\partial_{\phi}\right]\,. (3.6)

It is easily verified that these satisfy the 𝖲𝖫(2,)×𝖴(1)\mathsf{SL}(2,\mathbb{R})\times\mathsf{U}(1) commutation relations

[H0,H±]=H±,[H+,H]=2H0,[W0,H±]=0,[W0,H0]=0.\displaystyle\begin{split}\left[H_{0},H_{\pm}\right]&=\mp H_{\pm}\,,\qquad\,\left[H_{+},H_{-}\right]=2H_{0}\,,\\ \left[W_{0},H_{\pm}\right]&=0\,,\qquad\qquad\left[W_{0},H_{0}\right]=0\,.\end{split} (3.7)

3.1.2 Near Horizon Extreme AdS-Kerr

The near horizon of extreme AdS-Kerr (AdS-NHEK) geometry Hartman:2008pb is given by (3.1) where

Γ(θ)=r+2+a2cos2θΔ0,α(θ)2=Δ01(a2/l2)cos2θ,γ(θ)=(r+2+a2)sinθα(θ)Γ(θ)Ξ,\displaystyle\Gamma(\theta)=\frac{r_{+}^{2}+a^{2}\cos^{2}\theta}{\Delta_{0}}\,,\qquad\alpha(\theta)^{2}=\frac{\Delta_{0}}{1-(a^{2}/l^{2})\cos^{2}\theta}\,,\qquad\gamma(\theta)=\frac{(r_{+}^{2}+a^{2})\sin\theta}{\alpha(\theta)\,\Gamma(\theta)\,\Xi}\,,\, (3.8)

and constants Δ0=1+a2/l2+6r+2/l2\Delta_{0}=1+a^{2}/l^{2}+6r_{+}^{2}/l^{2}, Ξ=1a2/l2\Xi=1-a^{2}/l^{2} and k=2ar+Ξ/(Δ0(r+2+a2))k=2\,a\,r_{+}\,\Xi/(\Delta_{0}(r_{+}^{2}+a^{2})). This metric obeys Rμν=3l2gμνR_{\mu\nu}=-3\,l^{-2}g_{\mu\nu}. It is of the form (2.23) with gT=rγΓ\sqrt{-g_{T}}=r\,\gamma\,\Gamma, gP=αΓ/r\sqrt{g_{P}}=\alpha\,\Gamma/r and g=αγΓ2\sqrt{-g}=\alpha\,\gamma\,\Gamma^{2}.

The parameter r+r_{+} is defined as the largest root of

(l2+a2+3r+2)r+2l2a2=0.\displaystyle(l^{2}+a^{2}+3\,r_{+}^{2})\,r_{+}^{2}-l^{2}a^{2}=0\,. (3.9)

Finally note that the NHEK geometry (3.2) is recovered in the limit ll\rightarrow\infty while

k1,α(θ)1,γ(θ)Λ(θ).\displaystyle k\rightarrow 1\,,\qquad\alpha(\theta)\rightarrow 1\,,\qquad\gamma(\theta)\rightarrow\Lambda(\theta)\,. (3.10)

As in NHEK, a crucial feature of the AdS-NHEK region is that the original 𝖴(1)×𝖴(1)\mathsf{U}(1)\times\mathsf{U}(1) Kerr-AdS isometry group is enhanced to 𝖲𝖫(2,)×𝖴(1)\mathsf{SL}(2,\mathbb{R})\times\mathsf{U}(1). In fact, AdS-NHEK has the same isometries as NHEK up to a rescaling of ϕ\phi. The 𝖴(1)\mathsf{U}(1) rotational symmetry is generated by the Killing vector field W0W_{0} in (3.3). The time translation symmetry becomes part of an enhanced 𝖲𝖫(2,)\mathsf{SL}(2,\mathbb{R}) isometry group generated by the Killing vector fields H0H_{0} in (3.4), H+H_{+} in (3.5) and

H\displaystyle H_{-} =2[12(t2+1r2)ttrrkrϕ].\displaystyle=\sqrt{2}\left[\frac{1}{2}\left(t^{2}+\frac{1}{r^{2}}\right)\,\partial_{t}-t\,r\,\partial_{r}-\frac{k}{r}\,\partial_{\phi}\right]\,. (3.11)

The Killing vectors satisfy the 𝖲𝖫(2,)×𝖴(1)\mathsf{SL}(2,\mathbb{R})\times\mathsf{U}(1) commutation relations in (3.7).

3.1.3 Super-Entropic Near Horizon Extremal AdS-Kerr

The near horizon geometry of the super-entropic extremal AdS-Kerr black hole Sinamuli:2015drn , or simply SE-NHEK metric, is of the form (3.1)(\ref{NHE}) where now

Γ(θ)=l2(1+3cos2θ)12,α(θ)2=4sin2θ,γ(θ)=4l23sinθα(θ)Γ(θ),k=38.\displaystyle{\Gamma}(\theta)=\frac{l^{2}(1+3\cos^{2}\theta)}{12}\,,\qquad{\alpha}(\theta)^{2}=\frac{4}{\sin^{2}\theta}\,,\qquad{\gamma}(\theta)=\frac{4\,l^{2}}{3}\frac{\sin\theta}{{\alpha}(\theta)\,{\Gamma}(\theta)}\,,\qquad{k}=\frac{\sqrt{3}}{8}\,.\quad (3.12)

There are essentially two ways to derive this metric. In Appendix A we describe how to obtain the near horizon geometry from the extremal super-entropic AdS-Kerr black hole Cvetic:2010jb ; Hennigar:2015cja . A more straightforward way is to start with the AdS-NHEK line element (3.1) with (3.8), and before taking ala\rightarrow l rescale ϕϕΞ{\phi}\rightarrow{\phi}\,\Xi. The coordinate can be chosen such that ϕϕ+2π\phi\sim\phi+2\pi (for the new angle ϕ\phi). This geometry has the special feature that the locations θ=0,π\theta=0,\pi are removed from the space-time. The isometry group of the SE-NHEK geometry is 𝖲𝖫(2,)×𝖴(1)\mathsf{SL}(2,\mathbb{R})\times\mathsf{U}(1) as for AdS-NHEK, with the same Killing vector fields (3.3)-(3.5) and (3.11)(\ref{eq:H-}) (with kk in (3.12)).

3.1.4 Near Horizon Extreme BTZ

For future reference we also describe the near horizon geometry of the extreme BTZ (NHEBTZ) black hole metric Coussaert:1994tu ; Balasubramanian:2009bg ; deBoer:2010ac . The line-element is

ds2\displaystyle ds^{2} =l24dr2r2+2rldtdϕ+r+2dϕ2.\displaystyle=\frac{l^{2}}{4}\frac{dr^{2}}{r^{2}}+2\frac{r}{l}dtd\phi+r_{+}^{2}d\phi^{2}. (3.13)

The geometry retains all the relevant aspects of black holes, i.e. a horizon, and necessary ingredients for energy extraction, i.e. an ergosphere. While the NHEBTZ region provides a rich context to study FFE, the focus of our work will remain primarily in 4 dimensions. On the BTZ spacetime, purely electromagnetic versions of the BZ process were found, in which plasma surprisingly plays no role Jacobson:2017xam . In section 5.5, we employ these exact analytical FFE solutions in BTZ to argue that our prescription reproduces the energy flux from the extreme black hole throat.

3.2 Action and stream equation

We now turn to the study of the force-free electrodynamics action in the near horizon geometries. For a near horizon extremal metric (3.1), the action (2.21) is

𝒮[Aϕ]=𝑑r𝑑θ[dα2(r2(rAϕ)2+1α2(θAϕ)2)+α2r2γI(Aϕ)2]dααr𝒞=αγ(ωFr+k)2αγ.\displaystyle\begin{split}\mathcal{S}[A_{\phi}]&=\int drd\theta\left[\frac{d_{\alpha}}{2}\left(r^{2}(\partial_{r}A_{\phi})^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}A_{\phi})^{2}\right)+\frac{\alpha}{2r^{2}\gamma}I(A_{\phi})^{2}\right]\\ &\qquad\qquad d_{\alpha}\equiv-\frac{\alpha}{r}\mathcal{C}=\alpha\,\gamma\left(\frac{\omega_{F}}{r}+k\right)^{2}-\frac{\alpha}{\gamma}\,.\end{split} (3.14)

The relevance of 𝒞\mathcal{C} is that it becomes zero at the so-called light surface or light cylinder. At these locations, an observer co-rotating with the field lines would have to travel at the speed of light.

Variation of this action gives the stream equation for AϕA_{\phi},

θ(dα1α2θAϕ)+r(dαr2rAϕ)12Aϕdα(r2(rAϕ)2+1α2(θAϕ)2)αr2γIAϕI=0.\displaystyle\partial_{\theta}(d_{\alpha}\,\frac{1}{\alpha^{2}}\partial_{\theta}A_{\phi})+\partial_{r}(d_{\alpha}\,r^{2}\partial_{r}A_{\phi})-\frac{1}{2}\partial_{A_{\phi}}d_{\alpha}\left(r^{2}(\partial_{r}A_{\phi})^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}A_{\phi})^{2}\right)-\frac{\alpha}{r^{2}\gamma}I\,\partial_{A_{\phi}}I=0\,. (3.15)

Further details about the actions and stream equations can be found in Appendix B. Observe that the stream equation (3.15) is highly nonlinear and can in general only be solved numerically. Moreover, the possibility of 𝒞\mathcal{C} having zeros in the domain of integration may lead to further complications. Despite these issues, the symmetries can be exploited to simplify the analysis. We will show that imposing scaling symmetry allows to solve the force-free equations semi-analytically and find energy extracting configurations.

4 Force-Free Electrodynamics solutions

In this section we construct solutions to the FFE stream equations in (AdS/SE-)NHEK. The stream equation (3.15) for the gauge field component Aϕ(r,θ)A_{\phi}(r,\theta) is written out explicitly for the (AdS/SE-)NHEK background geometries (see also Appendix B). To obtain the stream equations in the form (3.15) we already have used one aspect of the symmetry of the problem, that is, the gauge field solution is required to have the same independence on time tt and azimuthal angle ϕ\phi as the stationary and axisymmetric background metrics. This strategy can be applied further by also imposing the scaling symmetry of the background near horizon metrics on the solution. This gives rise to two ansatze for the behavior of the solution as a function of the radius rr, which we will refer to as the ‘scaling ansatz’ (which was considered earlier in Zhang:2014pla ; Lupsasca:2014hua ) and the ‘log ansatz’. For these ansatze, the stream equations reduce further to a single ODE for the θ\theta-profile of AϕA_{\phi}, which can be solved numerically. The ODE’s are summarized in section 4.2.

4.1 Ansatze

Consider the stationary and axisymmetric field strength ansatz (2.24), written out explicitly to

F=rAϕdrdϕ+θAϕdθdϕωFrAϕdrdtωFθAϕdθdt+Iαω¯gPdrdθ\displaystyle F=\partial_{r}A_{\phi}dr\wedge d\phi+\partial_{\theta}A_{\phi}d\theta\wedge d\phi-\omega_{F}\partial_{r}A_{\phi}dr\wedge dt-\omega_{F}\partial_{\theta}A_{\phi}d\theta\wedge dt+\frac{I}{\alpha\bar{\omega}}\sqrt{g_{P}}dr\wedge d\theta (4.1)

where gPαω¯\frac{\sqrt{g_{P}}}{\alpha\bar{\omega}} scales as 1/r21/r^{2} for each of the near horizon geometries we consider. In the form (4.1), it is easy to read off the conditions for self-similar behavior of the field strength under scaling transformations.

4.1.1 Scaling ansatz

The field strength (4.1) will display scaling symmetry

FλhF\displaystyle F\rightarrow\lambda^{h}F (4.2)

under a scaling transformation rλrr\rightarrow\lambda\,r, tt/λt\rightarrow t/\lambda generated by H0=rrttH_{0}=r\partial_{r}-t\partial_{t} in (3.4), only if

rAϕrh1,θAϕrh,ωFr,Irh+1.\displaystyle\partial_{r}A_{\phi}\sim r^{h-1},\quad\partial_{\theta}A_{\phi}\sim r^{h},\quad\omega_{F}\sim r,\quad I\sim r^{h+1}\,. (4.3)

These conditions are solved by the ‘scaling ansatz’ for AϕA_{\phi} in terms of a field Φ(θ)\Phi(\theta), and II and ωF\omega_{F} as functions of AϕA_{\phi}:

Aϕ=rhΦ(θ),h0I=I0Aϕ1+1/hωF=ω0Aϕ1/h\displaystyle\begin{split}A_{\phi}&=r^{h}\Phi(\theta),\qquad h\neq 0\\ I&=I_{0}\,A_{\phi}^{1+1/h}\\ \omega_{F}&=\omega_{0}A_{\phi}^{1/h}\end{split} (4.4)

where I0I_{0} and ω0\omega_{0} are integration constants. By construction, the scaling ansatz field strength satisfies the symmetries of the (AdS/SE-)NHEK region

W0F=0,H+F=0,H0F=hF.\displaystyle\mathcal{L}_{W_{0}}F=0\,,\qquad\,\mathcal{L}_{H_{+}}F=0\,,\qquad\mathcal{L}_{H_{0}}F=-hF\,\,. (4.5)

Moreover, the scaling ansatz vector potential, with At=ω0Aϕ1+1/h/(1+1/h)+cA_{t}=\omega_{0}A_{\phi}^{1+1/h}/(1+1/h)+c satisfies the same symmetries, W0A=0\mathcal{L}_{W_{0}}A=0, H+A=0\mathcal{L}_{H_{+}}A=0 and H0A=hA\mathcal{L}_{H_{0}}A=-hA, if the constant cc equals zero.

4.1.2 Log ansatz

The h=0h=0 case needs to be handled separately. Imposing the scaling symmetry

FF\displaystyle F\rightarrow F (4.6)

under the scaling transformation rλrr\rightarrow\lambda\,r, tt/λt\rightarrow t/\lambda, requires

rAϕr1,θAϕ1,ωFr,Ir.\displaystyle\partial_{r}A_{\phi}\sim r^{-1},\quad\partial_{\theta}A_{\phi}\sim 1,\quad\omega_{F}\sim r,\quad I\sim r. (4.7)

This leads to the ‘log ansatz’ in terms of a field Φ(θ)\Phi(\theta):

Aϕ=log(rΦ(θ))/ω0I=I0rΦ(θ)ωF=ω0rΦ(θ)\displaystyle\begin{split}A_{\phi}&=\log(r\,\Phi(\theta))/\omega_{0}\\ I&=I_{0}\,r\,\Phi(\theta)\\ \omega_{F}&=\omega_{0}\,r\,\Phi(\theta)\end{split} (4.8)

with constants I0I_{0} and ω0\omega_{0}. The same invariance (4.5) of the field strength applies to this log ansatz. However, the gauge field is not in a highest-weight representation of 𝖲𝖫(2,)\mathsf{SL}(2,\mathbb{R}) as H0A0\mathcal{L}_{H_{0}}A\neq 0. In this sense the log ansatz could be called an approximate symmetric ansatz.

4.2 Equations of motion

First let us focus on the NHEK background. The stream equation (B.3) for a field AϕA_{\phi} of the form specified in the scaling ansatz (4.4) reduces to an ODE for the field Φ(θ)\Phi(\theta), which we can call the ‘NHEK scaling EOM’:

θ(dθΦ)+dh(h+1)Φ12(Φd)(h2Φ2+(θΦ)2)1ΛI02(1+1h)Φ1+2/h=0withd=Λ(ω0Φ1/h+1)21Λ.\displaystyle\begin{split}&\partial_{\theta}\left(d\,\partial_{\theta}\Phi\right)+d\,h(h+1)\Phi-\frac{1}{2}(\partial_{\Phi}d)\left(h^{2}\Phi^{2}+(\partial_{\theta}\Phi)^{2}\right)-\frac{1}{\Lambda}I_{0}^{2}(1+\frac{1}{h})\Phi^{1+2/h}=0\\ &\qquad\qquad\text{with}\quad d=\Lambda(\omega_{0}\Phi^{1/h}+1)^{2}-\frac{1}{\Lambda}\,.\end{split} (4.9)

Here dd is itself a functional of Φ(θ)\Phi(\theta) and is defined in (3.14) to be proportional to the functional 𝒞\mathcal{C}, which determines the location of light surfaces.

Evaluating the EOM (3.14) for the log ansatz (4.8) leads to the ‘NHEK log EOM’ for Φ(θ)\Phi(\theta),

θ(DθΦ)12(ΦD)(Φ2+(θΦ)2)1ΛI02Φ=0withD=Λ(1+1ω0Φ)21Λ1ω02Φ2.\displaystyle\begin{split}&\partial_{\theta}\left(D\,\partial_{\theta}\Phi\right)-\frac{1}{2}(\partial_{\Phi}D)\left(\Phi^{2}+(\partial_{\theta}\Phi)^{2}\right)-\frac{1}{\Lambda}I_{0}^{2}\Phi=0\\ &\qquad\qquad\text{with}\quad D=\Lambda\left(1+\frac{1}{\omega_{0}\Phi}\right)^{2}-\frac{1}{\Lambda}\frac{1}{\omega_{0}^{2}\Phi^{2}}\,.\end{split} (4.10)

Similarly, for a near-horizon region of AdS-Kerr (3.1), the ‘AdS-NHEK scaling EOM’

θ(dα1α2θΦ)+dαh(h+1)Φ12(Φdα)(h2Φ2+1α2(θΦ)2)αγI02(1+1h)Φ1+2/h=0\displaystyle\partial_{\theta}\left(d_{\alpha}\frac{1}{\alpha^{2}}\partial_{\theta}\Phi\right)+d_{\alpha}\,h(h+1)\Phi-\frac{1}{2}(\partial_{\Phi}d_{\alpha})\left(h^{2}\Phi^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}\Phi)^{2}\right)-\frac{\alpha}{\gamma}I_{0}^{2}(1+\frac{1}{h})\Phi^{1+2/h}=0
withdα=αγ(ω0Φ1/hk)2+αγ\displaystyle\qquad\qquad\qquad\text{with}\quad d_{\alpha}=\alpha\gamma(\omega_{0}\Phi^{1/h}-k)^{2}+\frac{\alpha}{\gamma} (4.11)

is the EOM (B.7) for the scaling ansatz (4.4). The metric functions α,γ\alpha,\gamma and kk are specified in (3.8) for AdS-NHEK and in (3.12) for SE-NHEK. The ‘AdS-NHEK log EOM’

θ(Dα1α2θΦ)12(ΦDα)(Φ2+1α2(θΦ)2)αγI02Φ=0withDα=αγ(1+kω0Φ)2αγ1ω02Φ2\displaystyle\begin{split}&\partial_{\theta}\left(D_{\alpha}\frac{1}{\alpha^{2}}\,\partial_{\theta}\Phi\right)-\frac{1}{2}(\partial_{\Phi}D_{\alpha})\left(\Phi^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}\Phi)^{2}\right)-\frac{\alpha}{\gamma}I_{0}^{2}\Phi=0\\ &\qquad\qquad\text{with}\quad D_{\alpha}=\alpha\gamma\left(1+\frac{k}{\omega_{0}\Phi}\right)^{2}-\frac{\alpha}{\gamma}\frac{1}{\omega_{0}^{2}\Phi^{2}}\end{split} (4.12)

is the EOM (B.8) for the log ansatz (4.8).

The functionals d,D,dαd,D,d_{\alpha} and DαD_{\alpha} introduced here become zero at the location of a light surface. For the solutions that we will discuss, these functionals will have a definite sign.

4.3 Boundary conditions

When solving the EOM’s in the previous section, the physical boundary conditions we impose on the field Φ(θ)\Phi(\theta) are the same as in Zhang:2014pla . The range of the angle θ\theta stretches from θ=0\theta=0 at the north pole, over θ=π/2\theta=\pi/2 at the equator, to θ=π\theta=\pi at the south pole. For the solution to be north-south symmetric, i.e. symmetric under reflection θπθ\theta\rightarrow\pi-\theta, we require the field to have a vanishing derivative at the equator,

Φ(π/2)=0.\displaystyle\Phi^{\prime}(\pi/2)=0. (4.13)

A second condition follows from considering the integrated polar current through a spherical cap S:θ<θ0S:\theta<\theta_{0}, as given in equation (2.15), C=SF=(2πΔt)I\int_{C=\partial S}\star F=\,(2\pi\Delta t)\,I. Consider the limit that the spherical cap shrinks to the point at the north pole θ00\theta_{0}\rightarrow 0. For a physical solution with non-diverging field strength FF at the north pole, the integrated polar current will vanish in this limit. For both our ansatze, (4.4) and (4.8), the vanishing of the polar current II at θ=0\theta=0 imposes the field Φ\Phi to vanish in that point. The second boundary condition is therefore

Φ(0)=0.\displaystyle\Phi(0)=0. (4.14)

4.4 Solutions

A shooting method is employed to numerically solve the EOM’s of section 4.2 using NDSolve in Mathematica. We recover a NHEK scaling solution that has previously been discussed in the literature, but have not succeeded in finding a NHEK log solution that satisfies the boundary condition (4.14). The new solutions we find are an AdS-NHEK scaling solution and an SE-NHEK log solution. The Φ(θ)\Phi(\theta) profiles for the numerical solutions are presented in Figures 2-4. To determine whether they are energy-extracting, we turn now to a discussion of the energy flux.

In the following sections, we will evaluate the energy and angular momentum flux densities of near horizon geometries to show that our force-free solutions do indeed produce non-trivial fluxes measured by stationary observers outside the near horizon throats.

5 Energy flux from extreme black hole throat

Before analyzing in this section the energy flux of our obtained solutions in rotating geometries, we first turn to a toy model. The toy model consists of a rotating electromagnetic (EM) field configuration, and serves to illustrate that the direction of the Poynting flux, i.e. whether the set-up has an inwards or outwards pointing flux of energy, depends on the rotation of the observer. The lesson relevant for the discussion of the energy flux of the (AdS/SE-)NHEK solutions, is that it is the Poynting flux measured by a Kerr observer rather than a near horizon observer (which rotate with respect to each other) that determines whether or not a solution is energy extracting.

5.1 Toy model

Refer to caption
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Figure 1: Toy model set-up of a rotating conducting cylinder in the lab frame (left) and a frame that rotates with the cylinder (right).

Consider a conducting cylinder that rotates with an angular velocity ΩH\Omega_{H} and is placed in a radial magnetic field BrB_{r}. This is an academic set-up that we consider for the sake of argument of describing the energy outflux in a rotating frame. The set-up has non-zero fields

Ez=rωFBr(r),Bθ=Bθ(r),Br=Br(r).\displaystyle E_{z}=r\omega_{F}B_{r}(r),\quad B_{\theta}=B_{\theta}(r),\quad B_{r}=B_{r}(r). (5.1)

The EE-field contributes a term σωFrBr\sigma\omega_{F}rB_{r} proportional to the conductivity σ\sigma to the current JzJ_{z}. Because the conducting cylinder moves with a velocity vv, the charges in it feel an electromotive force qv×Bqv\times B, adding another term to the current. In total, Jz=σ(ωFΩH)rBrJ_{z}=\sigma(\omega_{F}-\Omega_{H})rB_{r}. The current induces, by the integral Ampere law, the BB-field BθJzσ(ωFΩH)r2BrB_{\theta}\sim J_{z}\sim\sigma(\omega_{F}-\Omega_{H})r^{2}B_{r}.

The Poynting vector, as defined in (C.27), is P=E×B=(ωFBrBθ,ωFBr2,0)P=E\times B=(-\omega_{F}B_{r}B_{\theta},\omega_{F}B_{r}^{2},0) for P=(Pr,Pθ,Pz)P=(P^{r},P^{\theta},P^{z}). Its radial component is

Pr=BθEzr=ωFBrBθσr2Br2ωF(ΩHωF)\displaystyle P^{r}=-\frac{B_{\theta}E_{z}}{r}=-\omega_{F}B_{r}B_{\theta}\sim\sigma r^{2}B_{r}^{2}\omega_{F}(\Omega_{H}-\omega_{F}) (5.2)

so that the sign of the vector is determined by the sign of ΩHωF\Omega_{H}-\omega_{F}.

The system can also be observed from a rotating frame with angular velocity ω=ΩH\omega=\Omega_{H} or θ=θΩHt\theta^{\prime}=\theta-\Omega_{H}t. In the rotating frame, the contribution to the current that in the lab frame originated from an electromotive force, has to follow from an electric field contribution. The total observed electric field (in the sense that it obeys Faraday’s equation in the rotating frame, see (C.38) in Appendix C) is given by Ezrot=r(ωFΩH)BrE_{z}^{rot}=r(\omega_{F}-\Omega_{H})B_{r}. The observed magnetic fields (C.39) remain the same as in (5.1). The Poynting flux in the rotating frame222Note that the mixing of EE and BB fields in rotating frames makes the definitions of EE and BB ambiguous, reflected in the Maxwell equations (C.43)-(C.46) for E,B,Erot,BrotE,B,E_{rot},B_{rot}. We refer to Appendix C for a discussion of EM fields in a rotating frame. can then be defined as Prot=Erot×BP_{rot}=E_{rot}\times B. It has radial component

Protr=BθEzrotr=Bθ(ωFΩH)Br(ωFΩH)2r2Br2.\displaystyle P^{r}_{rot}=-\frac{B_{\theta}E_{z}^{rot}}{r}=-B_{\theta}(\omega_{F}-\Omega_{H})B_{r}\sim-(\omega_{F}-\Omega_{H})^{2}r^{2}B_{r}^{2}. (5.3)

This is the Poynting flux in the right figure of Figure 1. It is inwards pointing, even though the physical Poynting flux in the lab frame (5.2) is outwards pointing.

Let us repeat the analysis of the toy model in a covariant language that will be straightforwardly applicable to the force-free electrodynamics in a rotating NHEK frame versus asymptotically non-rotating Kerr frame.

The field strength in the lab frame (C.26) is

Fμνlab=Brr(dθωFdt)dzBθrdrdz\displaystyle F_{\mu\nu}^{lab}=B_{r}r\left(d\theta-\omega_{F}dt\right)\wedge dz-\frac{B_{\theta}}{r}dr\wedge dz (5.4)

and the field strength in a rotating frame (C.48) (with θ=θωt\theta^{\prime}=\theta-\omega t) is

Fμνrot=Brr(dθ+(ωωF)dt)dzBθrdrdz.\displaystyle F_{\mu\nu}^{rot}=B_{r}r\left(d\theta^{\prime}+(\omega-\omega_{F})dt\right)\wedge dz-\frac{B_{\theta}}{r}dr\wedge dz\,. (5.5)

In particular, we will consider a frame that co-rotates with the cylinder, ω=ΩH\omega=\Omega_{H}.

The conserved energy flux seen by a stationary observer in the lab frame can be calculated from the Maxwell stress-energy tensor

Tμν=14gμνFαβFαβ+FμαFνα\displaystyle T_{\mu\nu}=-\frac{1}{4}g_{\mu\nu}F_{\alpha\beta}F^{\alpha\beta}+F_{\mu\alpha}F_{\nu}^{\phantom{\nu}\alpha} (5.6)

as

μ=Tμνχν\displaystyle\mathcal{E}^{\mu}=-T^{\mu\nu}\chi_{\nu} (5.7)

where χ=t\chi=\partial_{t} is the global timelike Killing vector. Similarly, the angular momentum flux

μ=Tμνην\displaystyle\mathcal{L}^{\mu}=T^{\mu\nu}\eta_{\nu} (5.8)

is defined in terms of the axial Killing vector η=θ\eta=\partial_{\theta}. Here and hereafter, it is understood that we have dropped the ‘EMEM’ label in the symbol TμνEMT^{EM}_{\mu\nu} to denote the electromagnetic stress-energy tensor defined in (5.6). The transformation matrix for the coordinate transformation from the lab frame, in cylindrical coordinates xμ=(t,r,θ,z)x^{\mu}=(t,r,\theta,z), to the rotating frame xμ=(t,r,θ,z)=(t,r,θΩHt,z)x^{\mu^{\prime}}=(t^{\prime},r^{\prime},\theta^{\prime},z^{\prime})=(t,r,\theta-\Omega_{H}t,z) is given by

xx=(10000100ΩH0100001).\displaystyle\frac{\partial x}{\partial x^{\prime}}=\left(\begin{array}[]{cccc}1&0&0&0\\ 0&1&0&0\\ \Omega_{H}&0&1&0\\ 0&0&0&1\end{array}\right). (5.13)

Under the coordinate transformation, the energy flux transforms to

μ=xμxμμ.\displaystyle\mathcal{E}^{\mu^{\prime}}=\frac{\partial x^{\mu^{\prime}}}{\partial x^{\mu}}\mathcal{E}^{\mu}. (5.14)

In particular, r=r\mathcal{E}^{r^{\prime}}=\mathcal{E}^{r}. This is the lab energy flux as measured by a rotating observer. In terms of the stress tensor in the rotating frame, it is given by

μ=Tνμχν=(TtμΩHTθμ)\displaystyle\mathcal{E}^{\mu^{\prime}}=-T^{\mu^{\prime}}_{\phantom{\mu}\nu^{\prime}}\chi^{\nu^{\prime}}=-(T^{\mu^{\prime}}_{\phantom{\mu^{\prime}}t^{\prime}}-\Omega_{H}T^{\mu^{\prime}}_{\phantom{\mu^{\prime}}\theta^{\prime}}) (5.15)

where we made use of χν=xνxμχμ=xνt=(1,0,ΩH,0)\chi^{\nu^{\prime}}=\frac{\partial x^{\nu^{\prime}}}{\partial x^{\mu}}\chi^{\mu}=\frac{\partial x^{\nu^{\prime}}}{\partial t}=(1,0,-\Omega_{H},0). It follows that the radial energy flux in the lab frame is obtained from a combination of the radial energy flux and angular momentum flux in the rotating frame

r=rotr+ΩHrotr,\displaystyle\mathcal{E}^{r}=\mathcal{E}^{r^{\prime}}_{rot}+\Omega_{H}\mathcal{L}^{r^{\prime}}_{rot}\,\,, (5.16)

where we introduced the notation rotrTtr\mathcal{E}^{r^{\prime}}_{rot}\equiv-T^{r^{\prime}}_{\phantom{\mu^{\prime}}t^{\prime}} and rotrTθr\mathcal{L}^{r^{\prime}}_{rot}\equiv T^{r^{\prime}}_{\phantom{\mu^{\prime}}\theta^{\prime}} in analogy with (5.7)-(5.8). We would like to point out that there is no ambiguity of interpretation in equation (5.16). It relates a component of the lab flux to components of the rotating frame fluxes, by making use of μ=xμxμ(TtμΩHTθμ)\mathcal{E}^{\mu}=-\frac{\partial x^{\mu}}{\partial x^{\mu^{\prime}}}(T^{\mu^{\prime}}_{\phantom{\mu^{\prime}}t^{\prime}}-\Omega_{H}T^{\mu^{\prime}}_{\phantom{\mu^{\prime}}\theta^{\prime}}). In this simple set-up where r=rr^{\prime}=r, we can change rr^{\prime} to rr on the right hand side of (5.16).

From equation (C.50) in the general discussion in the appendix, the energy flux rotr=r(ΩHωF)BrBθ\mathcal{E}^{r^{\prime}}_{rot}=r(\Omega_{H}-\omega_{F})B_{r}B_{\theta} equals the Poynting flux ProtrP^{r}_{rot} in (5.3), and rotr=rBrBθ\mathcal{L}^{r}_{rot}=-rB_{r}B_{\theta}. The relation (5.16) thus relates the radially inwards Poynting vector measured in the rotating frame to the outwards one measured in the lab frame

Pr=Protr+ΩHrotr,\displaystyle P^{r}=P^{r}_{rot}+\Omega_{H}\mathcal{L}^{r}_{rot}\,\,, (5.17)

consistent with equations (5.2) and (5.3). The outflux PrP^{r} in (5.2) is positive when ΩH>ωF\Omega_{H}>\omega_{F}, and rotational energy can be transferred from the cylinder to the field. The suggestive notation ΩH\Omega_{H} for the angular velocity of the cylinder indicates that we will think of the rotation of a black hole in an analogous way.

5.2 Energy flux in Kerr

In this section we derive the analogue of the relation (5.16) for the energy flux measured in a Kerr geometry as a function of the flux measured by an observer in the near-horizon region.

The NHEK geometry (3.2), with xμ=(t,ϕ,r,θ)x^{\mu}=(t,\phi,r,\theta), is obtained from the Kerr geometry in Boyer-Lindquist coordinates xμ^=(t^,ϕ^,r^,θ^)x^{\hat{\mu}}=(\hat{t},\hat{\phi},\hat{r},\hat{\theta}) through the coordinate transformation (see (A.3))

t^=tζ,ϕ^=ϕ+t2Mζ,r^=2M2ζr+M,θ^=θ\displaystyle\hat{t}=\frac{t}{\zeta},\qquad\hat{\phi}=\phi+\frac{t}{2M\zeta},\qquad\hat{r}=2M^{2}\zeta r+M,\qquad\hat{\theta}=\theta (5.18)

in the limit where the scaling parameter ζ\zeta vanishes. The transformation matrix is

x^x=(1ζ00012Mζ100002M2ζ00001).\displaystyle\frac{\partial\hat{x}}{\partial x}=\left(\begin{array}[]{cccc}\frac{1}{\zeta}&0&0&0\\ \frac{1}{2M\zeta}&1&0&0\\ 0&0&2M^{2}\zeta&0\\ 0&0&0&1\end{array}\right)\,\,. (5.23)

We are interested in the energy flux seen by a stationary Kerr observer (with hatted coordinates). It is defined in terms of the Kerr stress tensor Tμ^ν^T^{\hat{\mu}\hat{\nu}} and the Kerr timelike Killing vector χμ^=(1,0,0,0)\chi^{\hat{\mu}}=(1,0,0,0) as Blandford:1977ds

μ^Tμ^ν^χν^=Tt^μ^.\displaystyle\mathcal{E}^{\hat{\mu}}\equiv-T^{\hat{\mu}\hat{\nu}}\chi_{\hat{\nu}}=-T^{\hat{\mu}}_{\phantom{\mu}\hat{t}}\,\,. (5.24)

The solutions we obtained are solutions in the NHEK geometry (with unhatted coordinates). We therefore need to work out first what the relation is between μ^\mathcal{E}^{\hat{\mu}} and quantities measured in NHEK. This follows closely the discussion in section 5.1 of the toy model (equations (5.14) and (5.15)), with the Kerr frame taking the role of the lab frame, and the NHEK frame the role of the rotating frame.

If we introduce the notation333Note that r\mathcal{E}^{r} is not the radial energy flux observed by a stationary NHEK observer, which would be defined as Tμνξν=Ttμ-T^{{\mu\nu}}\xi_{\nu}=-T^{\mu}_{\phantom{\mu}t} in terms of the NHEK timelike Killing vector ξ\xi. When it is necessary to distinguish this object, we will refer to it as rotμTtμ\mathcal{E}^{\mu}_{rot}\equiv-T^{\mu}_{\phantom{\mu}t}, following the notation in equation (5.16) in the toy model.

μTμνχν\displaystyle\mathcal{E}^{\mu}\equiv-T^{{\mu\nu}}\chi_{\nu} (5.25)

in terms of the transformed TμνT^{{\mu\nu}} and χμ\chi^{\mu}, then we find

r=12M2ζr^.\displaystyle\mathcal{E}^{r}=\frac{1}{2M^{2}\zeta}\mathcal{E}^{\hat{r}}. (5.26)

This gives the scaling between the energy flux rate per NHEK time, r\mathcal{E}^{r}, and the energy flux rate per Kerr time, r^\mathcal{E}^{\hat{r}}, and expresses that the scale invariant quantity is the energy rΔtr^Δt^\mathcal{E}^{r}\Delta t\sim\mathcal{E}^{\hat{r}}\Delta\hat{t}.

Furthermore, because the stationary Kerr observer is rotating from the NHEK-perspective

χμ=xμxμ^χμ^=xμt^=(ζ,12M,0,0),\displaystyle\chi^{\mu}=\frac{\partial x^{\mu}}{\partial x^{\hat{\mu}}}\chi^{\hat{\mu}}=\frac{\partial x^{\mu}}{\partial\hat{t}}=\left(\zeta,-\frac{1}{2M},0,0\right), (5.27)

it follows that

r=(ζTtr12MTϕr).\displaystyle\mathcal{E}^{r}=-\left(\zeta T^{r}_{\phantom{\mu}t}-\frac{1}{2M}T^{r}_{\phantom{\mu}\phi}\right). (5.28)

We thus find the following expression for the Kerr energy flux as a function of NHEK observables

r^=λ22(Ttr1λTϕr),\displaystyle\mathcal{E}^{\hat{r}}=-\frac{\lambda^{2}}{2}\left(T^{r}_{\phantom{\mu}t}-\frac{1}{\lambda}T^{r}_{\phantom{\mu}\phi}\right), (5.29)

which follows most directly from the transformation Tν^μ^=Tνμxμ^xμxνxν^T^{\hat{\mu}}_{\phantom{\mu}\hat{\nu}}=T^{\mu}_{\phantom{\mu}\nu}\frac{\partial x^{\hat{\mu}}}{\partial x^{\mu}}\frac{\partial x^{\nu}}{\partial x^{\hat{\nu}}}. Here the scaling parameter

λ=2Mζ\displaystyle\lambda=2M\zeta (5.30)

was introduced, which has the following interpretation. By writing the Kerr to NHEK angle transformation as

ϕ^=ϕ+1λt,\displaystyle\hat{\phi}=\phi+\frac{1}{\lambda}t\,\,, (5.31)

the scale factor can be interpreted as the angular velocity ΩANHEK\Omega_{A}^{NHEK} of the asymptotic (Kerr) region as seen by a NHEK observer

ΩANHEK=1λ.\displaystyle\Omega_{A}^{NHEK}=\frac{1}{\lambda}. (5.32)

The rotation ω=r\omega=r of the NHEK metric (of the form (2.23)) should not exceed the value ΩANHEK\Omega_{A}^{NHEK}, and therefore the ‘gluing’ from NHEK to the asymptotic Kerr region should take place at

r=1λ.\displaystyle r_{*}=\frac{1}{\lambda}. (5.33)

This makes the statement that the NHEK region is glued to a Kerr region at rr\rightarrow\infty more precise (with λ0\lambda\rightarrow 0 per definition of the NHEK metric). We propose that the radial energy outflux in (5.29) evaluated at the gluing radius rr_{*},

r^(r)=λ22(Ttr1λTϕr)|r=r,\displaystyle\mathcal{E}^{\hat{r}}(r_{*})=-\frac{\lambda^{2}}{2}\left.\left(T^{r}_{\phantom{\mu}t}-\frac{1}{\lambda}T^{r}_{\phantom{\mu}\phi}\right)\right\rvert_{r=r_{*}}, (5.34)

gives a good measure for determining whether a force-free electrodynamics solution in a near-horizon geometry is energy-extracting. What is relevant in particular, is the sign of the total energy outflux through a constant r^\hat{r} hypersurface Σr^\Sigma_{\hat{r}},

E=Σr^r^(r)𝑑Σr^\displaystyle E=\int_{\Sigma_{\hat{r}}}\mathcal{E}^{\hat{r}}(r_{*})\,d\Sigma_{\hat{r}} (5.35)

with the directed surface element dΣr^d\Sigma_{\hat{r}} in Kerr related to the one in NHEK by dΣr^=12M2ζdΣrd\Sigma_{\hat{r}}=\frac{1}{2M^{2}\zeta}d\Sigma_{r}. For the axisymmetric and stationary solutions of section 4.4, the flux (5.34) is a function of θ^\hat{\theta} only, and as dΣrd\Sigma_{r} is just the volume element dtdϕdθdt\wedge d\phi\wedge d\theta multiplied with a positive function of θ\theta, it suffices for the determination of the sign of the extracted energy during a time interval Δt^\Delta\hat{t} to evaluate

E2πΔt^0π/2r^(r)𝑑θ^.\displaystyle E\sim 2\pi\Delta\hat{t}\int_{0}^{\pi/2}\mathcal{E}^{\hat{r}}(r_{*})\,d\hat{\theta}\,. (5.36)

Our proposal can be compared to the energy outflux measured by a zero angular momentum observer (ZAMO) in the NHEK frame. For a constant tt surface in NHEK with unit normal uμ(r,0,0,0)u_{\mu}\sim(-r,0,0,0), the associated ZAMO uμ(1r,1,0,0)u^{\mu}\sim(\frac{1}{r},-1,0,0) is such that upon evaluation at rr_{*} it takes the form

uμ(r)(ζ,12M,0,0).\displaystyle u^{\mu}(r_{*})\sim(\zeta,-\frac{1}{2M},0,0)\,\,. (5.37)

By comparison with the rotating NHEK observer χμ\chi^{\mu} in (5.27), we conclude that the energy outflux measured by the ZAMO uμ(r)u^{\mu}(r_{*}) matches (up to possible normalizations) the one in (5.34) measured by the stationary asymptotic Kerr observer χμ^=(1,0,0,0)\chi^{\hat{\mu}}=(1,0,0,0). This argument mimics the comments (D.6) and (D.7) in Appendix D as applied to the toy model.

5.3 Energy flux in AdS-Kerr

The discussion in the previous subsection can straightforwardly be repeated for the AdS case. As summarized in Appendix A, the transformation between AdS-Kerr (hatted coordinates) and its near-horizon region AdS-NHEK is

t^=tr0ϵ,ϕ^=ϕ+ΩHexttr0ϵ,r^=r++ϵr0r,θ^=θ,\displaystyle\hat{t}=t\frac{r_{0}}{\epsilon},\qquad\hat{\phi}=\phi+\Omega_{H}^{ext}\frac{t\,r_{0}}{\epsilon},\qquad\hat{r}=r_{+}+\epsilon\,r_{0}\,r,\qquad\hat{\theta}=\theta, (5.38)

with ΩHext\Omega_{H}^{ext} given in (A.9) and r0r_{0} in (A.8). The same coordinate transformation applies for the SE-NHEK limit from super-entropic AdS-Kerr, if ϕ^\hat{\phi} in (5.38) refers to the angle ψ^\hat{\psi} in the metric (A.10), and with ΩHext\Omega_{H}^{ext} given in (A.15) and r0r_{0} in (A.14). For the rest of this section we will refer to AdS-NHEK for definiteness, but the whole discussion applies equally well to SE-NHEK.

The conserved energy flux (5.24) measured by an observer χμ^=(1/Ξ,0,0,0)\chi^{\hat{\mu}}=(1/\Xi,0,0,0) at rest in AdS-Kerr is given in terms of the stress tensor components of the near-horizon observer

χμ(ϵr0,ΩHext,0,0)\displaystyle\chi^{\mu}\sim\left(\frac{\epsilon}{r_{0}},-\Omega_{H}^{ext},0,0\right) (5.39)

as

r^\displaystyle\mathcal{E}^{\hat{r}} =ϵr0(ϵr0TtrΩHextTϕr).\displaystyle=-\epsilon r_{0}\left(\frac{\epsilon}{r_{0}}T^{r}_{\phantom{\mu}t}-\Omega_{H}^{ext}T^{r}_{\phantom{\mu}\phi}\right)\,\,. (5.40)

The scaling parameter

λ=ϵr0ΩHext\displaystyle\lambda=\frac{\epsilon}{r_{0}\Omega_{H}^{ext}} (5.41)

sets the maximum value 1/λ1/\lambda of the rotation ω=kr\omega=k\,r of the NHEK region, resulting in a gluing radius

r=1kλ\displaystyle r_{*}=\frac{1}{k\lambda} (5.42)

at which we evaluate the flux,

r^(r)=ϵr0(ϵr0TtrΩHextTϕr)|r=r.\displaystyle\mathcal{E}^{\hat{r}}(r_{*})=-\epsilon r_{0}\left.\left(\frac{\epsilon}{r_{0}}T^{r}_{\phantom{\mu}t}-\Omega_{H}^{ext}T^{r}_{\phantom{\mu}\phi}\right)\right\rvert_{r=r_{*}}\,. (5.43)

An AdS-NHEK ZAMO uμ(1r,k,0,0)u^{\mu}\sim(\frac{1}{r},-k,0,0) evaluated at rr_{*} is of the form

uμ(r)(ϵr0,ΩHext,0,0)\displaystyle u^{\mu}(r_{*})\sim\left(\frac{\epsilon}{r_{0}},-\Omega_{H}^{ext},0,0\right) (5.44)

so that the Poynting flux measured by this observer will match the flux r^\mathcal{E}^{\hat{r}} measured by χμ\chi^{\mu}.

5.4 Discussion of energy flux profile

The main equations for energy extraction are given in equations (5.15) (for the toy model), (5.29) (for the Kerr energy flux r^\mathcal{E}^{\hat{r}}) and (5.40) (for the AdS-Kerr energy flux r^\mathcal{E}^{\hat{r}}). These equations reflect the transformation under respectively the coordinate transformation between the lab and rotating frame in the toy model, and the near-horizon coordinate transformation, with Tν^μ^=Tνμxμ^xμxνxν^T^{\hat{\mu}}_{\phantom{\mu}\hat{\nu}}=T^{\mu}_{\phantom{\mu}\nu}\frac{\partial x^{\hat{\mu}}}{\partial x^{\mu}}\frac{\partial x^{\nu}}{\partial x^{\hat{\nu}}}. Let us distill from the (AdS-)Kerr energy flux formula the main expected behavior. More specifically we want to determine what factors will be crucial to the sign of the flux.

We start by repeating here the equation that can be applied for both the Kerr and the AdS-Kerr energy fluxes, i.e. equation (5.34) with rr_{*} defined in (5.42),

r^(r)(Ttr1λTϕr)|r=r,r=1kλ.\displaystyle\mathcal{E}^{\hat{r}}(r_{*})\sim-\left.\left(T^{r}_{\phantom{\mu}t}-\frac{1}{\lambda}T^{r}_{\phantom{\mu}\phi}\right)\right\rvert_{r=r_{*}},\qquad r_{*}=\frac{1}{k\lambda}. (5.45)

For a NHEK solution, the corresponding Kerr flux is given by this r^(r)\mathcal{E}^{\hat{r}}(r_{*}) with the scaling parameter λ\lambda defined in (5.30) and k=1k=1. For an AdS-NHEK solution, similarly the AdS-Kerr flux is given by the same equation with λ\lambda now equal to (5.41), with parameters r0r_{0} and ΩHext\Omega_{H}^{ext} given in (A.8) and (A.9), and kk defined under equation (3.8). Finally, for an SE-NHEK solution, one can again use the flux equation with (5.41), where now r0r_{0} and ΩHext\Omega_{H}^{ext} are the ones from equations (A.14) and (A.15), and kk is defined in (3.12).

The two terms in the above flux equation are not independent, but related to each other as

Tϕr=1ωFTtr.\displaystyle T^{r}_{\phantom{r}\phi}=-\frac{1}{\omega_{F}}T^{r}_{\phantom{r}t}. (5.46)

Plugging this relation into (5.45) and replacing λ\lambda by krkr_{*}, we can write

r^(r)Ttr(1+krωF)|r=r.\displaystyle\mathcal{E}^{\hat{r}}(r_{*})\sim-\left.T^{r}_{\phantom{\mu}t}\left(1+\frac{kr}{\omega_{F}}\right)\right\rvert_{r=r_{*}}\,. (5.47)

All the geometries we consider are of the form (3.1), which in turn is of the form of a general rotating metric (2.23) with angular velocity Ωgtϕ/gϕϕ\Omega\equiv-g_{t\phi}/g_{\phi\phi} equal to Ω=kr\Omega=-kr. This allows to further rewrite the flux profile as

r^(r)ωFrotr(ΩωF)|r=r,\displaystyle\mathcal{E}^{\hat{r}}(r_{*})\sim\left.-\omega_{F}\,\mathcal{E}^{r}_{rot}\,\left(\Omega-\omega_{F}\right)\right\rvert_{r=r_{*}}, (5.48)

where we used the notation rotrTtr\mathcal{E}^{r}_{rot}\equiv-T^{r}_{\phantom{r}t} for the flux measured by an observer at rest in the near horizon region or ‘rotating frame’. It is clear from this form that the sign of the flux will be determined by whether or not the metric angular velocity is larger than the field angular velocity, as well as by the sign of the field angular velocity ωF\omega_{F} and the sign of the flux as measured by a non-rotating observer in the near-horizon region.

Equation (5.48) for the (AdS-)Kerr flux makes the equivalence with the toy model manifest: coupling back to the notation used in section 5.1 by replacing r^Pr\mathcal{E}^{\hat{r}}\rightarrow P^{r}, rotrProtr\mathcal{E}^{r}_{rot}\rightarrow P^{r}_{rot} and ΩΩH\Omega\rightarrow\Omega_{H}, equation (5.48) expresses that the lab Poynting flux PrP^{r} scales like ωFProtr(ΩHωF)-\omega_{F}P^{r}_{rot}(\Omega_{H}-\omega_{F}), as can be read off directly from the expressions in Figure 1.

5.5 Energy flux in BTZ

The aim here is to demonstrate the extent of the validity of applying the proposed toy model to the derivation of an energy flux from extreme near horizon black hole throats. To this end we employ an exact solution to FFE for rotating black holes, namely, the solution describing the BZ process Jacobson:2017xam in the 3-dimensional rotating black hole known as BTZ. The presumably unique, exact EM field is given in a simple, closed form for the BTZ metric (A.17) with coordinates (t^,ϕ^,r^)(\hat{t},\hat{\phi},\hat{r}). This result provides us with a set-up where the full FFE solution is known, i.e. not just in the near-horizon region. In particular, the FFE solution in BTZ will allow us to check equation (5.54) for the BTZ energy flux as measured by a NHEBTZ observer.

We begin by directly applying the near horizon procedure to the FFE solution in the BTZ metric. The energy extracting FFE solution in BTZ obtained in Jacobson:2017xam is given by

F^=Φ˙2πdt^dϕ^+Q2πr^dr^dt^Qr^(Ω(r^)ΩF)2πα(r^)2(dϕΩ(r^)dt^)dr^\displaystyle\hat{F}=\frac{\dot{\Phi}}{2\pi}d\hat{t}\wedge d\hat{\phi}+\frac{Q}{2\pi\hat{r}}d\hat{r}\wedge d\hat{t}-\frac{Q\,\hat{r}(\Omega(\hat{r})-\Omega_{F})}{2\pi\alpha(\hat{r})^{2}}(d\phi-\Omega(\hat{r})d\hat{t})\wedge d\hat{r} (5.49)

with electric charge QQ and magnetic monopole current Φ˙\dot{\Phi}, and the functions α\alpha and Ω\Omega given in (A.18). Including Znajek’s regularity condition implies Φ˙=Qr+(ΩHΩF)\dot{\Phi}=Qr_{+}(\Omega_{H}-\Omega_{F}), where the horizon angular velocity is given by ΩH=r/(lr+)\Omega_{H}=r_{-}/(lr_{+}) in terms of the horizons r±r_{\pm}.

Consider in particular the extreme BTZ solution (ΩHext=1/l\Omega^{ext}_{H}=1/l), with Φ˙=0\dot{\Phi}=0 (required to have a finite field strength in the NHEBTZ background) and ΩF=1/l\Omega_{F}=1/l. Its energy flux as defined in (5.24), with χ=t^\chi=\partial_{\hat{t}}, reads

μ^=Q24π2(r^2r+2)(1,1l,0).\displaystyle\mathcal{E}^{\hat{\mu}}=\frac{Q^{2}}{4\pi^{2}(\hat{r}^{2}-r_{+}^{2})}\left(1,\frac{1}{l},0\right)\,. (5.50)

Note that there is no radial energy outflux for this special case of the extreme BTZ solution. This is a consequence of the regularity condition imposed by the near-horizon solution. It causes the field angular velocity to reach the horizon angular velocity of the extremal BTZ black hole, ΩF=ΩHext\Omega_{F}=\Omega_{H}^{ext}, while energy extraction is achieved in the range 0<ΩF<ΩHext0<\Omega_{F}<\Omega_{H}^{ext}.

Following the near horizon limiting procedure defined in Appendix A (which involves defining new coordinates xμx^{\mu} in addition to taking the limit ϵ0\epsilon\rightarrow 0) for the energy flux μ^dxμ^=μdxμ=Q24π2ldϕ\mathcal{E}\equiv\mathcal{E}_{\hat{\mu}}dx^{\hat{\mu}}=\mathcal{E}_{\mu}dx^{\mu}=\frac{Q^{2}}{4\pi^{2}l}d\phi with (5.50) yields

μ=(Q24π2r,0,0),\displaystyle\mathcal{E}^{\mu}=\left(\frac{Q^{2}}{4\pi^{2}r},0,0\right), (5.51)

and for the extreme electromagnetic field (5.49) one finds

F=lQ4πrdϕdr.\displaystyle F=\frac{lQ}{4\pi r}d\phi\wedge dr\,. (5.52)

This result for the near horizon solution in the NHEBTZ background (3.13) is obtained specifically by making use of the conditions Φ˙=0\dot{\Phi}=0 and ΩF=1/l\Omega_{F}=1/l which impose finiteness and Znajek’s condition.

Imagine we had not known the full FFE solution in BTZ, but only the field (5.52) in NHEBTZ. The only non-vanishing component of the corresponding stress energy tensor is Tϕt=lQ24π2rT^{t}_{\phantom{t}\phi}=\frac{lQ^{2}}{4\pi^{2}r}. Following the discussion in the preceding sections, the energy flux measured by a rotating NHEBTZ observer χ=ϵt1lϕ\chi=\epsilon\partial_{t}-\frac{1}{l}\partial_{\phi} yields

μ=(ϵTμt1lTμϕ)=(Q24π2r,0,0),\displaystyle\mathcal{E}^{\mu}=-\left(\epsilon{T^{\mu}}_{t}-\frac{1}{l}{T^{\mu}}_{\phi}\right)=\left(\frac{Q^{2}}{4\pi^{2}r},0,0\right), (5.53)

in agreement with (5.51). The energy flux (5.53) computed solely with the field in NHEBTZ gives rise to the same energy flux \mathcal{E} as the one measured by the χ=t^\chi=\partial_{\hat{t}} observer at rest in BTZ. This is the extent to which our analysis of the NHEBTZ is exactly equivalent to our toy model prescription.

Now let us take a look at the gluing procedure. It suggests that the object

μ^(r)=xμ^xμ(ϵTμt1lTμϕ)|r=r=Q24π2rϵ(1,1l,0)\displaystyle\mathcal{E}^{\hat{\mu}}(r_{*})=-\left.\frac{\partial x^{\hat{\mu}}}{\partial x^{\mu}}\left(\epsilon{T^{\mu}}_{t}-\frac{1}{l}{T^{\mu}}_{\phi}\right)\right|_{r=r_{*}}=\frac{Q^{2}}{4\pi^{2}r_{*}\epsilon}\left(1,\frac{1}{l},0\right) (5.54)

allows the NHEBTZ observer, with no knowledge of the full BTZ solution, to obtain the profile of the energy outflux measured outside the throat. The gluing radius rr_{*} marking the ‘edge’ of the near horizon region is determined to be

r=r+2ϵ.\displaystyle r_{*}=\frac{r_{+}^{2}}{\epsilon}. (5.55)

This follows from a completely analogous reasoning as before. Namely, the angular velocity ΩA\Omega_{A}, which can be read off from the BTZ to near-horizon angle transformation ϕ^=ϕ+ΩAt\hat{\phi}=\phi+\Omega_{A}t given in (A.20), sets the maximal value ω(r)\omega(r_{*}) of the rotation ωgtϕ/gϕϕ=rlr+2\omega\equiv g_{t\phi}/g_{\phi\phi}=\frac{r}{lr_{+}^{2}} of the NHEBTZ metric (3.13). Writing out the evaluation at rr_{*} in (5.54) gives rise to a finite quantity

μ^(r)=Q24π2r+2(1,1l,0).\displaystyle\mathcal{E}^{\hat{\mu}}(r_{*})=\frac{Q^{2}}{4\pi^{2}r_{+}^{2}}\left(1,\frac{1}{l},0\right). (5.56)

It matches the full BTZ flux in (5.50) evaluated at the gluing point r^=r+2+ϵr\hat{r}_{*}=\sqrt{r_{+}^{2}+\epsilon r_{*}}.

6 Energy flux of force-free solutions

We are interested in the profile of r^(r)\mathcal{E}^{\hat{r}}(r_{*}) (defined in the previous section) as a function of θ^\hat{\theta} ranging from the north pole to the equator, and the positivity of 0π/2r^(r)𝑑θ^\int_{0}^{\pi/2}\mathcal{E}^{\hat{r}}(r_{*})d\hat{\theta} as a sign of energy extraction. The Kerr flux r^\mathcal{E}^{\hat{r}} takes the role of the Poynting vector in the lab frame of the toy model of section 5.1. It can be energy extracting even if the NHEK flux, analogous to the Poynting vector in the rotating frame of the toy model, is not. To analyze this statement, we will also consider the NHEK flux as measured by a stationary asymptotic observer (1,0,0,0)(1,0,0,0) in the NHEK frame, Ttr-T^{r}_{\phantom{r}t}, and the corresponding extracted energy at the boundary of NHEK

ENH=limrΣrTtr𝑑Σr,\displaystyle E_{NH}=-\lim_{r\rightarrow\infty}\int_{\Sigma_{r}}T^{r}_{\phantom{r}t}\,d\Sigma_{r}, (6.1)

with dΣr=gdtdϕdθd\Sigma_{r}=\sqrt{-g}\,dt\wedge d\phi\wedge d\theta. This is the object considered in Lupsasca:2014pfa to discuss energy extraction444 To compare to their notation, limrTtrdΣr\lim_{r\rightarrow\infty}T^{r}_{\phantom{r}t}\,d\Sigma_{r} becomes their =hn(r)νTανχ(t)α|r\mathcal{E}_{\infty}=\sqrt{-h}\,n^{\nu}_{(r)}T_{\alpha\nu}\,\chi^{\alpha}_{(t)}|_{r\rightarrow\infty} (with χ=t\chi=\partial_{t} and nn the normal to Σr\Sigma_{r}). It is pointed out in their footnote 2 that the NHEK and Kerr energies differ because of the mixing with angular momentum. . It is to be compared to the energy (5.35), rewritten using equation (5.28) as

E=limζ0Σr(ζTtr(r)12MTϕr(r))𝑑Σr,\displaystyle E=-\lim_{\zeta\rightarrow 0}\int_{\Sigma_{r}}\left(\zeta T^{r}_{\phantom{\mu}t}(r_{*})-\frac{1}{2M}T^{r}_{\phantom{\mu}\phi}(r_{*})\right)\,d\Sigma_{r}\,, (6.2)

where now we explicitly wrote the limit ζ0\zeta\rightarrow 0 that was implicit in equation (5.35), and r=1/(2Mζ)r_{*}=1/(2M\zeta). The AdS version of this expression is immediate from (5.39):

E=limϵ0Σr(ϵr0Ttr(r)ΩHextTϕr(r))𝑑Σr,\displaystyle E=-\lim_{\epsilon\rightarrow 0}\int_{\Sigma_{r}}\left(\frac{\epsilon}{r_{0}}T^{r}_{\phantom{\mu}t}(r_{*})-\Omega_{H}^{ext}T^{r}_{\phantom{\mu}\phi}(r_{*})\right)\,d\Sigma_{r}\,, (6.3)

with r=r0ΩHext/(kϵ)r_{*}=r_{0}\Omega_{H}^{ext}/(k\epsilon).

For the scaling solutions (both in NHEK and AdS-NHEK), the scaling of the relevant stress tensor components is Ttrr2h+2T^{r}_{\phantom{r}t}\sim r^{2h+2} and Tϕrr2h+1T^{r}_{\phantom{r}\phi}\sim r^{2h+1}. It follows that the extracted energy (6.2) scales like

Elimζ0 2πΔtr2h+1\displaystyle E\sim\lim_{\zeta\rightarrow 0}\,2\pi\Delta t\,\,r_{*}^{2h+1} (6.4)

where we used the NHEK notation, but the same conclusion will apply to the AdS-NHEK case. The NHEK energy flux rate E/ΔtE/\Delta t for the scaling solution will thus be finite only for the special value h=12h=-\frac{1}{2}. This special value was also pointed out in Lupsasca:2014pfa 555 Our hh differs from the one in Lupsasca:2014pfa by a sign. . However, from the point of view of the Kerr frame, the energy flux is measured in units of Kerr time t^=t/ζ\hat{t}=t/\zeta,

Elimζ0 2πΔt^r2h\displaystyle E\sim\lim_{\zeta\rightarrow 0}\,2\pi\Delta\hat{t}\,\,r_{*}^{2h} (6.5)

and the Kerr energy flux rate E/Δt^E/\Delta\hat{t} is finite for h=0h=0. This motivates the study of the log ansatz discussed in section 4.1.2. Indeed the log ansatz allows for a finite energy outflux in this sense: it has Ttrr2T^{r}_{\phantom{r}t}\sim r^{2} and TϕrrT^{r}_{\phantom{r}\phi}\sim r or r^\mathcal{E}^{\hat{r}} finite.

We discuss now in detail the h=1h=1 scaling solutions in NHEK and AdS-NHEK. They have infinite energy outflux.

The h=1h=1 scaling solution in NHEK was previously discussed in Zhang:2014pla (and Lupsasca:2014hua ). We repeat it here in our notation before we present the new solutions: the AdS-NHEK h=1h=1 scaling solution and an SE-NHEK log solution.

Scaling solution in NHEK
Refer to caption
Refer to caption
Figure 2: Solution Φ(θ)\Phi(\theta) and corresponding Poynting flux PrP^{r} as a function of θ\theta, for the energy extracting NHEK scaling solution for parameter values ω0=1,h=1,I0=0.1\omega_{0}=-1,h=1,I_{0}=0.1 and ΩHext=12M=0.5\Omega_{H}^{ext}=\frac{1}{2M}=0.5, and with Φ(π/2)=1.44774\Phi(\pi/2)=1.44774. This reproduces the solution of Zhang:2014pla (up to a sign disagreement). The Kerr flux is smaller than the NHEK flux.

For the scaling ansatz in section 4.1.1, we find NHEK and Kerr stress tensor components

Ttr=ω0I0r2h+2Φ(θ)1+2/hΦ(θ)4M4Γ(θ)2Λ(θ),Tϕr=TtrωF=Ttrrω0Φ1/h\displaystyle T^{r}_{\phantom{r}t}=\frac{\omega_{0}I_{0}r^{2h+2}\Phi(\theta)^{1+2/h}\Phi^{\prime}(\theta)}{4M^{4}\Gamma(\theta)^{2}\Lambda(\theta)},\qquad-T^{r}_{\phantom{r}\phi}=\frac{T^{r}_{\phantom{r}t}}{\omega_{F}}=\frac{T^{r}_{\phantom{r}t}}{r\omega_{0}\Phi^{1/h}} (6.6)

and

r^=2M2ζ(ζTtr12MTϕr)=I0r2h+1ζΦ(θ)1+1/h(1+2ω0MrζΦ(θ)1/h)Φ(θ)4M3Γ(θ)2Λ(θ).\displaystyle\mathcal{E}^{\hat{r}}=-2M^{2}\zeta\left(\zeta T^{r}_{\phantom{\mu}t}-\frac{1}{2M}T^{r}_{\phantom{\mu}\phi}\right)=\frac{I_{0}r^{2h+1}\zeta\Phi(\theta)^{1+1/h}\left(1+2\omega_{0}Mr\zeta\Phi(\theta)^{1/h}\right)\Phi^{\prime}(\theta)}{4M^{3}\Gamma(\theta)^{2}\Lambda(\theta)}\,. (6.7)

The first plot in Figure 2 shows the numerically obtained solution Φ(θ)\Phi(\theta) of the EOM (4.9) for h=1h=1. It satisfies the boundary conditions (4.13) and (4.14). What is plotted in the second figure is the infinite energy flux rate r^(r)\mathcal{E}^{\hat{r}}(r_{*}) rescaled by a power of ζ\zeta to extract the θ\theta-profile of the Poynting flux,

Pr=ζ2hr^(r),r=12Mζ.\displaystyle P^{r}=\zeta^{2h}\mathcal{E}^{\hat{r}}(r_{*}),\qquad r_{*}=\frac{1}{2M\zeta}\,. (6.8)

This Kerr outflux is compared in the third plot to the (infinite) NHEK outflux rescaled to the finite

PNHEKr=ζ2h+2Ttr(r),r=12Mζ.\displaystyle P^{r}_{NHEK}=-\zeta^{2h+2}T^{r}_{\phantom{r}t}(r_{*}),\qquad r_{*}=\frac{1}{2M\zeta}\,. (6.9)

Both profiles have a positive integral over θ\theta, i.e. both EE and ENHE_{NH} are positive, and the extracted energy ENHE_{NH} is actually greater than EE in this case.

This solution was first presented in Zhang:2014pla . The Poynting flux considered in Zhang:2014pla is the one observed by a ZAMO uμ=2Γ(θ)M(r,0,0,0)u_{\mu}=-\sqrt{2\Gamma(\theta)}M(r,0,0,0) in the NHEK frame, using the general definitions (D.1)-(D.3). The radial component for the Poynting flux (D.4) equals Tρruρ-T^{r}_{\phantom{r}\rho}u^{\rho}. It was discussed in the paragraph around equation (5.37) to produce the same energy outflux profile as we find for r^(r)\mathcal{E}^{\hat{r}}(r_{*}).

Scaling solution in AdS-NHEK
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Figure 3: Solution Φ(θ)\Phi(\theta) and corresponding Poynting flux PrP^{r} as a function of θ\theta, for the AdS-NHEK scaling solution for parameter values h=1,I0=0.2h=1,I_{0}=0.2, =1,a=0.25,k=0.68,ω0=12,r+=0.226654\ell=1,a=-0.25,k=-0.68,\omega_{0}=\frac{1}{2},r_{+}=0.226654 and ΩHext=2.06\Omega_{H}^{ext}=-2.06, and with Φ(π/2)=1.585633\Phi(\pi/2)=1.585633. The near horizon flux PAdSNHEKrP^{r}_{AdS-NHEK} is inwards while PrP^{r} does detect energy extraction.

For the AdS-NHEK scaling solution, we find the following AdS-NHEK and AdS-Kerr mixed stress tensor components

Ttr=ω0I0r2h+2Φ(θ)1+2/hΦ(θ)α(θ)γ(θ)Γ(θ)2,Tϕr=TtrωF=Ttrrω0Φ1/h\displaystyle T^{r}_{\phantom{r}t}=\frac{\omega_{0}I_{0}r^{2h+2}\Phi(\theta)^{1+2/h}\Phi^{\prime}(\theta)}{\alpha(\theta)\gamma(\theta)\Gamma(\theta)^{2}},\qquad-T^{r}_{\phantom{r}\phi}=\frac{T^{r}_{\phantom{r}t}}{\omega_{F}}=\frac{T^{r}_{\phantom{r}t}}{r\omega_{0}\Phi^{1/h}} (6.10)

and

r^=ϵr0(ϵr0TtrΩHextTϕr)=I0r2h+1ϵΦ(θ)1+1/h(r0ΩHext+ω0rϵΦ(θ)1/h)Φ(θ)α(θ)γ(θ)Γ(θ)2.\displaystyle\mathcal{E}^{\hat{r}}=-\epsilon r_{0}\left(\frac{\epsilon}{r_{0}}T^{r}_{\phantom{\mu}t}-\Omega_{H}^{ext}T^{r}_{\phantom{\mu}\phi}\right)=\frac{I_{0}r^{2h+1}\epsilon\Phi(\theta)^{1+1/h}\left(r_{0}\Omega_{H}^{ext}+\omega_{0}\,r\epsilon\Phi(\theta)^{1/h}\right)\Phi^{\prime}(\theta)}{\alpha(\theta)\gamma(\theta)\Gamma(\theta)^{2}}\,. (6.11)

Figure 3 shows the numerical function Φ(θ)\Phi(\theta) obtained for h=1h=1, which solves EOM (4.11) with boundary conditions (4.13)-(4.14). Further, the θ\theta-profile of the Poynting flux, again appropriately rescaled to

Pr=ϵ2hr^(r),r=r0ΩHextkϵ\displaystyle P^{r}=\epsilon^{2h}\mathcal{E}^{\hat{r}}(r_{*}),\qquad r_{*}=\frac{r_{0}\Omega_{H}^{ext}}{k\epsilon} (6.12)

is compared to the rescaled AdS-NHEK outflux

PAdSNHEKr=ϵ2h+2Ttr(r),r=r0ΩHextkϵ.\displaystyle P^{r}_{AdS-NHEK}=-\epsilon^{2h+2}T^{r}_{\phantom{r}t}(r_{*}),\qquad r_{*}=\frac{r_{0}\Omega_{H}^{ext}}{k\epsilon}\,. (6.13)

In this case we observe an inwards AdS-NHEK flux (ENH<0E_{NH}<0) but an outwards flux in AdS-Kerr (E>0E>0). This is reminiscent of the toy model, and provides an example where it matters to describe the energy extraction from the point of view of a Kerr rather than a near-horizon observer.

Log solution in SE-NHEK

While we have not succeeded in finding a log solution in (AdS-)NHEK with the boundary condition Φ0\Phi\rightarrow 0 at θ0\theta\rightarrow 0, we do present such a solution in SE-NHEK.

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Figure 4: Solution Φ(θ)\Phi(\theta) and corresponding Poynting flux PrP^{r} as a function of θ\theta, for the SE-NHEK log solution with parameter values =1,I0=0.9,ω0=0.5\ell=1,I_{0}=0.9,\omega_{0}=0.5 and ΩHext=3/4\Omega_{H}^{ext}=3/4, and with Φ(π/2)=0.68\Phi(\pi/2)=-0.68. The last figure shows the flux measured by a non-rotating SE-NHEK observer.

Figure 4 shows the numerically obtained Φ(θ)\Phi(\theta) for the specified set of parameter values. The plotted Φ(θ)\Phi(\theta) solves the EOM (4.12) with boundary conditions (4.13)-(4.14). The mixed stress tensor components

Ttr=I0r2Φ(θ)Φ(θ)α(θ)γ(θ)Γ(θ)2,Tϕr=TtrωF=Ttrrω0Φ(θ),\displaystyle T^{r}_{\phantom{r}t}=\frac{I_{0}\,r^{2}\Phi(\theta)\Phi^{\prime}(\theta)}{\alpha(\theta)\gamma(\theta)\Gamma(\theta)^{2}},\qquad-T^{r}_{\phantom{r}\phi}=\frac{T^{r}_{\phantom{r}t}}{\omega_{F}}=\frac{T^{r}_{\phantom{r}t}}{r\omega_{0}\Phi(\theta)}\,, (6.14)

and

r^=ϵr0(ϵr0TtrΩHextTϕr)=I0rϵ(r0ΩHext+rϵω0Φ(θ))Φ(θ)ω0α(θ)γ(θ)Γ(θ)2\displaystyle\mathcal{E}^{\hat{r}}=-\epsilon r_{0}\left(\frac{\epsilon}{r_{0}}T^{r}_{\phantom{\mu}t}-\Omega_{H}^{ext}T^{r}_{\phantom{\mu}\phi}\right)=\frac{I_{0}r\epsilon\left(r_{0}\Omega_{H}^{ext}+r\epsilon\,\omega_{0}\Phi(\theta)\right)\Phi^{\prime}(\theta)}{\omega_{0}\alpha(\theta)\gamma(\theta)\Gamma(\theta)^{2}} (6.15)

are such that the AdS-Kerr flux rate r^(r)\mathcal{E}^{\hat{r}}(r_{*}) is finite. It is shown in Figure 4 with the notation

Pr=r^(r),r=r0ΩHextkϵ,\displaystyle P^{r}=\mathcal{E}^{\hat{r}}(r_{*}),\qquad r_{*}=\frac{r_{0}\Omega_{H}^{ext}}{k\epsilon}\,, (6.16)

along with the (rescaled) SE-NHEK outflux

PSENHEKr=ϵ2Ttr(r),r=r0ΩHextkϵ.\displaystyle P^{r}_{SE-NHEK}=-\epsilon^{2}T^{r}_{\phantom{r}t}(r_{*}),\qquad r_{*}=\frac{r_{0}\Omega_{H}^{ext}}{k\epsilon}\,. (6.17)

The SE-NHEK flux is again inwards while the AdS-Kerr flux is outwards.

In the scaling solutions, the boundary condition Φ0\Phi\rightarrow 0 at θ0\theta\rightarrow 0 gives rise to a fine-tuning of the field strength to a finite value at the north pole. For the log solution this is not the case: even though Φ0\Phi\rightarrow 0, the field strength squared FμνFμνF_{\mu\nu}F^{\mu\nu} diverges at θ0\theta\rightarrow 0 (so does the angular component of the Poynting vector, while PrP^{r} is finite). This unphysical feature of the solution might be allowed because of the special geometry of SE-NHEK near the north pole, but this remains unclear.

Discussion of energy fluxes

The energy outfluxes PrP^{r} in Figures 2-4 all have the property that they change sign at the special value of θ\theta where the field angular velocity ωF\omega_{F} equals the angular velocity Ω\Omega of the geometry. This is consistent with equation (5.48). The corresponding critical value θc\theta_{c} is determined from the condition ω0Φ(θc)=1\omega_{0}\Phi(\theta_{c})=-1 for NHEK, and ω0Φ(θc)=k\omega_{0}\Phi(\theta_{c})=-k for AdS/SE-NHEK. The toy model, with constant ωF\omega_{F} and ΩH\Omega_{H}, has a flux of definite sign and thus no analogue of θc\theta_{c}.

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Figure 5: Polar vector plots of the (ZAMO) Poynting flux stream lines for the NHEK, AdS-NHEK and SE-NHEK solution, in the (r,θ)(r,\theta) plane of the near horizon geometry. The flux changes sign at the critical angle θc\theta_{c} (blue dashed lines). The density plot shows the magnitude of the radial Poynting flux ranging from negative (purple) over zero (yellow) to positive (red). Along the flux lines, the angular velocity ωF\omega_{F} is constant (white solid lines) in agreement with the conducting cylinder toy model.

Let us provide a different visualization of the solutions through vector plots of the flux in the (r,θ)(r,\theta) plane of the geometry. Figure 5 shows, for each of the solutions, the streamlines of the vector field (Px,Py)(P^{x},P^{y}), with (Px,Py)=(PrcosθrPθsinθ,rPθcosθ+Prsinθ)(P^{x},P^{y})=\left(P^{r}\cos\theta-rP^{\theta}\sin\theta,rP^{\theta}\cos\theta+P^{r}\sin\theta\right) in a polar vector plot, with x=rcosθx=r\cos\theta, y=rsinθy=r\sin\theta. The Poynting flux PμP^{\mu} that is used to obtain these figures is the conserved energy flux measured by the rotating observer (ZAMO) in (5.37) and (5.44). The result for the vector plots is qualitatively similar to the result one would obtain from using the conserved energy flux μ^(r,θ;λ)\mathcal{E}^{\hat{\mu}}(r,\theta;\lambda) with λ(r)\lambda(r_{*}) replaced by λ(r)\lambda(r). The magnitude of the radial flux PrP^{r} is superimposed as a density plot with color-coding: negative (purple) over zero (yellow) to positive (red). The first quadrant of each plot in Figure 5 corresponds to the range (θ[0,π/2]\theta\in[0,\pi/2]) of Figures 2-4. When the solution is extended by symmetry to the full angular range θ[0,2π]\theta\in[0,2\pi], the net energy outflux obtained by integrating the Poynting flux over the full range vanishes by energy conservation. To determine a non-trivial power output, we therefore consider the near horizon black hole regions embedded into an externally imposed split-monopolar magnetic field sourced by toroidal currents in a razor-thin disk at the equator Blandford:1977ds . This magnetic field is given by the solution in the northern hemisphere which is mirrored into the southern hemisphere. All the solutions we found for near-horizon black holes threaded by a split monopole magnetic field have net positive energy outflux. The AdS- and SE-NHEK solution bring in energy at the equator and emit energy near the poles. The NHEK solution has net positive energy outflux near the equator. Figure 6 shows the same information as Figure 5, but in Kerr coordinates.

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Figure 6: Polar vector plots of the Poynting flux stream lines for the NHEK, AdS-NHEK and SE-NHEK solution, in the (r^,θ^)(\hat{r},\hat{\theta}) plane of (AdS/SE-)Kerr. Only the first quadrant is shown. In NHEK and AdS-NHEK, the location where the flux changes sign (purple line) corresponds at the equator to the start of the Kerr ‘ergoregion’ as determined by the NHEK observer, which is the orange shaded region bounded by the gray dashed line. The region behind the horizon is shaded in black.

7 Discussion and outlook

We have presented symmetric FFE solutions in two different near horizon geometries of AdS-Kerr. They have the property that an observer at rest in the near horizon metric measures an energy influx, while a rotating observer – corresponding to an observer at rest in the Kerr region – measures an energy outflux. This behavior is consistent with the simple toy model set-up of a rotating conducting cylinder in Figure 1, which shows that the angular flux contribution can be large enough to change the sign of net energy flux. The solutions have non-negative FμνFμν2(B2E2)F_{\mu\nu}F^{\mu\nu}\equiv 2(B^{2}-E^{2}), and therefore correspond to magnetically dominated plasmas. This is required to avoid superluminal motion of the plasma. That said, both solutions still display an unphysical feature. The AdS-NHEK solution has an infinite energy outflux at the boundary of NHEK, similar to the NHEK scaling solution of Zhang:2014pla . The SE-NHEK solution has diverging field strength near the north pole. However, as the north pole is effectively removed from the SE-NHEK geometry, this drawback might actually be irrelevant.

We have shown the log ansatz can be used to produce an FFE solution with finite energy outflux. It would be interesting to extend this to other near-horizon geometries, most notably the original NHEK metric, which is most relevant for astrophysics. Perhaps another set of physical boundary conditions than the ones used in this paper can be used.

The energy-extracting solutions presented in this paper require the presence of plasma, as in the usual BZ process. It could be investigated whether solutions describing a plasma-less version of the BZ process, as obtained in Jacobson:2017xam for BTZ, also appear in the context of AdS-Kerr.

The use of AdS geometries in this paper suggests the question whether an AdS/CFT interpretation of our FFE solutions exists, in the spirit of Jacobson:2017xam ; Hawking:1998kw . Since the AdS-Kerr solution is only known in our case in the near-horizon region, the only AdS factor that is available to us for such an AdS/CFT interpretation is the warped (at constant θ\theta) AdS3 factor that makes up the 4D (AdS-)NHEK geometry. This is the AdS space that gives rise to the conjectured Kerr/CFT correspondence of Guica:2008mu . However, an immediate repetition of the strategy in Jacobson:2017xam for the calculation of a dual CFT conductivity would require the presence of an EM field strength component FtϕF_{t\phi}, which is missing by construction in the toroidally invariant solutions we presented. We leave these open questions for future work.

Acknowledgements

We want to thank Elizabeth Tolman for early collaboration on this project. Part of this work was conducted at the ‘First USU Strings and Black Holes Workshop’, which was supported by the Department of Physics and the DGCAMP group at Utah State University. The work of MJR is partially supported through the NSF grant PHY-1707571, SEV-2016-0597 and PGC2018-095976-B-C21 from MCIU/AEI/FEDER, UE. The work of N.C. is supported by the Israel Science Foundation under grant 447/17. The research of H.V. is supported by NSF grant PHY-1620059.

Appendix A Kerr black holes and their near horizons

We summarize in this appendix how to take the near horizon limits of various Kerr black holes. More details can be found e.g. in the review Compere:2012jk .

Near horizon Extreme Kerr black hole: NHEK

In Boyer-Lindquist coordinates, the Kerr solution, parametrized by the angular momentum per mass aa and mass MM, is

ds2=(12Mr^Σ)dt^24Mar^sin2θ^Σdt^dϕ^+ΣΔdr^2+Σdθ2+Asin2θ^Σdϕ^2\displaystyle ds^{2}=-\left(1-\frac{2M{\hat{r}}}{\Sigma}\right)d{\hat{t}}^{2}-\frac{4Ma{\hat{r}}\sin^{2}{\hat{\theta}}}{\Sigma}d{\hat{t}}\,d{\hat{\phi}}+\frac{\Sigma}{\Delta}d{\hat{r}}^{2}+\Sigma\,d{\theta}^{2}+\frac{A\sin^{2}{\hat{\theta}}}{\Sigma}d{\hat{\phi}}^{2}\, (A.1)

where Σ=r^2+a2cos2θ^\Sigma={\hat{r}}^{2}+a^{2}\cos^{2}{\hat{\theta}}, Δ=r^22Mr^+a2\Delta={\hat{r}}^{2}-2M{\hat{r}}+a^{2} and A=(r^2+a2)2Δa2sin2θ^A=({\hat{r}}^{2}+a^{2})^{2}-\Delta\,a^{2}\sin^{2}{\hat{\theta}}. The determinant of the metric is g=Σsinθ^\sqrt{-g}=\Sigma\sin\hat{\theta}. The roots of Δ=0\Delta=0 are the black hole inner and outer event horizons r±=M±M2a2r_{\pm}=M\pm\sqrt{M^{2}-a^{2}}. The Kerr black hole is stationary, axisymmetric and asymptotically flat. It has an angular velocity Ωgt^ϕ^/gϕ^ϕ^=2Mar^/A\Omega\equiv-g_{\hat{t}\hat{\phi}}/g_{\hat{\phi}\hat{\phi}}=2Ma\hat{r}/A that vanishes asymptotically. The angular velocity at the outer horizon is ΩHΩ(r+)=a/(r+2+a2)\Omega_{H}\equiv\Omega(r_{+})=a/(r_{+}^{2}+a^{2}).

Extremal Kerr (a=Ma=M) has coinciding horizons r+=r=Mr_{+}=r_{-}=M and horizon angular velocity

ΩHext=12M.\displaystyle\Omega_{H}^{ext}=\frac{1}{2M}\,. (A.2)

The so-called Near Horizon of Extreme Kerr (NHEK) geometry can be thought of as a zoom in on the near horizon region r=r+r=r_{+} of the black hole. Following Bardeen:1999px , the NHEK metric (3.2) can be obtained from the extremal Kerr black hole geometry (A.1) in Boyer-Lindquist coordinates (t^,r^,θ^,ϕ^)(\hat{t},\hat{r},\hat{\theta},\hat{\phi}) by defining new coordinates

t^tζ,ϕ^ϕ+t2Mζ,r^2M2ζr+M,θ^θ\displaystyle\hat{t}\rightarrow\frac{t}{\zeta},\qquad\hat{\phi}\rightarrow\phi+\frac{t}{2M\zeta},\qquad\hat{r}\rightarrow 2M^{2}\zeta r+M,\qquad\hat{\theta}\rightarrow\theta (A.3)

and taking the limit ζ0\zeta\rightarrow 0. The location of the horizon is at r=0r=0 in these coordinates. From the relation ϕ=ϕ^12Mt^\phi=\hat{\phi}-\frac{1}{2M}\hat{t} between the new angle ϕ\phi and the Kerr angle ϕ^\hat{\phi}, it is clear that the NHEK geometry co-rotates with extremal Kerr at the angular velocity of the horizon (A.2). The scale parameter ζ\zeta can be rescaled without changing the resulting near horizon metric. This points to an extra scaling symmetry of the NHEK geometry under rλrr\rightarrow\lambda r and tt/λt\rightarrow t/\lambda. It is discussed in more detail in section 3.1.1.

Near horizon extreme AdS-Kerr black hole: AdS-NHEK

In this section and the next we discuss two types of near horizon geometries that follow from two types of extremal limits of the AdS-Kerr black hole (in Boyer-Lindquist coordinates)

ds2=ΔaΣa(dt^asin2θ^Ξdϕ^)2+ΣaΔadr^2+ΣaΔθdθ^2+Δθsin2θ^Σa(adt^r^2+a2Ξdϕ^)2\displaystyle ds^{2}=-\frac{\Delta_{a}}{\Sigma_{a}}\left(d\hat{t}-\frac{a\sin^{2}\hat{\theta}}{\Xi}\,d\hat{\phi}\right)^{2}+\frac{\Sigma_{a}}{\Delta_{a}}\,d\hat{r}^{2}+\frac{\Sigma_{a}}{\Delta_{\theta}}\,d\hat{\theta}^{2}+\frac{\Delta_{\theta}\sin^{2}\hat{\theta}}{\Sigma_{a}}\left(a\,d\hat{t}-\frac{\hat{r}^{2}+a^{2}}{\Xi}\,d\hat{\phi}\right)^{2} (A.4)

where

Δa=(r^2+a2)(1+r^2/l2)2mr^Ξ=1a2/l2,\displaystyle\Delta_{a}=(\hat{r}^{2}+a^{2})(1+\hat{r}^{2}/l^{2})-2m\hat{r}\,\qquad\Xi=1-a^{2}/l^{2}\,, (A.5)
Δθ=1a2cos2θ^/l2Σa=r^2+a2cos2θ^.\displaystyle\Delta_{\theta}=1-a^{2}\cos^{2}\hat{\theta}/l^{2}\,\qquad\Sigma_{a}=\hat{r}^{2}+a^{2}\cos^{2}\hat{\theta}\,. (A.6)

In one case we take the traditional extreme limit where the inner and outer horizons degenerate to a single horizon at r^=r+=r\hat{r}=r_{+}=r_{-}. In the other case we will take the so called super-entropic limit ala\rightarrow l while also fixing the mass m=8l/33m=8\,l/3\sqrt{3} for the black hole to be extreme. More details on these two different prescriptions are described next.

The outer and inner horizon of AdS-Kerr are defined as the largest and smallest root of Δa\Delta_{a} (which allows to eliminate mm for r±r_{\pm}). As it was shown in Hartman:2008pb ; Compere:2012jk , to find the near horizon geometry of the extreme AdS-Kerr black hole (3.1) one has to first find the extreme limit of (A.4)(\ref{KerrAds}) where the inner and outer horizons degenerate r=r+=rr=r_{+}=r_{-}, then introduce new coordinates

t^tr0ϵ,ϕ^ϕ+ΩHexttr0ϵ,r^r++ϵr0r,θ^θ,\displaystyle\hat{t}\rightarrow t\frac{r_{0}}{\epsilon},\qquad\hat{\phi}\rightarrow\phi+\Omega_{H}^{ext}\frac{t\,r_{0}}{\epsilon},\qquad\hat{r}\rightarrow r_{+}+\epsilon\,r_{0}\,r,\qquad\hat{\theta}\rightarrow\theta, (A.7)

with r0r_{0} and ΩHext\Omega_{H}^{ext} defined below, and finally take the limit ϵ0\epsilon\rightarrow 0.

The extremality condition a(r+)a(r_{+}) is given in (3.9)(\ref{eq:horizon}) and r0r_{0} is defined as

r02=(r+2+a2)Δ0,Δ0=1+a2l2+6r+2l2.\displaystyle r_{0}^{2}=\frac{(r_{+}^{2}+a^{2})}{\Delta_{0}}\,,\qquad\Delta_{0}=1+\frac{a^{2}}{l^{2}}+6\frac{r_{+}^{2}}{l^{2}}\,. (A.8)

The parameter ΩHext\Omega_{H}^{ext} is given by the AdS-Kerr angular velocity of the (outer) horizon

ΩHext=Ξar+2+a2,\displaystyle\qquad\Omega^{ext}_{H}=\frac{\Xi\,a}{r_{+}^{2}+a^{2}}\,, (A.9)

where the superscript refers to the angular velocity being evaluated at extremality (3.9)(\ref{eq:horizon}).

Near horizon of super-entropic AdS-Kerr black hole: SE-NHEK

A different extremal limit for the AdS-Kerr black hole has been studied in the super-entropic limit ala\rightarrow l in Hennigar:2015cja . Here we show how to derive the near horizon geometry of these super-entropic extremal black holes, as first discussed in Sinamuli:2015drn .

Following Hennigar:2015cja we first take the limit ala\rightarrow l, but at the same time to avoid a singularity in the metric rescale the coordinate ϕ^=ψ^Ξ\hat{\phi}=\hat{\psi}\,\Xi and identify ψ^\hat{\psi} with period 2π/Ξ2\pi/\Xi to prevent conical singularities. The black hole (A.4) in this limit is super-entropic (see Cvetic:2010jb for details) and becomes

ds2=ΔlΣl(dt^lsin2θ^dψ^)2+ΣlΔldr^2+Σlsin2θ^dθ^2+sin4θ^Σl(ldt^(r^2+l2)dψ^)2\displaystyle ds^{2}=-\frac{\Delta_{l}}{\Sigma_{l}}\left(d\hat{t}-{l\sin^{2}\hat{\theta}}\,d\hat{\psi}\right)^{2}+\frac{\Sigma_{l}}{\Delta_{l}}\,d\hat{r}^{2}+\frac{\Sigma_{l}}{\sin^{2}\hat{\theta}}\,d\hat{\theta}^{2}+\frac{\sin^{4}\hat{\theta}}{\Sigma_{l}}\left(l\,d\hat{t}-(\hat{r}^{2}+l^{2})\,d\hat{\psi}\right)^{2} (A.10)

where

Δl=(r^2+l2)(1+r^2/l2)2mr^Σl=r^2+l2cos2θ^.\displaystyle\Delta_{l}=(\hat{r}^{2}+l^{2})(1+\hat{r}^{2}/l^{2})-2m\hat{r}\,\qquad\Sigma_{l}=\hat{r}^{2}+l^{2}\cos^{2}\hat{\theta}\,. (A.11)

The coordinate ψ^\hat{\psi} is non-compact and hence we choose to compactify it by ψ^ψ^+2π\hat{\psi}\sim\hat{\psi}+2\pi. The black hole event horizon topology is that of a sphere with two punctures (at the poles) and for horizons to exist there is a minimal extremal value of the mass mml=8l/(33)m\equiv m_{l}=8\,l/(3\sqrt{3}). Note that now there are only three roots of Δl|m=ml=0\Delta_{l}|_{m=m_{l}}=0 located at r={l/3,(1±22i)l/3}r=\{l/\sqrt{3},(-1\pm 2\sqrt{2}i)\,l/\sqrt{3}\}. The event horizon is therefore located at

r+rl=l3.\displaystyle r_{+}\equiv r_{l}=\frac{l}{\sqrt{3}}. (A.12)

Now we derive the near horizon region r=rlr=r_{l} of these extreme super-entropic black holes, dubbed here SE-NHEK metric (3.1) with functions (3.12)(\ref{eq:SEdefd}). It can be obtained from the extremal m=mlm=m_{l} super-entropic AdS-Kerr black hole geometry (A.10) by defining new coordinates in the same way as in (A.7) but starting from the super-entropic black hole (A.10) with angle ψ^\hat{\psi}, namely

t^tr0ϵ,ψ^ϕ+ΩHexttr0ϵ,r^r++ϵr0r,θ^θ,\displaystyle\hat{t}\rightarrow t\frac{r_{0}}{\epsilon},\qquad\hat{\psi}\rightarrow\phi+\Omega_{H}^{ext}\frac{t\,r_{0}}{\epsilon},\qquad\hat{r}\rightarrow r_{+}+\epsilon\,r_{0}\,r,\qquad\hat{\theta}\rightarrow\theta, (A.13)

and taking the limit ϵ0\epsilon\rightarrow 0. Note that in this super-entropic extremal limit r0r_{0} defined in (A.8) equals r+r_{+}, i.e.

r0=l3,\displaystyle r_{0}=\frac{l}{\sqrt{3}}\,, (A.14)

and ΩHext\Omega_{H}^{ext} is given by the horizon angular velocity ΩHgt^ψ^/gψ^ψ^(r+)\Omega_{H}\equiv-g_{\hat{t}\hat{\psi}}/g_{\hat{\psi}\hat{\psi}}(r_{+}) of the geometry (A.10), evaluated at the extremal value of r+r_{+} in (A.12),

ΩHext=34l.\displaystyle\Omega_{H}^{ext}=\frac{3}{4l}\,. (A.15)

With these values filled in, the SE-NHEK limit (A.13) can be written out as

t^rlt/ϵ,ψ^ϕ+(3/4)t/ϵ,r^rl(1+ϵr),θ^θ.\displaystyle\hat{t}\rightarrow r_{l}\,t/\epsilon\,,\qquad\hat{\psi}\rightarrow\phi+(\sqrt{3}/4)\,t/\epsilon\,,\qquad\hat{r}\rightarrow r_{l}\,(1+\epsilon\,r)\,,\qquad\hat{\theta}\rightarrow\theta\,. (A.16)

It was shown in Sinamuli:2015drn that the super-entropic limit and the near-horizon limit of AdS-Kerr commute, i.e. the SE-NHEK metric can alternatively be obtained from a super-entropic limit of AdS-NHEK.

Near horizon of extremal BTZ: NHEBTZ

The BTZ black hole background metric Banados:1992wn , which is a three-dimensional solution of Einstein’s equations with a negative cosmological constant, is

ds2\displaystyle ds^{2} =α(r^)2dt^2+dr^2α(r^)2+r^2(dϕ^Ω(r^)dt^)2\displaystyle=-\alpha(\hat{r})^{2}d\hat{t}^{2}+\frac{d\hat{r}^{2}}{\alpha(\hat{r})^{2}}+\hat{r}^{2}(d\hat{\phi}-\Omega(\hat{r})d\hat{t})^{2} (A.17)

with

α(r^)=(r^2r+2)(r^2r2)r^2l2,Ω(r^)=rr+r^2l.\displaystyle\alpha(\hat{r})=\frac{(\hat{r}^{2}-r_{+}^{2})(\hat{r}^{2}-r_{-}^{2})}{\hat{r}^{2}l^{2}},\qquad\Omega(\hat{r})=\frac{r_{-}r_{+}}{\hat{r}^{2}l}. (A.18)

It has horizons r±r_{\pm} at the locations where α(r^)\alpha(\hat{r}) vanishes, and angular velocity Ω(r^)\Omega(\hat{r}). In the extremal limit, the inner and outer horizon coincide r+=rr_{+}=r_{-} and the horizon angular velocity becomes

ΩHext=1l.\displaystyle\Omega_{H}^{ext}=\frac{1}{l}\,. (A.19)

The near-horizon extreme BTZ geometry or NHEBTZ geometry (3.13) can be obtained from the coordinate transformation (see e.g. deBoer:2010ac )

t^=tϵ,ϕ^=ϕ+tϵl,r^2=r+2+ϵr\displaystyle\hat{t}=\frac{t}{\epsilon},\qquad\hat{\phi}=\phi+\frac{t}{\epsilon l},\qquad\hat{r}^{2}=r_{+}^{2}+\epsilon r (A.20)

in the limit ϵ0\epsilon\rightarrow 0.

Appendix B Stream equations in near-horizon regions

For the NHEK metric (3.1) with (3.2), the action in (2.25) becomes

𝒮[Aϕ]=𝑑r𝑑θ[d2(r2(rAϕ)2+(θAϕ)2)+12r2ΛI(Aϕ)2]d𝒞r=Λ(ωFr+1)21Λ\displaystyle\begin{split}\mathcal{S}[A_{\phi}]&=\int drd\theta\left[\frac{d}{2}\left(r^{2}(\partial_{r}A_{\phi})^{2}+(\partial_{\theta}A_{\phi})^{2}\right)+\frac{1}{2r^{2}\Lambda}I(A_{\phi})^{2}\right]\\ &\qquad\qquad d\equiv-\frac{\mathcal{C}}{r}=\Lambda(\frac{\omega_{F}}{r}+1)^{2}-\frac{1}{\Lambda}\end{split} (B.1)

or alternatively, using (2.18),

𝒮[At]=drdθr2[D2(r2(rAt)2+(θAt)2)+12ΛI(At)2]DrωF2𝒞=Λ(1+rωF)21Λr2ωF2.\displaystyle\begin{split}\mathcal{S}[A_{t}]&=\int\frac{drd\theta}{r^{2}}\left[\frac{D}{2}\left(r^{2}(\partial_{r}A_{t})^{2}+(\partial_{\theta}A_{t})^{2}\right)+\frac{1}{2\Lambda}I(A_{t})^{2}\right]\\ &\qquad\qquad D\equiv-\frac{r}{\omega_{F}^{2}}\mathcal{C}=\Lambda\left(1+\frac{r}{\omega_{F}}\right)^{2}-\frac{1}{\Lambda}\frac{r^{2}}{\omega_{F}^{2}}.\end{split} (B.2)

From these actions we obtain respectively the NHEK EOM for AϕA_{\phi},

θ(dθAϕ)+r(dr2rAϕ)12δdδAϕ(r2(rAϕ)2+(θAϕ)2)1r2ΛIδIδAϕ=0,\displaystyle\partial_{\theta}(d\,\partial_{\theta}A_{\phi})+\partial_{r}(d\,r^{2}\partial_{r}A_{\phi})-\frac{1}{2}\frac{\delta d}{\delta A_{\phi}}\left(r^{2}(\partial_{r}A_{\phi})^{2}+(\partial_{\theta}A_{\phi})^{2}\right)-\frac{1}{r^{2}\Lambda}I\frac{\delta I}{\delta A_{\phi}}=0, (B.3)

and the one for AtA_{t},

θ(Dr2θAt)+r(DrAt)12δDδAt((rAt)2+1r2(θAt)2)1r2ΛIδIδAt=0.\displaystyle\partial_{\theta}(\frac{D}{r^{2}}\partial_{\theta}A_{t})+\partial_{r}(D\partial_{r}A_{t})-\frac{1}{2}\frac{\delta D}{\delta A_{t}}\left((\partial_{r}A_{t})^{2}+\frac{1}{r^{2}}(\partial_{\theta}A_{t})^{2}\right)-\frac{1}{r^{2}\Lambda}I\frac{\delta I}{\delta A_{t}}=0. (B.4)

For an AdS-NHEK metric (3.1), with either (3.8) or (3.12), the action (2.25) is

𝒮[Aϕ]=𝑑r𝑑θ[dα2(r2(rAϕ)2+1α2(θAϕ)2)+α2r2γI(Aϕ)2]dααr𝒞=αγ(ωFr+k)2αγ\displaystyle\begin{split}\mathcal{S}[A_{\phi}]&=\int drd\theta\left[\frac{d_{\alpha}}{2}\left(r^{2}(\partial_{r}A_{\phi})^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}A_{\phi})^{2}\right)+\frac{\alpha}{2r^{2}\gamma}I(A_{\phi})^{2}\right]\\ &\qquad\qquad d_{\alpha}\equiv-\frac{\alpha}{r}\mathcal{C}=\alpha\gamma(\frac{\omega_{F}}{r}+k)^{2}-\frac{\alpha}{\gamma}\end{split} (B.5)

or

𝒮[At]=drdθr2[Dα2(r2(rAt)2+1α2(θAt)2)+α2γI(At)2]DααrωF2𝒞=γα(1+krωF)2αγr2ωF2.\displaystyle\begin{split}\mathcal{S}[A_{t}]&=\int\frac{drd\theta}{r^{2}}\left[\frac{D_{\alpha}}{2}\left(r^{2}(\partial_{r}A_{t})^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}A_{t})^{2}\right)+\frac{\alpha}{2\gamma}I(A_{t})^{2}\right]\\ &\qquad\qquad D_{\alpha}\equiv-\frac{\alpha r}{\omega_{F}^{2}}\mathcal{C}=\gamma\alpha\left(1+k\frac{r}{\omega_{F}}\right)^{2}-\frac{\alpha}{\gamma}\frac{r^{2}}{\omega_{F}^{2}}\,.\end{split} (B.6)

Variation of the action gives the AdS-NHEK EOM for AϕA_{\phi},

θ(dα1α2θAϕ)+r(dαr2rAϕ)12δdαδAϕ(r2(rAϕ)2+1α2(θAϕ)2)αr2γIδIδAϕ=0,\displaystyle\partial_{\theta}(d_{\alpha}\,\frac{1}{\alpha^{2}}\partial_{\theta}A_{\phi})+\partial_{r}(d_{\alpha}\,r^{2}\partial_{r}A_{\phi})-\frac{1}{2}\frac{\delta d_{\alpha}}{\delta A_{\phi}}\left(r^{2}(\partial_{r}A_{\phi})^{2}+\frac{1}{\alpha^{2}}(\partial_{\theta}A_{\phi})^{2}\right)-\frac{\alpha}{r^{2}\gamma}I\frac{\delta I}{\delta A_{\phi}}=0, (B.7)

and for AtA_{t},

θ(Dαr2α2θAt)+r(DαrAt)12δDαδAt((rAt)2+1r2α2(θAt)2)αr2γIδIδAt=0.\displaystyle\partial_{\theta}(\frac{D_{\alpha}}{r^{2}\alpha^{2}}\partial_{\theta}A_{t})+\partial_{r}(D_{\alpha}\partial_{r}A_{t})-\frac{1}{2}\frac{\delta D_{\alpha}}{\delta A_{t}}\left((\partial_{r}A_{t})^{2}+\frac{1}{r^{2}\alpha^{2}}(\partial_{\theta}A_{t})^{2}\right)-\frac{\alpha}{r^{2}\gamma}I\frac{\delta I}{\delta A_{t}}=0. (B.8)

Appendix C EM fields in different frames

We review the identification of EM fields in the EM tensor that allow the standard form of Maxwell’s equations to be obtained from the covariant expressions in terms of the field strength. Different frames are considered. In particular the relation between electromagnetic fields in rotating frames in (C.38) is useful for the description of the toy model in the main text.

Carthesian

In Carthesian coordinates in mostly plus convention, the standard definition

Fμν=(0ExEyEzEx0BzByEyBz0BxEzByBx0)\displaystyle F_{\mu\nu}=\left(\begin{array}[]{cccc}0&-E_{x}&-E_{y}&-E_{z}\\ E_{x}&0&B_{z}&-B_{y}\\ E_{y}&-B_{z}&0&B_{x}\\ E_{z}&B_{y}&-B_{x}&0\end{array}\right) (C.5)

(or Ei=Fi0E_{i}=F_{i0} and Bi=12ϵ0ijkFjkB_{i}=\frac{1}{2}\epsilon_{0ijk}F^{jk}, with ϵμναβ\epsilon_{{\mu\nu}\alpha\beta} the covariant permutation tensor of the spacetime) is easily shown to provide as equivalent formulations of Maxwell’s equations

νFμν=jμ{E=j0×B=Et+j\displaystyle\partial_{\nu}F^{\mu\nu}=j^{\mu}\qquad\qquad\left\{\begin{array}[]{ll}\nabla\cdot E=j^{0}\\ \nabla\times B=\frac{\partial E}{\partial t}+j\end{array}\right. (C.8)

and

νF~μν=0{B=0×E=Bt,\displaystyle\partial_{\nu}\tilde{F}^{\mu\nu}=0\qquad\qquad\left\{\begin{array}[]{ll}\nabla\cdot B=0\\ \nabla\times E=-\frac{\partial B}{\partial t}\end{array}\right., (C.11)

with

F~μν=12ϵμναβFαβ.\displaystyle\tilde{F}^{\mu\nu}=\frac{1}{2}\epsilon^{{\mu\nu}\alpha\beta}F_{\alpha\beta}. (C.12)

The electromagnetic stress energy tensor is defined as

Tμν=FμαFνα14FαβFαβgμν\displaystyle T_{\mu\nu}=F_{\mu\alpha}F_{\nu}^{\phantom{\nu}\alpha}-\frac{1}{4}F_{\alpha\beta}F^{\alpha\beta}g_{\mu\nu} (C.13)

and related to the Poynting vector Pi=(E×B)i=ϵ0ijkEjBkP^{i}=(E\times B)^{i}=\epsilon_{0}^{\phantom{0}ijk}E_{j}B_{k} as

T0i=Pi.\displaystyle T^{i}_{\phantom{ii}0}=-P^{i}. (C.14)
Cylindrical

In cylindrical coordinates, we use

Fμν\displaystyle F_{\mu\nu} =(0ErEθEzEr0BzrBθ/rEθBzr0BrrEzBθ/rBrr0)\displaystyle=\left(\begin{array}[]{cccc}0&-E_{r}&-E_{\theta}&-E_{z}\\ E_{r}&0&B_{z}r&-B_{\theta}/r\\ E_{\theta}&-B_{z}r&0&B_{r}r\\ E_{z}&B_{\theta}/r&-B_{r}r&0\end{array}\right) (C.19)

to obtain the equivalent formulations

νFμν=jμ{E=j0×B=Et+j\displaystyle\nabla_{\nu}F^{\mu\nu}=j^{\mu}\qquad\qquad\left\{\begin{array}[]{ll}\nabla\cdot E=j^{0}\\ \nabla\times B=\frac{\partial E}{\partial t}+j\end{array}\right. (C.22)

and

νF~μν=0{B=0×E=Bt.\displaystyle\nabla_{\nu}\tilde{F}^{\mu\nu}=0\qquad\qquad\left\{\begin{array}[]{ll}\nabla\cdot B=0\\ \nabla\times E=-\frac{\partial B}{\partial t}\end{array}\right.. (C.25)

Here, μ\nabla_{\mu} is the covariant derivative in the metric

ds2=dt2+dr2+r2dθ2+dz2.\displaystyle ds^{2}=-dt^{2}+dr^{2}+r^{2}d\theta^{2}+dz^{2}. (C.26)

The field strength (C.19) can be obtained from the Carthesian expression (C.5) by the transformation FΛTFΛF\rightarrow\Lambda^{T}F\Lambda under the transformation from Carthesian coordinates xx to cylindrical coordinates xx^{\prime} with transformation matrix Λ=x/x\Lambda=\partial x/\partial x^{\prime}. The components of the electromagnetic fields are given by Ei=Fi0E_{i}=F_{i0} and Bi=12ϵ0ijkFjkB_{i}=\frac{1}{2}\epsilon_{0ijk}F^{jk}. In the alternative choice of basis eθgθθeθ\vec{e}_{\theta}\rightarrow\sqrt{g_{\theta\theta}}\vec{e}_{\theta} (or Eθ=Eθcyl/rE_{\theta}=E_{\theta}^{cyl}/r and Bθ=Bθcyl/rB_{\theta}=B_{\theta}^{cyl}/r), the form of Maxwell’s equations in curvilinear, cylindrical coordinates is recovered.

The same relation (C.14) holds for the Poynting flux defined as Pi=(E×B)i=ϵ0ijkEjBkP^{i}=(E\times B)^{i}=\epsilon_{0}^{\phantom{0}ijk}E_{j}B_{k},

P=(BzEθBθEzr,BrEzBzErr,BθErBrEθr).\displaystyle P=\left(\frac{B_{z}E_{\theta}-B_{\theta}E_{z}}{r},\frac{B_{r}E_{z}-B_{z}E_{r}}{r},\frac{B_{\theta}E_{r}-B_{r}E_{\theta}}{r}\right). (C.27)
Rotating frame

We can go from cylindrical coordinates xμ=(t,r,θ,z)=(t,r,θ+ωt,z)x^{\mu}=(t,r,\theta,z)=(t^{\prime},r^{\prime},\theta^{\prime}+\omega t^{\prime},z^{\prime}) to rotating cylindrical coordinates xμ=(t,r,θ,z)=(t,r,θωt,z)x^{\mu^{\prime}}=(t^{\prime},r^{\prime},\theta^{\prime},z^{\prime})=(t,r,\theta-\omega t,z), with metric ds2=dt2+dr2+r2dθ2+dz2ds^{2}=-dt^{2}+dr^{2}+r^{2}d\theta^{2}+dz^{2} transformed into the metric ds2=dt2+dr2+r2(dθ+ωdt)2+dz2ds^{\prime 2}=-dt^{\prime 2}+dr^{\prime 2}+r^{\prime 2}(d\theta^{\prime}+\omega dt^{\prime})^{2}+dz^{\prime 2} such that the primed frame rotates with angular velocity ω\omega counterclockwise about the zz axis. In the rotating frame in cylindrical coordinates (t,r,θ,z)(t^{\prime},r^{\prime},\theta^{\prime},z^{\prime}), the transformed field strength is then given by666 One goes between contravariant and covariant EM fields by Eθ=Eθ/r2E^{\theta}=E_{\theta}/r^{2} and Bθ=Bθ/r2B^{\theta}=B_{\theta}/r^{2}. Also, as remarked in the previous section on the cylindrical frame, we can use EθEθ/rE^{\theta}\rightarrow E^{\theta}/r, BθBθ/rB^{\theta}\rightarrow B^{\theta}/r to recover the curvilinear notation.

Frotμν\displaystyle F^{\mu^{\prime}\nu^{\prime}}_{rot} =(0ErEθ/r2EzEr0Bzrot/rBθrot/rEθ/r2Bzrot/r0Brrot/rEzBθrot/rBrrot/r0)\displaystyle=\left(\begin{array}[]{cccc}0&E_{r}&E_{\theta}/r^{2}&E_{z}\\ -E_{r}&0&B_{z}^{rot}/r&-B_{\theta}^{rot}/r\\ -E_{\theta}/r^{2}&-B_{z}^{rot}/r&0&B_{r}^{rot}/r\\ -E_{z}&B_{\theta}^{rot}/r&-B_{r}^{rot}/r&0\end{array}\right) (C.32)

and

Fμνrot\displaystyle F_{\mu^{\prime}\nu^{\prime}}^{rot} =(0ErrotEθrotEzrotErrot0rBzBθ/rEθrotrBz0rBrEzrotBθ/rrBr0)\displaystyle=\left(\begin{array}[]{cccc}0&-E_{r}^{rot}&-E_{\theta}^{rot}&-E_{z}^{rot}\\ E_{r}^{rot}&0&rB_{z}&-B_{\theta}/r\\ E_{\theta}^{rot}&-rB_{z}&0&rB_{r}\\ E_{z}^{rot}&B_{\theta}/r&-rB_{r}&0\end{array}\right) (C.37)

with the rotating EM fields as a function of the lab EM fields given by

Eθrot=Eθ,Errot=Er+ωrBz,Ezrot=EzωrBr\displaystyle E_{\theta}^{rot}=E_{\theta},\quad E_{r}^{rot}=E_{r}+\omega rB_{z},\quad E_{z}^{rot}=E_{z}-\omega rB_{r} (C.38)
Bθrot=Bθ,Brrot=BrωrEz,Bzrot=Bz+ωrEr\displaystyle B_{\theta}^{rot}=B_{\theta},\quad B_{r}^{rot}=B_{r}-\omega rE_{z},\quad B_{z}^{rot}=B_{z}+\omega rE_{r} (C.39)

or Erot=E+(ωez×r)×BE_{rot}=E+(\omega\vec{e}_{z}\times\vec{r})\times B and Brot=B(ωez×r)×EB_{rot}=B-(\omega\vec{e}_{z}\times\vec{r})\times E. The rotating fields are obtained from the field strength through

Eirot=Fi0,Birot=12ϵ0ijkFjk.\displaystyle E_{i^{\prime}}^{rot}=F_{i^{\prime}0^{\prime}},\qquad B_{i^{\prime}}^{rot}=\frac{1}{2}\epsilon_{0^{\prime}i^{\prime}j^{\prime}k^{\prime}}F^{j^{\prime}k^{\prime}}. (C.40)

The field strength in (C.32) gives the Maxwell equations

νFrotμν=jrotμ{E=jrot0×Brot=Et+jrot\displaystyle\nabla_{\nu^{\prime}}F^{\mu^{\prime}\nu^{\prime}}_{rot}=j^{\mu^{\prime}}_{rot}\qquad\qquad\left\{\begin{array}[]{ll}\nabla\cdot E=j^{0^{\prime}}_{rot}\\ \nabla\times B_{rot}=\frac{\partial E}{\partial t}+j_{rot}\end{array}\right. (C.43)

and

νF~rotμν=0{B=0×Erot=Bt,\displaystyle\nabla_{\nu^{\prime}}\tilde{F}^{\mu^{\prime}\nu^{\prime}}_{rot}=0\qquad\qquad\left\{\begin{array}[]{ll}\nabla\cdot B=0\\ \nabla\times E_{rot}=-\frac{\partial B}{\partial t}\end{array}\right.\,, (C.46)

with

jrotμ=(ρ,jr,jθρω,jz)\displaystyle j^{\mu^{\prime}}_{rot}=\left(\rho,j^{r},j^{\theta}-\rho\,\omega,j^{z}\right) (C.47)

and μ\nabla_{\mu^{\prime}} the covariant derivative in the metric

ds2=dt2+dr2+r2(dθ+ωdt)2+dz2.\displaystyle ds^{\prime 2}=-dt^{\prime 2}+dr^{\prime 2}+r^{\prime 2}(d\theta^{\prime}+\omega dt^{\prime})^{2}+dz^{\prime 2}. (C.48)

The rotating frame Poynting flux

Prot\displaystyle P_{rot} =(BzrotEθrotBθrotEzrotr,BrrotEzrotBzrotErrotr,BθrotErrotBrrotEθrotr)\displaystyle=\left(\frac{B_{z}^{rot}E_{\theta}^{rot}-B_{\theta}^{rot}E_{z}^{rot}}{r^{\prime}},\frac{B_{r}^{rot}E_{z}^{rot}-B_{z}^{rot}E_{r}^{rot}}{r^{\prime}},\frac{B_{\theta}^{rot}E_{r}^{rot}-B_{r}^{rot}E_{\theta}^{rot}}{r^{\prime}}\right) (C.49)

is determined by the Maxwell stress tensor through

T0i\displaystyle T^{i^{\prime}}_{\phantom{ii}0^{\prime}} =Proti.\displaystyle=-P^{i^{\prime}}_{rot}\,\,. (C.50)

Further references on EM fields in rotating frames are Arendt:1998vq and ThorneMacDonald .

Appendix D General curved space EM field definitions

For uu a future-pointing unit time-like vector field (uμuμ=1u^{\mu}u_{\mu}=-1) in a 4-dimensional curved spacetime gμνg_{\mu\nu}, the associated observer with four-velocity uu measures EM fields (see e.g. Felice:2010cra )

Eμ\displaystyle E_{\mu} =Fμνuν\displaystyle=F_{\mu\nu}u^{\nu} (D.1)
Bμ\displaystyle B_{\mu} =12ϵσμαβFαβuσ\displaystyle=\frac{1}{2}\epsilon_{\sigma\mu\alpha\beta}F^{\alpha\beta}u^{\sigma} (D.2)

and Poynting vector

Pμ=ϵσμνρuσEνBρ.\displaystyle P^{\mu}=\epsilon^{\sigma\mu\nu\rho}u_{\sigma}E_{\nu}B_{\rho}. (D.3)

The Poynting vector is defined as

Pμ=γαμTαβuβ=TρμuρuμuβTρβuρ\displaystyle P^{\mu}=-\gamma^{\mu}_{\phantom{\mu}\alpha}T^{\alpha\beta}u_{\beta}=-T^{\mu}_{\phantom{\alpha}\rho}u^{\rho}-u^{\mu}u_{\beta}T^{\beta}_{\phantom{\beta}\rho}u^{\rho} (D.4)

in terms of the induced metric γαβ\gamma_{\alpha\beta} on the hypersurface orthogonal to uu,

γαβ=gαβ+uαuβ.\displaystyle\gamma^{\alpha\beta}=g^{\alpha\beta}+u^{\alpha}u^{\beta}\,\,. (D.5)
Rotating cylinder

We now apply these definitions to the rotating cylinder spacetime (C.48). For an observer uμ=(1,0,0,0)u^{\mu^{\prime}}=(1,0,0,0) at rest in the rotating frame, (D.1) and (D.2) extract the fields E=(Errot,Eθrot,Ezrot)E=(E_{r}^{rot},E_{\theta}^{rot},E_{z}^{rot}) and B=(Brrot,Bθrot,Bzrot)B=(B_{r}^{rot},B_{\theta}^{rot},B_{z}^{rot}), and (D.4) gives (C.50) for the Poynting flux (C.49). (Notice however that (D.3) does not reproduce (C.49), because the observer’s four-velocity is not normalized to unity.)

On the other hand, the unit normal to a constant time surface is given by uμ=(1,0,0,0)u_{\mu^{\prime}}=(-1,0,0,0). The corresponding observer

uμ=(1,0,ω,0)\displaystyle u^{\mu^{\prime}}=(1,0,-\omega,0) (D.6)

is a zero angular momentum observer or ‘ZAMO’, as it satisfies uμημ=0u^{\mu^{\prime}}\eta_{\mu^{\prime}}=0 with η\eta the angular Killing vector of the spacetime. The definitions (D.1)-(D.3) then extract the lab EM fields E=(Er,Eθ,Ez)E=(E_{r},E_{\theta},E_{z}) and B=(Br,Bθ,Bz)B=(B_{r},B_{\theta},B_{z}), as well as the the lab Poynting vector (C.27). Indeed, the ZAMO rotates in the rotating frame and corresponds to an observer at rest in the lab frame (C.26),

uμ=(1,0,0,0)\displaystyle u^{\mu}=(1,0,0,0) (D.7)

via uμ=xμxμuμu^{\mu^{\prime}}=\frac{\partial x^{\mu^{\prime}}}{\partial x^{\mu}}u^{\mu}.

References