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Inspirals from the innermost stable circular orbit of Kerr black holes:
Exact solutions and universal radial flow

Andrew Mummery [email protected]    Steven Balbus Oxford Astrophysics, Denys Wilkinson Building, Keble Road, Oxford, OX1 3RH, United Kingdom
Abstract

We present exact solutions of test particle orbits spiralling inward from the innermost stable circular orbit (ISCO) of a Kerr black hole. Our results are valid for any allowed value of the angular momentum aa-parameter of the Kerr metric. These solutions are of considerable physical interest. In particular, the radial 4-velocity of these orbits is both remarkably simple and, with the radial coordinate scaled by its ISCO value, universal in form, otherwise completely independent of the black hole spin.

I 1. Introduction

Classes of exact orbital solutions in the full Kerr geometry are a known, but under-utilised commodity. Examples include pure circular orbits, radial plunges rev1 , so-called zoom-whirl orbits, and homoclinic orbits, which separate long-lived bound and plunging states LP1 (see LP2 for a useful ‘periodic table’ of different black hole orbits). The study of relativistic test-particle orbits characterised by the energy and angular momentum of a circular orbit, but which are not moving on that orbit, is not new Darwin , but has yet to be astrophysically fully exploited. In this Letter, we analyse an important sub-class of these orbits, and present exact Kerr orbital solutions in a parameter regime of direct physical interest to black hole accretion. While simple in mathematical form, these solutions exhibit revealing features which are important for understanding the accretion process, but have not been discussed before.

One of the most salient features of orbits in Kerr spacetimes is the existence of an innermost stable circular orbit, or ISCO. Exterior to the radial ISCO coordinate r=rIr=r_{I}, circular orbits are stable and approach their Keplerian 1/r1/\sqrt{r} velocity behaviour on scales large compared to the horizon radius. Interior to r=rIr=r_{I}, the angular momentum of a circular orbit increases inward, which means that the orbits are unstable: a tiny perturbation from circular motion will eventually acquire a significant inward radial velocity, even while formally conserving its angular momentum and energy.

Orbits interior to the ISCO are of astrophysical interest because of their direct relevance to black hole accretion theory (e.g., SS ; NT ; PT ). In particular, the question of whether, and if so under what conditions, there can be significant X-ray emission or other observational signatures from matter flowing inward from the ISCO is an active area of current research Wilkins ; Fabian . This problem is generally approached via numerical techniques (e.g., Wilkins ; Potter ), as the assumptions of the classical analytic “viscous” solutions of black hole accretion theory completely breakdown at, and within, the ISCO. The classical viscous disc solution for UrU^{r} diverges at the formal ISCO radius NT ; PT , and without a more fundamental understanding of the inflow dynamics, it is not even clear how to frame the underlying equations! With a few notable exceptions Rey ; Wilkins ; Fabian virtually all existing accretion models are artificially cut-off at the ISCO.

In this work we show that there is an overlooked but dramatic simplification of this problem, which provides a clear path forward. The implicit averaging procedure associated with viscous (more accurately, turbulent) disc theory no longer makes sense when the orbits are not circular, but plunging Rey . The need to shed angular momentum vanishes. Instead, in the Kerr geometry angular momentum is simply advected inward with the fluid elements, and thus remains approximately constant and independent of position. What is new here is an explicit solution for the Kerr radial 4-velocity, which determines the surface density directly from mass conservation, and is is both simple and universal in form. This is a key result of this paper. With UrU^{r} known, we present exact, closed analytic solutions to the general problem of a test particle starting at r=rIr=r_{I} at time t=t=-\infty, and thereafter inspiraling toward the origin. The orbital shape (radial coordinate as a function of azimuthal angle ϕ\phi) is determined entirely in terms of elementary functions. For the Schwarzschild geometry, this orbital shape is exceptionally simple (see eq. [16]). Despite making an appearance in Chandrasekhar’s classic text Chand , it seems to have remained dormant and largely unreferenced in the astrophysical literature. The orbital solutions for more general Kerr geometries, also of astrophysical interest but which seem not to have been discussed in the literature, are best expressed in parameterised r(ψ),ϕ(ψ)r(\psi),\phi(\psi) form, in a manner analogous to the classical Friedman matter-dominated cosmologies.

II 2. Preliminary analysis

Throughout this work we use geometric units in which both cc, the speed of light, and GG, the Newtonian gravitational constant, are set equal to unity. In coordinates xμx^{\mu}, the invariant line element is dτ2=gμνdxμdxν{\rm d}\tau^{2}=-g_{\mu\nu}{\rm d}x^{\mu}{\rm d}x^{\nu}, where gμνg_{\mu\nu} is the usual covariant metric tensor with spacetime indices μ,ν\mu,\nu. (We use the signature convention +++-+++.) The coordinates are standard (t,r,θ,ϕ)(t,r,\theta,\phi) Boyer-Lindquist, where tt is time as measured at infinity, and the other symbols have their usual quasi-spherical interpretation. We shall work exclusively in the Kerr midplane θ=π/2\theta=\pi/2. For black hole mass MM and angular momentum aa (both having dimensions of length in our choice of units), the non-vanishing gμνg_{\mu\nu} required for our calculation are presented here for convenience (e.g. HEL ):

g00\displaystyle g_{00} =1+2M/r,g0ϕ=gϕ0=2Ma/r,\displaystyle=-1+2M/r,\quad g_{0\phi}=g_{\phi 0}=-2Ma/r,
gϕϕ\displaystyle g_{\phi\phi} =r2+a2+2Ma2/r,grr=r2/(r22Mr+a2).\displaystyle=r^{2}+a^{2}+2Ma^{2}/r,\quad g_{rr}=r^{2}/(r^{2}-2Mr+a^{2}). (1)

The 4-velocity vectors are denoted by Uμ=dxμ/dτU^{\mu}={\rm d}x^{\mu}/{\rm d}\tau. Their covariant counterparts UμU_{\mu}, in particular U0U_{0} and UϕU_{\phi}, have a significance as conserved quantities and are discussed further below. Test particles orbits which spiral inwards, starting at a distant time t=t=-\infty from a circular orbit at r=rIr=r_{I}, will preserve their energy and angular momentum. General expressions for the circular angular momentum and energy at radius rr may be found in HEL :

Uϕ\displaystyle U_{\phi} =(Mr)1/2𝒟(1+a2/r22aM1/2/r3/2),\displaystyle={(Mr)^{1/2}\over{\cal D}}(1+a^{2}/r^{2}-2aM^{1/2}/r^{3/2}), (2)
U0\displaystyle U_{0} =1𝒟(12M/r+aM1/2/r3/2),\displaystyle=-{1\over{\cal D}}(1-2M/r+aM^{1/2}/r^{3/2}), (3)

where

𝒟2=13M/r+2aM1/2/r3/2.{\cal D}^{2}=1-3M/r+2aM^{1/2}/r^{3/2}. (4)

The circular orbits described by eqs. (2) and (3) are not stable at all radii, and it may be shown (e.g., HEL ) that these orbits are stable only when the following condition is satisfied:

(16Mr3a2r2+8aM1/2r3/2)>0,\left(1-{6M\over r}-{3a^{2}\over r^{2}}+{8aM^{1/2}\over r^{3/2}}\right)>0, (5)

which corresponds to rUϕ>0\partial_{r}U_{\phi}>0. The location of marginal stability r=rIr=r_{I} corresponds to this expression vanishing:

rI2\displaystyle r_{I}^{2} =6MrI8aMrI+3a2\displaystyle=6Mr_{I}-8a\sqrt{Mr_{I}}+3a^{2}
=2MrI3+16MrI3(13a4MrI)2.\displaystyle={2Mr_{I}\over 3}+{16Mr_{I}\over 3}\left(1-{3a\over 4\sqrt{Mr_{I}}}\right)^{2}. (6)

The form of the second equality will be especially convenient in what follows below.

We label the constants of motion J=Uϕ(rI),γ=U0(rI)J=U_{\phi}(r_{I}),\gamma=-U_{0}(r_{I}), and use equation (II) to substitute for rI2r_{I}^{2}. The resulting numerators and denominators factor cleanly, leading to an additional simplification:

J\displaystyle J =23M(12a3MrI),\displaystyle=2\sqrt{3}M\left(1-{2a\over 3\sqrt{Mr_{I}}}\right), (7)
γ\displaystyle\gamma =433(MrI)1/2(13a4MrI)=(12M3rI)1/2,\displaystyle={4\over 3}\sqrt{3}\left(M\over r_{I}\right)^{1/2}\left(1-{3a\over 4\sqrt{Mr_{I}}}\right)=\left(1-{2M\over 3r_{I}}\right)^{1/2}, (8)

where in the second γ\gamma equality we have made use of equation (II). Notice that γ\gamma is independent of aa, apart from the simple implicit rIr_{I} dependence.

III 3. Orbital Solutions

III.1 3a. Radial velocity of the ISCO inspiral

As noted earlier, general relativistic dynamics allows for radial motion in orbits whose angular momentum and energy values correspond to an exactly circular orbit. While the governing equation is easily stated

grr(Ur)2+U0U0+UϕUϕ=1,g_{rr}(U^{r})^{2}+U^{0}U_{0}+U^{\phi}U_{\phi}=-1, (9)

its direct solution is generally a matter of some algebraic complexity. Expressing all non-radial 4-velocities in terms of JJ and γ\gamma, and multiplying through by 1/grr1/g_{rr}, we have

(Ur)2+Jr2(2Maγr+(12Mr)J)γr2[(r2+a2+2Ma2r)γ2MaJr]=1a2r2+2Mr.({U^{r}})^{2}+{{J}\over r^{2}}\left({2Ma{\gamma}\over r}+\left(1-{2M\over r}\right){J}\right)\\ -{{\gamma}\over r^{2}}\left[\left(r^{2}+a^{2}+{2Ma^{2}\over r}\right){\gamma}-{2Ma{J}\over r}\right]=-1-{a^{2}\over r^{2}}+{2M\over r}. (10)

Equation (10) is of the form (Ur)2+Veff(r)=0({U^{r}})^{2}+V_{\rm eff}(r)=0, where VeffV_{\rm eff} is a cubic in 1/r1/r which may always be factored:

Veff(r)=V0(r1r1)(r2r1)(r3r1),V_{\rm eff}(r)=-V_{0}\left({r_{1}\over r}-1\right)\left({r_{2}\over r}-1\right)\left({r_{3}\over r}-1\right), (11)

where r1,r2r_{1},r_{2} and r3r_{3} are the general (possibly complex) roots of VeffV_{\rm eff}. (VeffV_{\rm eff} is, up to an irrelevant factor of 22, the usual effective potential.)

For an arbitrary circular orbit of radius r=rcr=r_{c}, both Veff(rc)=0V_{\rm eff}(r_{c})=0 and rVeff(rc)=0\partial_{r}V_{\rm eff}(r_{c})=0, and rcr_{c} will thus be a double root of the polynomial. For the particular case of a marginally stable circular orbit, there is an additional condition, r2Veff(rc)=0\partial^{2}_{r}V_{\rm eff}(r_{c})=0. Thus, rIr_{I} must be a triple root of Ur{U^{r}}. The normalisation constant V0V_{0} may be found by going back to equation (10) and taking the formal limit rr\rightarrow\infty. We find

V0=1γ2=2M3rI,V_{0}=1-\gamma^{2}={2M\over 3r_{I}}, (12)

which leads directly to our final equation for UrU^{r}:

Urdrdτ=2M3rI(rIr1)3/2.{U^{r}}\equiv{{\rm d}r\over{\rm d}\tau}=-\sqrt{2M\over 3{r_{I}}}\left({{r_{I}}\over r}-1\right)^{3/2}. (13)

This may also be verified by a (considerably more lengthy!) direct computation. Note the universality of this remarkable result: there is no aa-dependence in this expression other than implicitly through rIr_{I}. Every Kerr orbit inspiraling from an ISCO is self-similar in its radial motion. As expected, no radial velocity solutions exist for r>rIr>r_{I}. Despite its generality, simplicity and importance, equation [13] does not appear to have been recognised before in the literature.

The azimuthal component of the intra-ISCO 4-velocity is also simple:

Uϕ=gϕ0γ+gϕϕJ=2Mγa+J(r2M)r(r22Mr+a2).U^{\phi}=-g^{\phi 0}{\gamma}+g^{\phi\phi}{J}={2M{\gamma}a+{J}(r-2M)\over r(r^{2}-2Mr+a^{2})}. (14)

III.2 3b. Schwarzschild orbits

We begin with the Schwarzschild limit a=0a=0. Then rI=6Mr_{I}=6M, J=23MJ=2\sqrt{3}M, and Uϕ=23M/r2U^{\phi}=2\sqrt{3}M/r^{2}. Defining x=r/rIx=r/r_{I}, we find

dϕdx=6MUϕUr=31x2(1x1)3/2,{{\rm d}\phi\over{\rm d}x}=6M{U^{\phi}\over U^{r}}=-\sqrt{3}{1\over x^{2}}\left({1\over x}-1\right)^{-3/2}, (15)

which immediately integrates to

x=r6M=11+12/ϕ2,x={r\over 6M}={1\over 1+12/\phi^{2}}, (16)

with the convention that ϕ\phi increases from -\infty to 0 as xx goes from 11 to 0. This is an exact orbital solution for the standard Schwarzschild metric, which is both non-circular and non-radial, extending from rIr_{I} to r=0r=0. The reader may verify this by direct substitution into the exact Schwarzschild orbit equation for u=1/ru=1/r:

d2udϕ2+u=MJ2+3Mu2.{{\rm d}^{2}u\over{\rm d}\phi^{2}}+u={M\over J^{2}}+3Mu^{2}. (17)

Equation (13) is also easily integrated. This result, moreover, holds for any Kerr ISCO-inspiral orbit, not just for those in the Schwarzschild geometry. With x=r/rIx=r/r_{I}, we find

τ=3rI32M(3sin1x+(x3)x1x)\tau=\sqrt{3r_{I}^{3}\over 2M}\left(3\sin^{-1}\sqrt{x}+(x-3)\sqrt{x\over 1-x}\right) (18)

a universal relationship between proper time τ\tau and coordinate rr. It may also be written in parametric form, reminiscent of closed Friedmann cosmologies:

x\displaystyle x =12(1cosψ)=sin2(ψ/2),\displaystyle={1\over 2}(1-\cos\psi)=\sin^{2}(\psi/2), (19)
τ\displaystyle\tau =3rI32M[12(3ψsinψ)2tan(ψ2)],\displaystyle=\sqrt{3r_{I}^{3}\over 2M}\left[{1\over 2}(3\psi-\sin\psi)-2\tan\left(\psi\over 2\right)\right], (20)

with ψ\psi running from π\pi to 0.

III.3 3c. General solution

The general parameterised azimuthal solution ϕ(ψ)\phi(\psi) is considerably more complicated. Start with

dτdψ=3rI32Msin2(ψ/2)tan2(ψ/2),{{\rm d}\tau\over{\rm d}\psi}=-\sqrt{3r_{I}^{3}\over 2M}\sin^{2}(\psi/2)\tan^{2}(\psi/2), (21)

whence

dϕdψ=Uϕ3rI32Msin2(ψ/2)tan2(ψ/2).{{\rm d}\phi\over{\rm d}\psi}=-U^{\phi}\sqrt{3r_{I}^{3}\over 2M}\sin^{2}(\psi/2)\tan^{2}(\psi/2). (22)

With UϕU^{\phi} substituted from (14) and r=rIsin2(ψ/2)r=r_{I}\sin^{2}(\psi/2), this equation has the formal solution

ϕ(ψ)=3rI32M1rI3[2M(Jaγ)I1JrII2],\phi(\psi)=\sqrt{3r_{I}^{3}\over 2M}{1\over r^{3}_{I}}\left[2M(J-a\gamma)I_{1}-Jr_{I}I_{2}\right], (23)

where I1I_{1} and I2I_{2} may be written in the single compact form:

Ij=πψtan2(ψ/2)(1+[1j]cos2(ψ/2))dψsin4(ψ/2)2Msin2(ψ/2)/rI+a2/rI2.I_{j}=\int^{\psi}_{\pi}{\tan^{2}(\psi^{\prime}/2)\left(1+[1-j]\cos^{2}(\psi^{\prime}/2)\right){\rm d}\psi^{\prime}\over\sin^{4}(\psi^{\prime}/2)-2M\sin^{2}(\psi^{\prime}/2)/r_{I}+a^{2}/r_{I}^{2}}. (24)

Both I1I_{1} and I2I_{2} have poles at the Kerr event horizons, r+r_{+}, rr_{-}, at the ψ\psi values given by

rIsin2(ψ±/2)=r±=M±M2a2.r_{I}\sin^{2}(\psi_{\pm}/2)=r_{\pm}=M\pm\sqrt{M^{2}-a^{2}}. (25)
Refer to caption
Figure 1: Coefficients C0,C+C_{0},C_{+} and CC_{-} appearing in the parametric ϕ(ψ)\phi(\psi)   solution (eqs. 32, 33), as a function of     a/Ma/M. (Spin axis plotted for 0.998<a/M<0.998-0.998<a/M<0.998.)

I1I_{1} and I2I_{2} may be evaluated by the Weierstrass substitution

t=tan(ψ/2).t=\tan(\psi^{\prime}/2). (26)

We then find I1=K1+K2I_{1}=K_{1}+K_{2}, I2=K2I_{2}=K_{2}, where

Kj\displaystyle K_{j} =2t2jαt42βt2+a2/rI2dt,\displaystyle=\int{2t^{2j}\over\alpha t^{4}-2\beta t^{2}+a^{2}/r_{I}^{2}}\,{\rm d}t, (27)
α\displaystyle\alpha =12M/rI+a2/rI2,β=M/rIa2/rI2.\displaystyle=1-2M/r_{I}+a^{2}/r_{I}^{2},\quad\beta=M/r_{I}-a^{2}/r_{I}^{2}. (28)

The two roots of the denominator of the KK-integrals are

t±2=α1(β±β2a2/rI2),t^{2}_{\pm}={\alpha^{-1}}\left(\beta\pm\sqrt{\beta^{2}-a^{2}/r_{I}^{2}}\right), (29)

which, from [25], are

t±=tan(ψ±/2)=x±1x±,x±r±/rI.t_{\pm}=\tan(\psi_{\pm}/2)=\sqrt{x_{\pm}\over 1-x_{\pm}},\quad x_{\pm}\equiv r_{\pm}/r_{I}. (30)

After factoring the denominators, the KK-integrals may be evaluated by partial fraction expansions. Omitting the lengthy but straightforward details, the final result for ϕ\phi is

ϕ(ψ)=C0tan(ψ/2)+Ctanh1(tan(ψ/2)tan(ψ/2))C+tanh1(tan(ψ+/2)tan(ψ/2)).\phi(\psi)=C_{0}\tan(\psi/2)+C_{-}\tanh^{-1}\left({\tan(\psi_{-}/2)\over\tan(\psi/2)}\right)\\ -C_{+}\tanh^{-1}\left({\tan(\psi_{+}/2)\over\tan(\psi/2)}\right). (31)

We have defined the constants

C0\displaystyle C_{0} =6rIM2M(Jaγ)rIJrI22MrI+a2,\displaystyle=\sqrt{6r_{I}\over M}\ {2M(J-a\gamma)-r_{I}J\over r^{2}_{I}-2Mr_{I}+a^{2}}, (32)
C±\displaystyle C_{\pm} =t±t+2t26rIM2M(Jaγ)(1+t±2)rIJt±2rI22MrI+a2.\displaystyle={t_{\pm}\over t_{+}^{2}-t_{-}^{2}}\sqrt{6r_{I}\over M}\ {2M(J-a\gamma)(1+t_{\pm}^{2})-r_{I}Jt_{\pm}^{2}\over r^{2}_{I}-2Mr_{I}+a^{2}}. (33)

This can also be written explicitly as a function of radius:

ϕ(r)=C0rrIr+Ctanh1(rr(rrI)(rrI))C+tanh1(r+r(rrI)(r+rI)).\phi(r)=C_{0}\sqrt{r\over r_{I}-r}+C_{-}\tanh^{-1}\left(\sqrt{{r_{-}\over r}{(r-r_{I})\over(r_{-}-r_{I})}}\right)\\ -C_{+}\tanh^{-1}\left(\sqrt{{r_{+}\over r}{(r-r_{I})\over(r_{+}-r_{I})}}\right). (34)

(The arguments of the tanh1\tanh^{-1} functions should be inverted for radial coordinates within the horizons r<r±r<r_{\pm}.) The CC-coefficients are plotted as a function of black hole spin in fig. [1]. The Schwarzschild limit a0a\rightarrow 0 and rI=6Mr_{I}=6M, for which C±=0C_{\pm}=0, C0=23C_{0}=-2\sqrt{3}, is easily verified. An example inspiral trajectory given by equation 34 with a/M=+0.75a/M=+0.75 is shown in fig. [2]. These solutions have been verified against numerical integration of the geodesic equations.

Refer to caption
Figure 2: Inspiral (eq. [34]) of a test particle from ISCO (r3.158Mr\simeq 3.158M) to event horizon (r+1.661Mr_{+}\simeq 1.661M) of a Kerr black hole, a/M=+0.75a/M=+0.75.

III.4 3d. Extremal spin limit

The above solution for ϕ(r)\phi(r) is ill-defined in the maximal a/M=±1a/M=\pm 1 limit, as the two event horizons of the Kerr geometry coincide (t+=tt_{+}=t_{-}), and the partial fraction approach used in solving equation (23) must be revisited. For the a=+Ma=+M solution, the ISCO and event horizons formally coincide in Boyer-Lindquist coordinates. For a=Ma=-M the orbit is more interesting, and we are able to solve exactly for r(ϕ)r(\phi). We rewrite equation 23 (with J=223M/9{J}=22\sqrt{3}M/9, γ=53/9{\gamma}=5\sqrt{3}/9, rI=9Mr_{I}=9M, a=Ma=-M and t=tan[ψ/2]t=\tan[\psi/2]) as

ϕ92=6t2(8t21)2dt16t4(8t21)2dt,{\phi\over 9\sqrt{2}}=\int{6t^{2}\over(8t^{2}-1)^{2}}\,{\rm d}t-\int{16t^{4}\over(8t^{2}-1)^{2}}\,{\rm d}t, (35)

which becomes

ϕ92=2t318t2.{\phi\over 9\sqrt{2}}={2t^{3}\over 1-8t^{2}}. (36)

With t2=r/(rIr)t^{2}=r/(r_{I}-r), we find for ϕ(r)\phi(r):

ϕ(r)=223M3/2r3/2(1r/M)1r/9M.\phi(r)={2\sqrt{2}\over 3M^{3/2}}{r^{3/2}\over(1-r/M)\sqrt{1-r/9M}}. (37)

Inverting equation (36) to solve for t(ϕ)t(\phi) (and thus r(ϕ)r(\phi)) is interesting, as it highlights the solutions from all branches of the resulting cubic equation

t3+4ϕ92t2ϕ182=0.t^{3}+{4\phi\over 9\sqrt{2}}t^{2}-{\phi\over 18\sqrt{2}}=0. (38)

In fact, there are actually four branches of interest in this problem! Physically this arises from frame dragging, which produces a multi-valued ϕ(r)\phi(r). The three nominal roots of the cubic, tjt_{j}, may be written:

tj\displaystyle t_{j} =22ϕ27[2cos(13cos1[2187128ϕ21]+2πj3)1],\displaystyle={2\sqrt{2}\phi\over 27}\left[2\cos\left({1\over 3}\cos^{-1}\left[{2187\over 128\phi^{2}}-1\right]+{2\pi j\over 3}\right)-1\right], (39)

with j=0,1,2j=0,1,2. The fourth branch t3t_{3} may be formally identified with the (j=0j=0) t0t_{0} root, but one must change cos\cos and cos1\cos^{-1} into cosh\cosh and cosh1\cosh^{-1} respectively, as the argument of the cos1\cos^{-1} exceeds unity for t3t_{3} orbits. All four branches are needed, as we now discuss.

Refer to caption
Refer to caption
Figure 3: Inspiral of a test particle from ISCO (r=9Mr=9M) to singularity of an extremal Kerr black hole a=Ma=-M (eq. [37] et seq.). Upper figure shows the magnitude of the ϕ\phi coordinate over the infall, with the four rj(ϕ)r_{j}(\phi) branches of the solution color-coded (see text). The value of the frame-dragging angle ϕ\phi_{\star} (eq. [41]) is shown by the horizontal dashed line. The lower figure shows the inspiral in quasi-Cartesian coordinates with the same color-coding scheme. Note the pronounced effect of counter rotating frame dragging upon the orbit.

The radial solutions for these roots are

rj=9Mtj21+tj2,r_{j}={9Mt_{j}^{2}\over 1+t_{j}^{2}}, (40)

with different roots corresponding to different “legs” of the orbit. The path of a test particle inspiralling from the retrograde ISCO of a maximally rotating Kerr black hole is as follows. The particle starts at r=9Mr=9M, with ϕ=\phi=-\infty. It spirals inwards towards the event horizon, with increasing ϕ\phi, until it crosses the special radius r=27M/11r_{\star}=27M/11 at an angle

ϕ=27316,\phi_{\star}=-{27\sqrt{3}\over 16}, (41)

whereupon frame-dragging bends the orbit backwards, and the particle begins to corotate with the black hole (Fig. 3). Note that this location is exterior to the ergosphere rE=2Mr_{E}=2M. During this initial phase the radial coordinate is given by the r1(ϕ)r_{1}(\phi) solution (eq. 39). Beyond this point, the orbit transitions onto the r2(ϕ)r_{2}(\phi) branch, with ϕ\phi once again tending towards -\infty as the particle approaches the event horizon rH=Mr_{H}=M. Within the event horizon, the orbit is first described by the r0(ϕ)r_{0}(\phi) expression, with |ϕ|<ϕ<|\phi_{\star}|<\phi<\infty, and then the final branch r3(ϕ)r_{3}(\phi) for 0<ϕ<|ϕ|0<\phi<|\phi_{\star}| (Fig 3).

IV 4. Discussion: accretion inside the ISCO

The most important result of this Letter for the modelling of black hole accretion flows is also the simplest, namely equation (13) for Ur(r){U^{r}}(r), the universal form of the radial 4-velocity for a test particle insprialling from the ISCO radius of a Kerr black hole while retaining its circular energy and angular momentum. This is of great astrophysical interest because the accretion of a steady mass flow M˙\dot{M} in a thin disk is characterised by a constant value of the mass flux 2πΣrUr2\pi\Sigma rU^{r} (here, Σ\Sigma is the disk surface density). Here, we have learned that within the ISCO, UrU^{r} is generally known a priori and is extremely simple (at least for midplane orbits). A stress term is not needed in this region, and may be ignored since now gravity alone is much more efficient at powering inward flow. By way of contrast, external to the ISCO, to have any systematic radial velocity at all, an enhanced stress is absolutely essential PT ; NT . With this external stress remaining finite at the ISCO itself, the interior and exterior solutions both have vanishingly small velocities at rIr_{I}, so that joining these two branches to form a global black hole accretion solution is a natural, and potentially very revealing, next step.

The energetics of the post-ISCO flow is also very important, and becomes much more accessible once the radial velocity is known a priori. The prompt acceleration results in a rapid drop in Σ\Sigma and therefore the hot internal radiation field will escape more easily. Offsetting this is a radial expansion producing global cooling. This radial expansion is to some extent offset by the vertical compression of the flow near the outer Kerr event horizon, a process which acts to heat the flow. An understanding of the interaction between these competing adiabatic effects, together with self-heating of the disc by its own emission will be needed to account for recent observations that appear to show an additional hot disk component, beyond the expectations of standard theory, in some sources Fabian .

A more precise knowledge of UrU^{r} is a very important aid for numerical accretion disk modellers. With a simple form for Ur=dr/dτU^{r}={\rm d}r/{\rm d}\tau, and detailed mathematical formulae for r(τ)r(\tau) and r(ϕ)r(\phi), these results promise to be of great practical utility for numerical code calibration Porth .

Finally, the imaging capabilities now available through the Event Horizon Telescope are on the verge of resolving the flow between the ISCO and event horizon itself Aki . The dynamic properties of the flow in the intra-ISCO region may one day soon be imaged directly. The data from such a study would no doubt provide interesting tests of the models derived here.

We conclude by noting that the mathematical methods used here also work well for other classes of noncircular orbits, which are defined by the energy and angular momentum of a non-ISCO circular orbit, and also for photon orbits. The analytic results of these studies will be fully described in a more lengthy investigation to follow.


Acknowledgements: We thank R. Blandford, K. Clough, P. Feirrera, C. Reynolds and J. Stone for stimulating conversations and helpful advice. This work is partially supported by the Hintze Family Charitable Trust and STFC grant ST/S000488/1.


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