Mode coupling of Schwarzschild perturbations: Ringdown frequencies
Enrique Pazos,1, 2 David Brizuela,3 José M. Martı́n-Garcı́a,4, 5 and Manuel Tiglio6
arXiv:1009.4665v1 [gr-qc] 23 Sep 2010
1
Center for Relativistic Astrophysics, School of Physics,
Georgia Institute of Technology, 837 State Street, Atlanta, GA 30332-0430
2
Departamento de Matemática, Universidad de San Carlos de Guatemala,
Edificio T4, Facultad de Ingenierı́a, Ciudad Universitaria z. 12, Guatemala
3
Theoretisch-Physikalisches Institut, Friedrich-Schiller-Universität, Max-Wien-Platz 1, 07743 Jena, Germany
4
Institut d’Astrophysique de Paris, CNRS, Univ. Pierre et Marie Curie, 98bis boulevard Arago, 75014 Paris, France
5
Laboratoire Univers et Théories, CNRS, Univ. Paris Diderot, 5 place Jules Janssen, 92190 Meudon, France
6
Department of Physics, Center for Fundamental Physics,
Center for Scientific Computation and Mathematical Modeling,
Joint Space Institute. University of Maryland, College Park, MD 20742, USA.
Within linearized perturbation theory, black holes decay to their final stationary state through
the well-known spectrum of quasinormal modes. Here we numerically study whether nonlinearities change this picture. For that purpose we study the ringdown frequencies of gauge-invariant
second-order gravitational perturbations induced by self-coupling of linearized perturbations of
Schwarzschild black holes. We do so through high-accuracy simulations in the time domain of
first and second-order Regge-Wheeler-Zerilli type equations, for a variety of initial data sets. We
consider first-order even-parity (ℓ = 2, m = ±2) perturbations and odd-parity (ℓ = 2, m = 0) ones,
and all the multipoles that they generate through self-coupling. For all of them and all the initial
data sets considered we find that —in contrast to previous predictions in the literature— the numerical decay frequencies of second-order perturbations are the same ones of linearized theory, and we
explain the observed behavior. This would indicate, in particular, that when modeling or searching
for ringdown gravitational waves, appropriately including the standard quasinormal modes already
takes into account nonlinear effects.
PACS numbers: 04.25.dk, 04.40.Dg, 04.30.Db, 95.30.Sf
I.
OUTLOOK AND MOTIVATION
Black hole no-hair theorems [1, 2] state that within
Einstein’s theory the end point of any system with
enough gravitational energy to form a black hole is remarkably simple: it is uniquely characterized by one
member of the Kerr family1 [3], which is described by
only two parameters: the spin and mass of the final black
hole.
As a consequence, the details by which different systems decay to such endpoints have been of interest for
many decades. Pioneering studies were done by a number
of authors in the early seventies, starting with studies of
linearized perturbations of non-rotating (Schwarzschild)
black holes (e.g., [4–6]). Press realized that there is always an intermediate stage where the ringdown is dominated by a set of oscillating and exponentially decaying
solutions, quasinormal modes (QNMs), whose spectrum
depends only on the mass of the black hole and the multipole index ℓ of the initial perturbation [7]. This regime is
followed by a power-law ‘tail’ decay due to backscattering
[8].
In the case of gravitational perturbations of nonrotating black holes the relevant equations from which
QNMs can be inferred are the Regge-Wheeler [9] and
1
Charge is expected not to play a significant role in most astrophysical scenarios.
Zerilli [10, 11] ones. For rotating black holes the corresponding one (though based on a curvature formalism, as
opposed to a metric one) is the Teukolsky equation [12].
Their QNMs were first studied by Teukolsky and Press
[13]. See [14, 15] for comprehensive reviews on the rich
area of QNMs.
The QNM with the lowest frequency is called the fundamental one. Since the subsequent ones (overtones) decay much faster, the ringdown of Kerr black holes in linearized theory is in practice described by a few oscillating
modes which decay exponentially in time, till they reach
the tail regime. It is interesting to note that the tail
decay problem for rotating black holes is still not completely understood [16–20].
From an observational point of view this universal ringdown spectrum is of great power: one can use a single QNM detection to infer the mass and spin of the
black hole source, assuming General Relativity to be correct. Alternatively, through a two-mode detection one
can test General Relativity and/or the assumption that a
black hole is the source of the measured signal [21]. The
main idea is that the QNM frequencies of both detections have to be consistent with respect to their inferred
masses/spins.
The LISA mission is expected to measure gravitational
waves in the low-frequency spectrum: (10−5 − 10−1 )
Hz, such as those emitted in the collision of supermassive binary black holes (SMBBHs) [22]. Flanagan and
Hughes [23] showed that, quite generically, the signal to
noise ratio for these sources in the inspiral regime should
2
be comparable to that one in the ringdown. Therefore,
detection of SMBBHs by LISA through the measurement
of QNMs seems to be feasible. Assuming a lower cutoff
of (10−4 − 10−5 ) Hz and requiring that the QNM signal
lives long enough to travel once through LISA’s propagation arms places a constraint on the mass range of the
SMBBH candidates: a few 105 M⊙ to (108 − 109 )M⊙ .
A step beyond detection analysis is that one of parameter estimation. In Ref. [22, 24] it was found that
through a single QNM detection LISA would be able to
accurately infer the mass and spin of supermassive black
holes: for black holes with mass M & 105 M⊙ the errors in
mass and spin would be smaller than one part in 102 , and
smaller than one part in 105 for the more optimistic case
M & 5 × 105 M⊙ 2 . These predicted accuracies depend
on the ringdown efficiency ǫrd , defined as the fraction
of mass radiated in ringdown waves. In these references
very conservative values were used: ǫrd ∼ 0.1%−3%. For
example, it has been found in numerical simulations of
two equal-mass, non-spinning black holes starting from
quasi-circular motion that around ǫrd ∼ 2% − 3% of the
total mass is radiated in the ringdown regime [25]. The
inclusion of different masses and/or spin increases this
value (see, for example, [26]).
In [22, 24] it was also found that at least a second detection of either mass or spin should be possible for LISA.
Resolving both spin and angular momentum (or, equivalently, both frequency and damping times associated with
the QNM oscillation of this second mode) might require
a very large critical signal to noise ratio, which might in
turn need the second mode to radiate a significant portion of the emitted gravitational wave when compared to
the first one. Whether this is feasible or not can only
be established by giving precise predictions of the amplitudes for secondary candidates.
Underlying in all these analyses is the implicit assumption that quasinormal modes and their spectrum of associated frequencies accurately describe the (intermediate)
stage of the ringdown to a final Kerr stationary state.
Which is certainly the case in linearized theory, but at the
same time there is evidence that effects of self-interaction
in gravitational waves might be observable with the expected sensitivity of LISA [27].
Similarly, quasinormal modes also play an important
role in the semi-analytical modeling of intermediate mass
black holes (IMBH), such as in the Effective One Body
approach [28, 29], where the gravitational wave as modeled within this formalism is stitched to a ringdown one
consisting of QNMs by enforcing continuity of the wave
and its derivatives and using the values of quasinormal
frequencies as expected from linearized theory [30–32]. In
this context, it is worth recalling that in close-limit stud-
2
Only cases with M & 105 M⊙ are considered in [22, 22, 24] because otherwise the QNM signal would be short lived enough
that special detection techniques might be needed.
ies of binary black holes it was found that corrections
from second-order perturbations were in some cases significant [33]. For IMBHs, which could have total masses
in the range of ∼ 100M⊙ − 104 M⊙ , it is especially important to accurately model the merger and ringdown since
they should fall in the frequency band of earth based
gravitational wave detectors. Although the existence of
IMBHs is still debatable, they could provide an interesting source for Advanced LIGO and VIRGO if they are
present in dense globular clusters [34] (see also [35]). Recent observational evidence of an IMBH can be found in
[36–39].
The previous discussions motivate us to study how
nonlinear perturbations of black holes decay in time: do
they do so just as in linearized theory or with a different
spectrum of frequencies? We carry out our study through
numerical simulations of first and second-order gaugeinvariant gravitational perturbations of Schwarzschild
black holes. We find that for all practical purposes,
and to high numerical accuracy, the complex decay frequencies of second-order perturbations are the standard
quasinormal ones from linearized theory –in contrast to
previous predictions in the literature [40–42]– and we explain why this appears to be the case. Essentially, in all
our simulations we find that mode-mode couplings excite nonlinearities in the early stages of the perturbations
before the quasinormal regime for the linearized perturbations kicks in. By the time the latter happens, those
couplings have decreased to negligible values and the excited nonlinearities essentially propagate as in linearized
theory; and, in particular, they decay with the standard
QNM frequencies.
The structure of the paper is as follows. Section II reviews the basics of Regge-Wheeler-Zerilli equations and
quasinormal modes, and Sec. III the main features of the
gauge-invariant approach here used for second-order perturbations. Section IV describes our numerical approach
and setup for solving the first and second-order ReggeWheeler and Zerilli equations, and Sec. V presents and
discusses our main results.
II. FIRST-ORDER PERTURBATIONS OF
SCHWARZSCHILD AND QUASINORMAL
MODES
Metric gravitational perturbations can be expanded in
tensor spherical harmonics. At the linear level modes
with different angular structure decouple from each other
if the background spacetime is spherically symmetric, as
is the case for the Schwarzschild metric. In addition,
for each multipole, perturbations of Schwarzschild can
be further split into two sectors with different parities,
which also decouple from each other in linearized theory.
For each multipole, each of these sectors is completely
described by a master function which depends on time
and radius. The Regge-Wheeler function contains all
the relevant information of the axial or odd-parity sec-
3
tor, whereas the Zerilli one encodes the polar or even
degrees of freedom. These functions satisfy master evolution equations,
102
(1)
(2)
{1} m
Φℓ denote, respectively, the firstwhere {1}Ψm
ℓ and
order Zerilli and Regge-Wheeler functions for a given
(ℓ, m) mode. The potentials that appear in these equations are given by
zerilli function
10
{1} m
{1}Φm
Φℓ = 0 ,
ℓ − VRW
{1} m
{1} m
Ψℓ − VZ Ψℓ = 0 ,
{1}
Ψ l=2, m=2
0
10-2
10-4
10-6
10-8
2
VZ ≡
ℓ(ℓ + 1) 6M r λ(λ + 2) + 3M (r − M )
− 3
,
r2
r
(rλ + 3M )2
VRW ≡
ℓ(ℓ + 1) 6M
− 3
r2
r
(3)
50
100
150
t/M
200
250
300
Figure 1: Solution to the first-order Zerilli equation at observer location r = 51.8M .
(4)
and are, in particular, independent of the azimuthal
index m. In these expressions λ ≡ 21 (ℓ − 1)(ℓ + 2),
M is the mass of the Schwarzschild black hole background, r its areal radius, and is the two-dimensional
D’Alambertian operator corresponding to the time and
radial sector of the background.
The complete spectrum of QNMs can be numerically
obtained by analyzing Eqs. (1,2) in the frequency domain. Computing in this way the amplitudes of QNMs
for any given initial data is not so straightforward,
though. Bearing in mind our motivation of studying the
behavior of second-order perturbations, we instead solve
Eqs. (1,2) in the time-domain. That is, we prescribe (a
variety of) initial data, evolve them and analyze the solutions at different observer locations as functions of time.
The early behavior of the solution depends on the type
of initial data, followed by the QNM ringdown of the
black hole. In Fig. 1 we show a typical solution of the
Zerilli equation, for a fixed observer at r = 51.8M as a
function of time. The initial data for this particular case
consist of a Gaussian profile to the initial time derivative of the Zerilli function, centered at r = 20M with a
width σ = 4M , and the initial value of the Zerilli function itself is set to zero. [This corresponds to what we call
time-derivative initial data in the following sections, see
Eqs. (12,13)]. To measure the complex QNM frequency
we perform a numerical fit to a function of the form
f (t) = A eat sin [b(t − t0 )] ,
0
(5)
where the parameters to be fitted are A, a, b and t0 and
the choice of the starting time for the QNM regime is
chosen as that one which optimizes the fit, as introduced
and explained in Ref. [43]. The quasinormal frequency
is therefore given as ω = a + bi. The expected value
for the fundamental QNM for an ℓ = 2 perturbation is
0.37367 − 0.08896i [15], while our fit for this simulation
yields 0.37077 − 0.08826i.
III. SECOND-ORDER GAUGE-INVARIANT
PERTURBATIONS OF SCHWARZSCHILD
We study second-order gravitational perturbations of
Schwarzschild black holes using a gauge-invariant formalism for arbitrary first and second-order perturbations
[44]. The key feature of this formalism is being able to
consider perturbations with arbitrary angular multipole
structure, and has been possible mostly due to the development of a suitable theoretical framework [45, 46] and
to the advance of very efficient symbolic algebra tools for
tensor-type calculations [47, 48].
Next we very briefly summarize those results of the
formalism presented in [44] which are relevant for the
current work; see that reference for more details.
Due to the intrinsic nonlinearities of General Relativity, any non-trivial solutions of Eqs. (1,2) generate
second-order contributions which are solutions of Zerilli
and Regge-Wheeler-type equations with source terms,
{2} m
{2}Φm
Φℓ =
ℓ − VRW
{2} m
{2} m
Ψℓ − VZ Ψℓ =
{2}
SΦ ,
SΨ .
{2}
(6)
(7)
The sources {2}SΨ and {2}SΦ depend quadratically on
the lower-order perturbations and their time and space
derivatives from both first-order sectors. That is, in general the coupling of even (odd) parity modes generates
odd (even) parity second-order modes; see Appendix A
for a detailed description of the selection rules for this
mode coupling.
Second-order Regge-Wheeler-Zerilli (RWZ) type functions are not unique: one can add to them any quadratic
combination of the first-order ones and they will still be
gauge invariant and will still satisfy equations of the form
(6,7) with different sources. For this reason, asking what
are the ringdown frequencies of second-order RWZ functions is not an unambiguous question; as opposed to, say,
asking what are the ringdown frequencies of the emitted
gravitational power. It turns out, however, that, as dis-
4
cussed in [44] and made explicit below, since the secondorder quantities, like {2}Ψ, {2}Φ, {2}SΨ and {2}SΦ , that
we use correspond to the ones labeled as regularized in
Ref. [44], there is a simple relationship between emitted power and the RWZ functions. Under such choice of
second-order RWZ functions it is therefore unambiguous
and physically motivated to ask what are their ringdown
frequencies.
Reference [44] deals with the most general case for
these sources and computation of the radiated energy.
Here we quantitatively explore the ringdown frequencies
First order
Multipoles Parity
(ℓ = 2 = |m|) even
(ℓ = 2, m = 0) odd
for some particular cases. Namely, we study first-order
(ℓ = |m| = 2) even-parity and (ℓ = 2, m = 0) odd-parity
perturbations and the modes that they generate through
self-coupling. That is, for simplicity we do not consider
the coupling between the mentioned even and odd-parity
first-order modes. We do not explicitly list the sources
{2}
SΨ and {2}SΦ for the cases here considered because
they are rather lengthy and complicated expressions, but
they are available from the authors upon request. The
generated modes and the radiated energy carried by them
are described next and summarized in Table I.
Second order
Multipoles
Parity
(ℓ = 4 = m),(ℓ = 4, m = 0),(ℓ = 2, m = 0) even
(ℓ = 4, m = 0),(ℓ = 2, m = 0) even
Table I: First-order modes considered and second-order ones generated by self-coupling.
A.
CASE A: even-parity ℓ = |m| = 2 perturbations
and generated modes
As discussed in Appendix A, the self-coupling between
these modes generates second-order (ℓ = 4, m = ±4)
even-parity (polar) ones, whereas the coupling between
them (m = 2 with m = −2) gives rise to second-order
(ℓ = 4, m = 0), (ℓ = 2, m = 0) and (ℓ = 0, m = 0)
even-parity (polar) modes, and (ℓ = 3, m = 0) and (ℓ =
1, m = 0) odd-parity (axial) ones. Since this paper only
deals with different radiative aspects of the system, we
can ignore modes with ℓ < 2.
Furthermore, we assume that the Zerilli functions
{1} ±2
Ψ2 that describe the first-order (l = 2, m = ±2)
modes are real
Ψ±2
2 ∈ R.
{1}
(8)
This means that both modes are described by the
Power(robs , t) =
dE
ǫ2
∂t {1}Ψ22
=
dt
12π
2
+
∗
same function, since generically the relation ( {1}Ψm
l ) =
m {1} −m
(−1)
Ψl holds, and, in essence, the system reduces
to a problem of self-coupling. The second-order evenparity (polar) modes inherit this property, in such a way
that we only need three functions to describe them:
{ {2}Ψ02 ,
Ψ44 } .
{2}
Due to the assumption (8), none of the second-order
odd-parity (axial) modes are generated. This happens
because the source for a m = 0 mode must be real.
Schematically, the generic term of the source for this axial (l = 3, m = 0) mode can be written as i {1}Ψ22 {1}Ψ−2
2
and it is straightforward to see that its real part vanishes
under the assumption (8).
In this particular CASE A, the radiated power associated with the mentioned modes for a given observer
located at robs as a function of time is given by
9ǫ4 n
2 ∂t {2}Ψ44
640π
where ǫ is the perturbative parameter and all the expressions on the right-hand side are evaluated, naturally, at
(robs , t). In principle this equation is valid only at null
infinity but, as it is usually the case in computations, we
evaluate it at a finite radius.
Ψ04 ,
{2}
B.
2
+ ∂t {2}Ψ04
2
o
+
ǫ4
∂t {2}Ψ02
96π
2
+ O ǫ5
,
(9)
CASE B: odd-parity (ℓ = 2, m = 0) perturbations
and generated modes
In principle, following the selection rules, the odd parity (ℓ = 2, m = 0) mode would generate by self-coupling
5
Hence, none of the second-order odd-parity modes are excited and, up to this order, we are left with two radiative
second-order modes,
the second-order (ℓ = 0, m = 0), (ℓ = 2, m = 0)
and (ℓ = 4, m = 0) even-parity modes, as well as the
(ℓ = 1, m = 0) and (ℓ = 3, m = 0) odd-parity ones. However, in this axisymmetric case (m = 0 for all modes),
the Clebsch-Gordan-like coefficients that appear in the
sources {2}SΦ and {2}SΨ vanish for those second-order
modes with an odd harmonic label ℓ (see Appendix A).
3ǫ2
∂t {1}Φ02
Power(robs , t) =
32π
IV.
2
3ǫ4
+
32π
NUMERICAL APPROACH FOR SOLVING
THE MASTER EQUATIONS
We now describe in some detail our numerical approach
for evolving the first and second-order RWZ equations,
since in the past difficulties have been reported with the
high-order derivatives in the sources of these equations.
We numerically solve the first and second-order equations using a pseudo-spectral collocation method. The
spatial derivatives are computed using Chebyshev polynomials and Gauss-Lobatto (GL) collocation points, and
the system is evolved in time using a standard fourthorder Runge-Kutta scheme. We use a small enough
timestep for the time integration so that the solution
converges exponentially with the number of collocation
points (see below). The accuracy of all the simulations
presented in this paper are at the level of double precision
round-off.
GL collocation points are not equally spaced; instead,
they cluster near the edges of the computational domain
(equally spaced points would not give exponential convergence). For that reason it is standard to use a multidomain approach. Here we subdivide our radial domain
in (non-overlapping) blocks of length 10M each, communicated through a penalty technique. At the interface
each incoming characteristic mode u+ is penalized according to (see [49] and references therein)
αN 2 δ +
u˙+ = (. . .) −
(u − v + )
rblock
where v + is the value of the same mode at the interface
point using the neighboring block, rblock is the size of
the corresponding block (10M in these simulations), α
is the associated characteristic speed, N the number of
collocation points on that block and δ a penalty parameter chosen here to be δ = 0.6. At the outer boundary
each characteristic incoming mode is similarly penalized
to zero; though this is done simply to achieve stability, in
our simulations the domain is large enough that our results are causally disconnected from the outer boundary.
The singularity of the black hole is dealt with through
excision. That is, by using Kerr-Schild coordinates for
{ {2}Ψ04 ,
Ψ02 } .
{2}
The radiated power is then given by
3
∂t {2}Ψ04
20
2
1
+ ∂t {2}Ψ02
9
2
+ O(ǫ5 ).
(10)
the background spacetime and placing an inner boundary inside the event horizon.
As an example, Fig. 2 shows a self-convergence test for
the first-order (ℓ = 2 = m) Zerilli function, extracted at
r = 51.8M 3 , both changing the number of collocation
points as well as the timestep. The initial data used for
such test correspond to the same one used in Fig. 1,
Ψ22 = 0 ,
{1}
Ψ̇22 (t = 0, r) = e−(r−r0 )
{1}
2
/σ2
,
(11)
with σ = 4M , r0 = 20M , and the spatial domain r ∈
[1.8M, 301.8M ]. In Fig. 3 we also show the result of a
convergence test for the generated second order (ℓ = 4 =
m) Zerilli mode. From these figures we see that using
30 collocation points per domain and a timestep ∆t =
0.001M gives a numerical error at the level of double
precision round-off; from hereon we use such resolutions
for all our simulations.
In order to compare the magnitude of the errors with
the solutions themselves, in Fig. 4 we show the absolute values of the first-order {1}Ψ22 and second-order
{ {2}Ψ02 , {2}Ψ04 , {2}Ψ44 } Zerilli solutions from the previous
plots at their highest resolutions, all extracted at the
same observer location.
We note in passing that for most of the ringdown the
order of magnitude of the second-order Zerilli functions
appears to be comparable to (and in one case even larger
than) the first-order one. There is no contradiction in
this, since their contribution to the radiated energy is
scaled by ǫ4 , while the contribution of the first order Zerilli function is scaled by ǫ2 , see Eq. (9).
A.
Setup of numerical simulations
We could introduce non-vanishing second-order modes
via initial second-order perturbations. However, we are
interested in mode-mode coupling. Put differently, we
3
We place observers at the beginning/end of each domain:
1.8M, 11.8M, 21.8M , etc.
6
10-2
10-6
10-8
10-10
10-12
10-14
10-16
10-18
10-6
10-8
10-10
10-12
10-14
10-16
0
50
100
10-9
150
t/M
200
250
10-11
10-18
300
0
50
100
150
t/M
200
250
300
Figure 3: Numerical errors in the second-order Zerilli function
{2} 4
Ψ4 for different spatial resolutions and a fixed timestep
∆t = 0.001M . The errors are to be interpreted as in the
previous figures. For N = 30 (which are the ones used in the
rest of this paper) and higher, they are at the level of double
precision round-off.
∆t1=0.010 - ∆t4=0.0005
∆t2=0.005 - ∆t4=0.0005
∆t3=0.001 - ∆t4=0.0005
10-10
temporal resolution errors
N15 - N60
N20 - N60
N30 - N60
N40 - N60
10-4
numerical error in {2}Ψ
10-4
spatial resolution errors
10-2
N10 - N60
N15 - N60
N20 - N60
N30 - N60
N40 - N60
10-12
10-13
10-14
10-15
10-17
l=2, m=2
l=2, m=0
l=4, m=0
Ψ l=4, m=4
10-2
0
50
100
150
t/M
200
250
300
Figure 2: Numerical errors for different spatial resolutions
using a fixed timestep ∆t = 0.01M (top), and for different
timesteps using a fixed spatial resolution of N = 60 points per
domain (bottom). Both figures show the differences between
several resolutions and the most accurate one, which is N =
60 for the top panel and ∆t4 = 0.0005M for the bottom one.
In both cases the observer is located at r = 51.8M . We
see exponential convergence and errors in the order of double
precision round-off.
zerilli function
10-18
{1}
Ψ
{2}
Ψ
{2}
Ψ
{2}
100
10-16
10-4
10-6
10-8
10-10
0
50
100
150
t/M
200
2. Time Symmetric (TS)
In the following section we solve the first-order RWZ
equations with four different types of initial data, varying
both the location r0 and width σ of the initial data,
3. Approximately Outgoing (OUT)
Ψ22 (t = 0, r) = M e−(r−r0 )
{1}
Ψ̇22 (t
{1}
Ψ̇22 (t
Ψ̇22 (t
= 0, r) = e
/σ2
,
2
/σ2
,
= 0, r) = −(1 − 2M/r)∂r {1}Ψ22 (t = 0, r).
4. Approximately Ingoing (IN)
Ψ22 (t = 0, r) = 0 ,
{1}
2
= 0, r) = 0 .
Ψ22 (t = 0, r) = M e−(r−r0 )
{1}
{1}
{1}
2
−(r−r0 ) /σ
2
.
300
Figure 4: Absolute value of first and second-order Zerilli functions extracted at r = 51.8M .
are interested in the particular solution of Eqs. (7,6) (that
is, the one with vanishing initial data), since the homogeneous one will be exactly the same as at first order.
Therefore, in this paper we always impose vanishing initial data for all the second-order modes and concentrate
on those modes generated by first-order mode coupling.
1. Time Derivative (TD)
250
Ψ22 (t = 0, r) = M e−(r−r0 )
(12)
{1}
(13)
{1}
Ψ̇22 (t
2
/σ2
= 0, r) = (1 − 2M/r)∂r
,
Ψ22 (t = 0, r).
{1}
7
V. DECAY FREQUENCIES OF
SECOND-ORDER PERTURBATIONS
{1}
Ψ
{2}
Ψ
source
10-5
{1}
10-10
10-15
ingoing ID
10-20
0
50
100
150
200
250
300
t/M
{1}
Ψ
{2}
Ψ
source
10-5
10-10
{1}
Ψ, {2}Ψ, source
100
10-15
outgoing ID
10-20
0
50
100
150
t/M
200
300
{1}
Ψ
{2}
100
Ψ
source
10-5
10-10
{1}
Ψ, {2}Ψ, source
250
10-15
time-derivative ID
10-20
0
50
100
150
200
250
300
t/M
{1}
Ψ
{2}
Ψ
source
Ψ, {2}Ψ, source
100
10-5
10-10
{1}
Ioka and Nakano have put forward the suggestion that
at second order new frequencies should appear in the
ringdown spectrum, which would be given by the sum of
different pairs of standard QNM frequencies. In particular, according to this prediction, the dominant frequency
would correspond to the double of the standard fundamental one from linearized theory [40, 41]. This seems
reasonable, since the sources for the second-order master equations are quadratic in the first-order modes, so
one might well expect that frequencies get summed-up
in Fourier space. The physical picture, however, appears
to be at the same time more subtle and simpler: our numerical simulations indicate that in practice second-order
perturbations decay with the standard QNM frequencies
from linearized theory.
Recall that the physical process here studied is the coupling of linear modes. That is, we initialize all secondorder perturbations to zero. The second-order master equations have sources which are, indeed, quadratic
in the first-order modes. What we observe in all our
simulations, though, is that those sources quickly excite the second-order perturbations and afterwards decay
very fast in time. As a consequence, once the secondorder modes have been excited and reached the regime
in which they oscillate with a constant complex frequency (i.e. what in linearized theory corresponds to the
QNM regime), they essentially propagate with a vanishing source. In other words, as first-order perturbations
do. And, in particular, they do oscillate and decay with
the same, standard, QNM frequencies from linearized
perturbation theory.
We show this behavior in some detail for the four initial data types (Sec. IV A) of CASE A perturbations
(Sec. III A), with r0 = 20M and σ = 4M . Figure 5 shows
the first-order Zerilli function and the (ℓ = 2, m = 0)
second-order one for different initial data profiles. In all
cases the source decays much faster than the second-order
solution itself and therefore its role in determining the behavior of the latter by the time it enters the QNM regime
is negligible. From the same figure one can notice that
the type of initial perturbation does determine the time
by which the second-order Zerilli function enters the tail
regime; but this is not surprising, since it already happens for the first-order one.
In order to gain further insight into these observations
we display the dynamics of first and second-order Zerilli
functions and the source term {2}SΨ of Eq. (7), now for
the (ℓ = 4, m = 0) second-order mode. Fig. 6 shows
these three quantities as functions of radius at different
times. The source term is dominant only during the first
∼ 20M , later decaying at a fast rate to several orders of
magnitude below the second-order Zerilli function.
Table II shows the fitted QNM frequencies from our
numerical data, for the different initial-data profiles of
CASE A perturbations, with r0 = 20M and σ = 4M .
Ψ, {2}Ψ, source
100
10-15
time-symmetric ID
10-20
0
50
100
150
200
250
300
t/M
Figure 5: CASE A simulations: first-order (ℓ = 2, m = 2)
Zerilli function and second-order (ℓ = 2, m = 0) one, along
with the source term for the second-order master equation
[Eq. (7)], as functions of time for different initial data profiles.
The source plays a role only at very early times in exciting
the second-order modes, afterwards being much smaller than
the first and second- order solutions.
8
102
{1}
Ψ
{2}
Ψ
source
function absolute value
100
-2
10
10-4
10-6
ID
TD
TS
IN
OUT
ℓ = 4, m = 0
0.80916 − 0.09418i
0.80920 − 0.09420i
0.80918 − 0.09416i
0.80931 − 0.09425i
2nd order
ℓ = 2, m = 0
err %
0.37334 − 0.08883i 0.1
0.37335 − 0.08766i 0.3
0.37373 − 0.08945i 0.1
0.37074 − 0.08902i 0.8
10-10
t=0M
-14
10
0
10
20
30
40
50
r/M
102
{1}
Ψ
{2}
Ψ
source
100
function absolute value
1st order
ℓ = 2, m = 2
err %
0.37077 − 0.08826i 0.8
0.37353 − 0.08837i 0.2
0.37061 − 0.08887i 0.8
0.37107 − 0.08624i 1.0
10-8
10-12
10-2
10-4
10-6
10-8
10-10
10-12
10-14
t = 12 M
0
10
20
30
40
50
r/M
102
{1}
Ψ
{2}
Ψ
source
100
function absolute value
ID
TD
TS
IN
OUT
10-2
10-4
10-6
10-8
10-10
10-12
10-14
t = 24 M
0
10
20
30
40
50
r/M
Figure 6: CASE A simulations: snapshots of the first-order
Zerilli function and second order (ℓ = 4, m = 0) one, along
with the source term, for ingoing initial data. The generic
behavior of the source is to rapidly decrease several orders of
magnitude below the solutions themselves. [Note: In the first
snapshot the second-order Zerilli function vanishes because it
corresponds to t = 0 and our setup of the physical problem.]
They agree quite well with those predicted by first-order
theory for each of those modes.
As described in Sec. IV, our numerical simulations are
of very high accuracy (both at first and second-order): all
the errors are at the level of double precision round-off,
∼ 10−14 −10−12 (see Figs. 2,3). Therefore, we do not consider lack of resolution as a possible reason for not finding
traces of the predicted new second-order QNM frequen-
2nd order
err %
ℓ = 4, m = 4
0.003 0.80916 − 0.09418i
0.005 0.80920 − 0.09420i
0 0.80918 − 0.09416i
0.019 0.80931 − 0.09425i
err %
0.003
0.005
0
0.019
Table II: Measured quasinormal frequencies from our numerical simulations (CASE A). They agree with those predicted by
linearized theory, even for the second-order modes generated
due to mode-mode coupling. The predicted QNM frequencies
from standard linearized perturbation theory, as quoted in
[15], are 0.37367 − 0.08896i for ℓ = 2 and 0.80918 − 0.09416i
for ℓ = 4 (in linearized theory there is degeneracy with respect to the azimuthal index m. The relative errors for real
and imaginary parts of the measured frequencies ω are computed as |ω − ωexact |/|ωexact |.
cies in our simulations. Similarly, one might think that
those predicted frequencies are in fact present, but with a
very small amplitude. Figure 7 indicates that in practice
that does not seem to be the case: the residual of the fit
for the second-order Zerilli function [in the case shown it
is the (ℓ = 2, m = 0) one, for TD initial data, first-order
perturbations] —defined as the function minus its fit—
does not appear at all to correspond to an oscillation
and decay with twice the standard complex fundamental
quasinormal frequency for that mode (or to an overtone).
Instead, it appears to be the residual associated with the
fact that QNMs are not complete.
For completeness, in Appendix B we provide results
of the fitted frequencies for the four initial data types of
CASE A perturbations, now varying both the location
and width of the initial data; all of them support the
same conclusion.
Finally, we briefly discuss the results of some CASE
B [odd-parity (ℓ = 2, m = 0) first-order mode] perturbations, since the conclusions are identical. As discussed
in Sec. III B and summarized in Table I, they generate
both (ℓ = 4, m = 0) and (ℓ = 2, m = 0) even-parity
second-order modes. The fitted frequencies from the numerical solutions (for a simulation of TD linear initial
data with r0 = 20M and σ = 4M ) for these secondorder modes yield, respectively, 0.37441 − 0.08921i and
0.80932 − 0.09419i, to be compared with the expected
values from perturbation theory: 0.37367 − 0.08896i for
ℓ = 2 and 0.80918 − 0.09416i for ℓ = 4.
9
100
NSF PHYS 0925345, 0941417, 0903973, 0955825 to
Georgia Tech, the Spanish MICINN Project FIS200806078-C03-03, the French A.N.R. Grant LISA Science
BLAN07-1 201699, and by the Deutsche Forschungsgemeinschaft (DFG) through SFB/TR 7 “Gravitational
Wave Astronomy”.
residual
solution
-1
absolute value
10
10-2
10-3
10-4
10-5
10-6
120
130
140
150
160
We thank Emanuele Berti, Vitor Cardoso, Chad Galley and Bence Kocsis for helpful discussions and suggestions. We also thank Carlos Ann for inspiration, Tryst
DC –where parts of this work were done– for hospitality,
and Eric Cartman for proof-reading the manuscript and
providing critical comments.
t/M
Figure 7: Residual from fitting a second-order Zerilli function
to a complex frequency mode. The fitted frequency corresponds to the standard fundamental quasinormal one for that
multipole index, and the residual does not appear to contain
traces of twice that frequency (or any other).
VI.
FINAL REMARKS
In this paper we have numerically evolved first and
second-order self-generated gauge-invariant gravitational
perturbations of Schwarzschild black holes with a variety
of initial data sets, studying the oscillation and decay behavior of nonlinear modes and, more specifically, whether
they correspond to the standard QNM frequencies or to
a different spectrum. We have found, in all cases, that
second-order modes decay through the standard QNM
frequencies, and that the picture behind this is remarkably simple: first-order perturbations trigger high-order
ones through source terms which afterwards rapidly decay in time. Besides, by the time the solutions reach the
regime in which they oscillate and decay at a constant
rate (the QNM regime in the case of linearized perturbations), the second-order modes for all practical purposes
propagate as in linearized theory.
Mode-mode coupling in the ringdown of black holes has
been previously studied through numerical simulations of
full Einstein equations [50, 51]; however, no conclusions
seem to have reached or sought for in terms of the deviations in the ringdown spectrum from the linearized one
(presumably due to lack of resolution).
The fact that nonlinear aspects of Einstein’s equations
in the ringdown of black holes appear to already be captured —at least in what oscillation and decay frequencies
concerns— by linearized perturbation theory is somehow
remarkable and should be of use both for modeling black
holes in the ringdown regime as well as in data analysis
searches of gravitational waves.
Acknowledgments
This research has been supported in part by NSF
Grant PHYS 0801213 to the University of Maryland,
Appendix A: Mode coupling: selection rules
In this appendix we summarize, for completeness, the
selection rules for mode coupling [45, 46]. A second-order
(l, m)-mode gets a contribution from a pair of first-order
modes (l̂, m̂) and (l̄, m̄) if three conditions are obeyed.
First, the harmonic labels must be related by the usual
composition formulas
|l̂ − ¯l| ≤ l ≤ ˆl + ¯l,
and m̂ + m̄ = m.
(A1)
Second, mode coupling must conserve parity. To any harmonic coefficient with label l, we associate a polarity sign
σ such that, under parity, the harmonic changes by a sign
σ(−1)l . Polar/even parity (axial/odd parity) harmonics
have σ = +1 (σ = −1). Then, parity conservation implies the third condition:
(−1)l̄+l̂−l = σσ̄σ̂,
(A2)
where σ̂ and σ̄ are the polarity signs corresponding to
the modes (l̂, m̂) and (l̄, m̄) respectively. In particular,
there is a special case in which the coupling of two modes
satisfying Eqs. (A1) and (A2) does not contribute to a
second-order mode, and the reason comes from the properties of the Clebsch-Gordan-like coefficients that appear
in the product formula for the tensor harmonics [45].
In axisymmetry (m̄ = m̂ = 0) the mentioned ClebschGordan-like coefficients vanish if ¯l + ˆl + l is odd.
This analysis can be extended to higher orders. In
particular, the parity condition implies that a collection
of k modes with harmonic labels {l1 , ..., lk } and polarities {σ1 , ..., σk } contributes to the mode (l, σ) only if
(−1)l σ = Πki=1 (−1)li σi .
10
Appendix B: Numerical decay frequencies of second-order perturbations from time domain simulations
r0
20
40
60
80
100
ℓ = 2, m = 0
0.37373 − 0.08949i
0.37147 − 0.08833i
0.37141 − 0.08834i
0.37102 − 0.08839i
0.37101 − 0.08840i
Ingoing
ℓ = 4, m = 0
0.80918 − 0.09416i
0.80916 − 0.09417i
0.80915 − 0.09413i
0.80917 − 0.09415i
0.80888 − 0.09414i
ℓ = 4, m = 4
0.80918 − 0.09416i
0.80916 − 0.09417i
0.80915 − 0.09413i
0.80917 − 0.09415i
0.80872 − 0.09417i
ℓ = 2, m = 0
0.37074 − 0.08902i
0.37079 − 0.08891i
0.37093 − 0.08844i
0.37140 − 0.08816i
0.37148 − 0.08782i
Outgoing
ℓ = 4, m = 0
0.80931 − 0.09425i
0.80911 − 0.09409i
0.80911 − 0.09417i
0.80913 − 0.09413i
0.80914 − 0.09426i
ℓ = 4, m = 4
0.80931 − 0.09425i
0.80911 − 0.09409i
0.80911 − 0.09417i
0.80913 − 0.09413i
0.80914 − 0.09426i
σ
2 0.37708 − 0.09116i 0.80918 − 0.09418i 0.80918 − 0.09418i 0.37365 − 0.08891i 0.80918 − 0.09416i 0.80918 − 0.09416i
4 0.37373 − 0.08949i 0.80919 − 0.09417i 0.80918 − 0.09417i 0.37079 − 0.08902i 0.80931 − 0.09425i 0.80911 − 0.09409i
8 0.37286 − 0.08893i 0.80875 − 0.09407i 0.80875 − 0.09407i 0.36887 − 0.08284i 0.80923 − 0.09599i 0.80921 − 0.09599i
r0
20
40
60
80
100
ℓ = 2, m = 0
0.37334 − 0.08883i
0.37277 − 0.08893i
0.37378 − 0.08921i
0.37383 − 0.08995i
0.37387 − 0.08999i
Time Derivative
ℓ = 4, m = 0
0.80916 − 0.09418i
0.80919 − 0.09417i
0.80920 − 0.09418i
0.80915 − 0.09411i
0.80914 − 0.09409i
ℓ = 4, m = 4
0.80916 − 0.09418i
0.80919 − 0.09417i
0.80920 − 0.09418i
0.80915 − 0.09411i
0.80914 − 0.09409i
ℓ = 2, m = 0
0.37335 − 0.08766i
0.37376 − 0.08984i
0.37267 − 0.08948i
0.37344 − 0.08852i
0.37321 − 0.08823i
Time symmetric
ℓ = 4, m = 0
0.80920 − 0.09420i
0.80915 − 0.09413i
0.80917 − 0.09416i
0.80917 − 0.09413i
0.80923 − 0.09422i
ℓ = 4, m = 4
0.80920 − 0.09420i
0.80915 − 0.09413i
0.80917 − 0.09416i
0.80917 − 0.09413i
0.80923 − 0.09422i
σ
2 0.37360 − 0.08906i 0.80917 − 0.09417i 0.80917 − 0.09417i 0.37404 − 0.08972i 0.80917 − 0.09416i 0.80916 − 0.09416i
4 0.37334 − 0.08893i 0.80916 − 0.09417i 0.80916 − 0.09418i 0.37335 − 0.08766i 0.80920 − 0.09420i 0.80920 − 0.09420i
8 0.37315 − 0.08935i 0.80924 − 0.09342i 0.80924 − 0.09334i 0.37943 − 0.08760i 0.80867 − 0.09424i 0.80867 − 0.09423i
Table III: For ℓ = 2 the expected fundamental frequency from linearized theory is 0.37367 − 0.08896i, while for ℓ = 4 frequency
it is 0.80918 − 0.09416i [15]. Shown are the fitted values from our numerical solutions to the second order Zerilli equations,
for four different sets of initial data. For each initial data configuration we vary the location r0 and width σ of the linearized
perturbations, keeping one fixed (r0 = 20M and σ = 4M , respectively) while varying the other. The fitted frequencies appear
to be insensitive to the choice of initial data and agree with the QNM frequencies from linearized perturbation theory.
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