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Quasinormal Ringing ofAcoustic Black Holes
京都大学大学院 人間・環境学研究科宇宙論・重力グループ M2
奥住 聡
共同研究者:阪上雅昭(京大 人・環) , 吉田英生(京大 工)
What is an Acoustic Black Hole?
“Acoustic BH” = Transonic Flow
down 1|| M1|| M 1|| M up
sonic point
effsc
velocityfluid:
velocitysound:
v
cs
)1(eff Mccvc sss
“effective” sound velocity in the lab
Acoustic BH region
In the supersonic region,sound waves cannot propagate against the flow.
= sonic horizon
“ Acoustic Black Hole”
0 scv0 scv0 scv
throat
“Laval Nozzle”:Convergent-Divergent Nozzle
THEORY
Graduate School of H&E Studies
EXPERIMENT
Graduate School of Engineering
TARGETS• Hawking Radiation
• Quasinormal Ringing
numerical
Planckian fit
Acoustic BH Experiment Project at Kyoto Univ.
compressor
mass flow meter
settling chamber
Laval nozzle
flow
20cm
Configuration
Quasinormal Ringing
“Characteristic ‘sound’ of BHs (and NSs)”
occurs when the geometry around a BH is perturbed
and settles down into its stationary state.
e.g. after BH formation / test particle infall
Described as a superposition of a countably infinite number
of damped sinusoids (QuasiNormal Modes, QNMs).
QNM frequencies contain the information on (M,J) of BHs.
Quasinormal Ringing of a BH
NS-NS merger to a BH (Shibata & Taniguchi, 2006)
QN ringing
inspiral phase merger phase
Definition of QNMs
Schroedinger-type wave eq. outgoing BCswith
QNMs are defined as solutions of
horizon
infinity
solutions:
n: complex
Example: Schwarzschild Black Hole
horizon
spatial infinity
Example: Schwarzschild Black Hole
~ rg-2
Example: Schwarzschild Black Hole
fundamental (n=0) mode
Goal of This Study
What form of nozzle yield the QNM easiest to observe?A measure of the detectability: “Q-value”
Are QNMs excited in experimentally feasible situations?
Numerical simulation (full order calculation)
Find the form of the nozzle which yield large Q
Experimental testing of gravitational-wave analysis
(such as matched filtering)
Does acoustic BH really have QNMs?
Questions
-- wave eq. for velocity potential perturbation
Sound Waves in Inhomogeneous Fluid Flow
Perturbation:
1D flow approx.:
Schroedinger-type Wave Equation
cs0: sound speed at stagnation points
, v, A : independent of t
M : Mach number
where
“effective potential”
Potential Barrier for Different Laval Nozzles
Consider a family of Laval nozzle:
nozzle radius
K : integer
r
tank 1 tank 2nozzleflow
Potential Barrier for Different Laval Nozzles
1.04L
3.92L-2
11.4L-2
1.19L
flow
sonic horizon
flow
sonic horizon
Procedure for Calculating QN Freq’s
Calculate the “S-matrix” for the potential barrier V():
Then, impose the outgoing B.C. ,
and find ’s that satisfy the boundary condition.
: “S-matrix”
WKB Approach
0
Region (I) & (III): WKB solutions for truncated V() Around : exact solution for truncated V()
Expand V() in a Taylor series about the maximum point 0:
(I)
(II) (III)
1st order: Schutz & Will, 1985
3rd order: Iyer & Will, 1987
6th order: Konoplya, 2004
Matching
matching regions2312
WKB Approach: S-Matrix
Here, is related to by
where
(1st WKB)
QNM Solutions by WKB Approach
Conditions for QNMs:
i.e.
QNM frequency
(1st WKB value)
QNM Frequencies of Different Laval Nozzles
(WKB approx.breaks down)
Q = 2
Q = 1
WKB solution:Schutz & Will (1985)Iyer & Will (1987)
: peak point of V
n=0 mode freq.
(3rd WKB value)
Numerical Simulation of Acoustic QN Ringing
We perform two types of simulations:
“Acoustic BH Formation”
initial state: no flow
set sufficiently large pressure difference
final state: transonic flow
“Weak Shock Infall”
initial state: transonic flow
let a weak shock “fall” into the horizon
final state: transonic flow
~ BH formation ~ test particle infall
flow
Example of Transonic Flow
flow
sonic horizonsupersonic subsonic
Result 1: Weak Shock Infall
steady shock
horizon
gif
weak shock
Result 1: Weak Shock Infall
steady shock
horizon
weak shock
QN ringing
gif
QNM fit(3rd WKB)
numerical
ringdown phase
observed waveform
Result 1: Weak Shock Infall
QNM fit(3rd WKB)
numerical
nonlinear phase
ringdown phase
Result 2: Acoustic BH Formation
observed waveform
QNM fit (3rd WKB)
numerical
nonlinear phase
ringdown phase
Result 2: Acoustic BH Formation
observed waveform
Numerical waveform agrees with the least damped QNM very well!
Numerical Simulation: Discussion
In both types of simulations, QNMs are actually excited.
The results agree with WKB analysis well ( for K
>1 ).Typical values in laboratories:
cf. real BH:(l=m=2, least-
damped)>2.0
LN
0~L
cs
QNMs of acoustic BHs decay too quickly. Difficult to detect in experiments…?
Partially Reflected Quasinormal Modes (PRQNMs)
outgoing B.C. + “half mirror” B.C.
“half mirror”
c
Example: Contact Surface in Perfect Fluid
Contact surface (contact discontinuity):• discontinuity of the density .
• the pressure p and the fluid velocity v are continuous.
• moves with the surrounding fluid, i.e., vc= v .
• partially reflects sound waves.
vcv v
1 2
Contact Surface(C.S.)
Example: Contact Surface in Perfect Fluid
vcv v
1 2
If vc(= v) << cs ,
refl. coeff. R() for sound waves propagating from 1 to 2is given by [e.g. Landau & Lifshitz, Fluid Mechanics]
C.S.
PRQNM Solutions by WKB Approach
Partially Reflecting B.C. :
Example: Contact Surface in Perfect Fluid
Re ReIm Im
Table: the least damped PRQNM frequency (3rd WKB value)
contact surface enhances Q-value!!
observed waveform
PRQNM fit (3rd WKB)
numerical
Numerical Simulation of PRQNMs
Numerical Simulation of PRQNMs
no contact surface contact surface present
SummaryFor future experiments, we have studied QN ringing of acoustic BHs in Laval nozzles.
A contact surface elongates the damping times of QNMs.
Acoustic BHs (transonic fluid flow) do have QNMs.
QNMs are excited in experimentally feasible situations.
A wider range of Q becomes accessible!
Experimental testing of gravitational-wave analysis(such as matched filtering) .Astrophysical BH surrounded by a “half mirror” ??
Future Works
PRQNM Solutions by WKB ApproachIn region (III),
right-going WKB sol.
left-going WKB sol.
c
region (III) region (IV)
23
PRQNM Solutions by WKB ApproachIn region (III),
right-going WKB sol.
left-going WKB sol.
Furthermore, if clies far away from the potential barrier,
QNM fit
PRQNM fit
Numerical Simulation of PRQNMs
For t <15, an “ordinary” QNM (not PRQNM) dominates,
since the potential barrier is not yet “aware”
of the contact surface.