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Recent developments in binary black holeevolutions
Peter Diener
Center for Computation and Technology
and
Department of Physics and Astronomy
Louisiana State University
With: M. Alcubierre, B. Brugmann, F. Guzman, I. Hawke,
S. Hawley, F. Herrmann, M. Koppitz, D. Pollney, E. Seidel,
R. Takahashi, J. Thornburg & J. Ventrella
November 3, 2005
Numrel 2005, NASA Goddard, November 3, 2005 1
Outline
• Quasi-circular binary black hole sequences
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
• FMR (Carpet)
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
• FMR (Carpet)
• New gauge parameter
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
• FMR (Carpet)
• New gauge parameter
• The battle of the gauges
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
• FMR (Carpet)
• New gauge parameter
• The battle of the gauges
• Convergence
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
• FMR (Carpet)
• New gauge parameter
• The battle of the gauges
• Convergence
• Improving the gauge
Numrel 2005, NASA Goddard, November 3, 2005 2
Outline
• Quasi-circular binary black hole sequences
• Unigrid simulations
• FMR (Carpet)
• New gauge parameter
• The battle of the gauges
• Convergence
• Improving the gauge
• Conclusions
Numrel 2005, NASA Goddard, November 3, 2005 2
Quasi-circular binary black hole sequences
0
20
40
60
80
100
120
140
4 5 6 7 8 9 10 11 12
P (M
AD
M)
L (MADM)
Cook sequenceMeudon sequence
T-B sequenceCook ISCO
Meudon ISCOT-B ISCO
0.75
0.8
0.85
0.9
0.95
1
0.05 0.1 0.15 0.2 0.25
J/M
AD
M2
MADM Ω
Grandclement et al. (2002)Cook (1994)
Baumgarte (2000)Tichy et al. (2004)
1PN (corot)1PN (irrot)
2PN (corot)2PN (irrot)
3PN (corot)3PN (irrot)
Numrel 2005, NASA Goddard, November 3, 2005 3
Unigrid simulations INumerical evolutions of the Cook-Baumgarte quasi-circular sequence (QC-0: L =4.99M to QC-4: L = 7.84M .
Numrel 2005, NASA Goddard, November 3, 2005 4
Unigrid simulations INumerical evolutions of the Cook-Baumgarte quasi-circular sequence (QC-0: L =4.99M to QC-4: L = 7.84M .Ingredients in the numerical code:
• BSSN evolution system, 1+log slicing and Γ-driver shift + an additional co-rotating shift to keep the black holes in place.
Numrel 2005, NASA Goddard, November 3, 2005 4
Unigrid simulations INumerical evolutions of the Cook-Baumgarte quasi-circular sequence (QC-0: L =4.99M to QC-4: L = 7.84M .Ingredients in the numerical code:
• BSSN evolution system, 1+log slicing and Γ-driver shift + an additional co-rotating shift to keep the black holes in place.
• Second order spatial finite differencing and a 3-step iterative Crank-Nicholsontime evolution scheme. For each model dx = 0.08M and dx = 0.06M . ForQC-0 additionally dx = 0.048M
Numrel 2005, NASA Goddard, November 3, 2005 4
Unigrid simulations INumerical evolutions of the Cook-Baumgarte quasi-circular sequence (QC-0: L =4.99M to QC-4: L = 7.84M .Ingredients in the numerical code:
• BSSN evolution system, 1+log slicing and Γ-driver shift + an additional co-rotating shift to keep the black holes in place.
• Second order spatial finite differencing and a 3-step iterative Crank-Nicholsontime evolution scheme. For each model dx = 0.08M and dx = 0.06M . ForQC-0 additionally dx = 0.048M
• “Lego-excision” with the “simple excision” boundary treatment.
Numrel 2005, NASA Goddard, November 3, 2005 4
Unigrid simulations INumerical evolutions of the Cook-Baumgarte quasi-circular sequence (QC-0: L =4.99M to QC-4: L = 7.84M .Ingredients in the numerical code:
• BSSN evolution system, 1+log slicing and Γ-driver shift + an additional co-rotating shift to keep the black holes in place.
• Second order spatial finite differencing and a 3-step iterative Crank-Nicholsontime evolution scheme. For each model dx = 0.08M and dx = 0.06M . ForQC-0 additionally dx = 0.048M
• “Lego-excision” with the “simple excision” boundary treatment.
• Sommerfeld out-going radiation boundary condition. Due to the constraintviolation introduced by this boundary condtion we use a “fish-eye” coordinatetransformation to push the boundaries far enough out, that the horizon region iscausally disconnected from the boundaries at time of common horizon formation.
Numrel 2005, NASA Goddard, November 3, 2005 4
Unigrid simulations INumerical evolutions of the Cook-Baumgarte quasi-circular sequence (QC-0: L =4.99M to QC-4: L = 7.84M .Ingredients in the numerical code:
• BSSN evolution system, 1+log slicing and Γ-driver shift + an additional co-rotating shift to keep the black holes in place.
• Second order spatial finite differencing and a 3-step iterative Crank-Nicholsontime evolution scheme. For each model dx = 0.08M and dx = 0.06M . ForQC-0 additionally dx = 0.048M
• “Lego-excision” with the “simple excision” boundary treatment.
• Sommerfeld out-going radiation boundary condition. Due to the constraintviolation introduced by this boundary condtion we use a “fish-eye” coordinatetransformation to push the boundaries far enough out, that the horizon region iscausally disconnected from the boundaries at time of common horizon formation.
• Apperent-, event- and isolated-horizon analysis.
Numrel 2005, NASA Goddard, November 3, 2005 4
Unigrid simulations II
0
10
20
30
40
50
60
70
80
90
5 6 7 80.0
0.2
0.4
0.6
0.8
1.0tim
e (M
)
t/tor
bit
initial proper separation of AHs (M)
torbit (left scale)tAH (left scale)
tAH/torbit (right scale)
Numrel 2005, NASA Goddard, November 3, 2005 5
Unigrid simulations III
Initial values: MADM = 1.01 and (J/M2)ADM = 0.779.
dx 0.080 0.060 0.048
a/m 0.450± 0.021 0.572± 0.025 0.632± 0.028Mirr 0.947 0.933 0.923
MAH 0.973± 0.003 0.978± 0.005 0.980± 0.006Jrad (%) 45.3± 2.9 29.6± 3.7 22.1± 4.5Erad (%) 3.61± 0.25 3.12± 0.45 2.97± 0.59TAH 15.72 16.53 17.11
Lazarus results (Baker et. al. 2001, 2002): Erad = 3% and
Jrad = 12%
Numrel 2005, NASA Goddard, November 3, 2005 6
FMR (Carpet)Basic grid setup:
• 8 levels of refinement.
• Rotating quadrant symmetry.
• Boundaries at 96M .
• Resolution on finest grid 0.025M .
• Fourth order finite differencing (except
shift advection terms).
• RK3 time integrator.
• 3rd order prolongation in space.
• 2nd order prolongation in time.
• Fixed size excision region.
Numrel 2005, NASA Goddard, November 3, 2005 7
New gauge parameterLapse:
∂tα = −2αψn(K −K0).
Numrel 2005, NASA Goddard, November 3, 2005 8
New gauge parameterLapse:
∂tα = −2αψn(K −K0).
Gamma driver shift:
∂tβi =
34αm
ψkBi,
∂tBi = ∂tΓi−αpηBi.
Numrel 2005, NASA Goddard, November 3, 2005 8
New gauge parameterLapse:
∂tα = −2αψn(K −K0).
Gamma driver shift:
∂tβi =
34αm
ψkBi,
∂tBi = ∂tΓi−αpηBi.
Drift correct:
The time derivative of the shift is
adjusted dynamically based on the
motion of the centroid of the apparent
horizon.
The angular and radial adjustments
are independently controlled by damped
harmonic oscillators where parameters
determine the damping time scales.
Numrel 2005, NASA Goddard, November 3, 2005 8
New gauge parameterLapse:
∂tα = −2αψn(K −K0).
Gamma driver shift:
∂tβi =
34αm
ψkBi,
∂tBi = ∂tΓi−αpηBi.
Drift correct:
The time derivative of the shift is
adjusted dynamically based on the
motion of the centroid of the apparent
horizon.
The angular and radial adjustments
are independently controlled by damped
harmonic oscillators where parameters
determine the damping time scales.
Gauge choice 1: n = 4, η = 2, p = 4, m = 1 and k = 2.
Gauge choice 2: n = 0, η = 4, p = 1, m = 1 and k = 2.
Numrel 2005, NASA Goddard, November 3, 2005 8
The battle of the gaugesFor Tichy-Brugmann sequence (D = 3.0)
0
2
4
6
8
10
0 20 40 60 80 100 120 140
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx =0.025Gauge 2, dx =0.025
Found common AH at T = 135M .
Numrel 2005, NASA Goddard, November 3, 2005 9
The battle of the gauges II
Numrel 2005, NASA Goddard, November 3, 2005 10
The battle of the gauges II
How can different gauges give so
different results?
Numrel 2005, NASA Goddard, November 3, 2005 10
The battle of the gauges II
How can different gauges give so
different results?
Remember that Brugmann et. al
evolved this data set for more than
140M without finding a common
apparent horizon.
Numrel 2005, NASA Goddard, November 3, 2005 10
The battle of the gauges II
How can different gauges give so
different results?
Remember that Brugmann et. al
evolved this data set for more than
140M without finding a common
apparent horizon.
Can the results be reconciled?
Numrel 2005, NASA Goddard, November 3, 2005 10
The battle of the gauges II
How can different gauges give so
different results?
Remember that Brugmann et. al
evolved this data set for more than
140M without finding a common
apparent horizon.
Can the results be reconciled?
To investigate this we decided
to perform several runs for each
gauge parameter set with different
resolutions.
Numrel 2005, NASA Goddard, November 3, 2005 10
Convergence
0
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0 20 40 60 80 100 120 140
Sca
led
diffe
renc
e
Time (MADM)
low-medium4 (medium-high)
Numrel 2005, NASA Goddard, November 3, 2005 11
Convergence II
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.02
Gauge 1, dx = 0.018Gauge 1, dx = 0.015Gauge 2, dx = 0.025Gauge 2, dx = 0.02
Gauge 2, dx = 0.018Gauge 2, dx = 0.015
Numrel 2005, NASA Goddard, November 3, 2005 12
Convergence II
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.02
Gauge 1, dx = 0.018Gauge 1, dx = 0.015Gauge 2, dx = 0.025Gauge 2, dx = 0.02
Gauge 2, dx = 0.018Gauge 2, dx = 0.015
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.02
Gauge 1, dx = 0.018Gauge 1, dx = 0.015Gauge 2, dx = 0.025Gauge 2, dx = 0.02
Gauge 2, dx = 0.018Gauge 2, dx = 0.015
Gauge 1, Rich. extrap.
Numrel 2005, NASA Goddard, November 3, 2005 12
Convergence II
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.02
Gauge 1, dx = 0.018Gauge 1, dx = 0.015Gauge 2, dx = 0.025Gauge 2, dx = 0.02
Gauge 2, dx = 0.018Gauge 2, dx = 0.015
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.02
Gauge 1, dx = 0.018Gauge 1, dx = 0.015Gauge 2, dx = 0.025Gauge 2, dx = 0.02
Gauge 2, dx = 0.018Gauge 2, dx = 0.015
Gauge 1, Rich. extrap.
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.02
Gauge 1, dx = 0.018Gauge 1, dx = 0.015Gauge 2, dx = 0.025Gauge 2, dx = 0.02
Gauge 2, dx = 0.018Gauge 2, dx = 0.015
Gauge 1, Rich. extrap.Gauge 2, Rich. extrap.
Numrel 2005, NASA Goddard, November 3, 2005 12
Convergence III
We assume that the properdistance as a function of time and
resolution is given by:
D(∆, t) = D(0, t) + a(t)∆2 + b(t)∆3.
Then given runs at 3 different resolutions, ∆1, ∆2, ∆3, we get:
D(∆1, t) = D(0, t) + a(t)∆21 + b(t)∆3
1,
D(∆2, t) = D(0, t) + a(t)∆22 + b(t)∆3
2,
D(∆3, t) = D(0, t) + a(t)∆23 + b(t)∆3
3,
which can be solved for D(0, t), a(t) and b(t).
Numrel 2005, NASA Goddard, November 3, 2005 13
Convergence IV
0
2
4
6
8
10
0 20 40 60 80 100 120 140
Pro
perd
ista
nce
Time (MADM)
Gauge 1, Rich. extrap.Gauge 1, pred. dx = 0.0125
Gauge 1, dx = 0.0125Gauge 2, Rich. extrap.
Gauge 2, pred. dx = 0.0125Gauge 2, dx = 0.0125
To get less than 1% error we estimate dx = M/200.
Numrel 2005, NASA Goddard, November 3, 2005 14
Improving the gauge
We realized that the damping
timescale for the drift correction
was not chosen optimally.
Recently Ryoji has experimented
with different damping timescales
(critical- or overdamping).-0.05
0
0.05
0.1
0.15
0.2
0.25
0.3
2.84 2.86 2.88 2.9 2.92 2.94 2.96 2.98 3 3.02 3.04
y
x
Gauge 1, dx = 0.018Gauge 2, dx = 0.018
Numrel 2005, NASA Goddard, November 3, 2005 15
Improving the gauge
0
2
4
6
8
10
0 20 40 60 80 100 120 140 160
Pro
perd
ista
nce
Time (MADM)
Gauge 1, dx = 0.025Gauge 1, dx = 0.0125
Gauge 1, Richardson extrapolatedImproved gauge, dx = 0.025Improved gauge, dx = 0.02
Improved gauge, dx = 0.015
Numrel 2005, NASA Goddard, November 3, 2005 16
Conclusions
• We have shown that even though 2 somewhat different gauge choices at a givenresolution may give very different answers they actually do converge to the sameresult.
Numrel 2005, NASA Goddard, November 3, 2005 17
Conclusions
• We have shown that even though 2 somewhat different gauge choices at a givenresolution may give very different answers they actually do converge to the sameresult.
• The data set from Brugmann et. al (2004) has been confirmed to actuallyperform more than an orbit before merger.
Numrel 2005, NASA Goddard, November 3, 2005 17
Conclusions
• We have shown that even though 2 somewhat different gauge choices at a givenresolution may give very different answers they actually do converge to the sameresult.
• The data set from Brugmann et. al (2004) has been confirmed to actuallyperform more than an orbit before merger.
• The resolution requirements are rather high. To reach less than 1% errors in theproperdistance we would need M/200 resolution. However, this can be improvedwith improved gauges and using full fourth order finite differencing.
Numrel 2005, NASA Goddard, November 3, 2005 17
Conclusions
• We have shown that even though 2 somewhat different gauge choices at a givenresolution may give very different answers they actually do converge to the sameresult.
• The data set from Brugmann et. al (2004) has been confirmed to actuallyperform more than an orbit before merger.
• The resolution requirements are rather high. To reach less than 1% errors in theproperdistance we would need M/200 resolution. However, this can be improvedwith improved gauges and using full fourth order finite differencing.
• We plan to revisit the QC sequence in order to map out the transition fromplunge to orbit.
Numrel 2005, NASA Goddard, November 3, 2005 17
Conclusions
• We have shown that even though 2 somewhat different gauge choices at a givenresolution may give very different answers they actually do converge to the sameresult.
• The data set from Brugmann et. al (2004) has been confirmed to actuallyperform more than an orbit before merger.
• The resolution requirements are rather high. To reach less than 1% errors in theproperdistance we would need M/200 resolution. However, this can be improvedwith improved gauges and using full fourth order finite differencing.
• We plan to revisit the QC sequence in order to map out the transition fromplunge to orbit.
• We need to improve our wave extraction techniques to be able to handle ourdrift-correct shift.
Numrel 2005, NASA Goddard, November 3, 2005 17
Conclusions
• We have shown that even though 2 somewhat different gauge choices at a givenresolution may give very different answers they actually do converge to the sameresult.
• The data set from Brugmann et. al (2004) has been confirmed to actuallyperform more than an orbit before merger.
• The resolution requirements are rather high. To reach less than 1% errors in theproperdistance we would need M/200 resolution. However, this can be improvedwith improved gauges and using full fourth order finite differencing.
• We plan to revisit the QC sequence in order to map out the transition fromplunge to orbit.
• We need to improve our wave extraction techniques to be able to handle ourdrift-correct shift.
• We need to get a better understanding of the new gauge parameter.
Numrel 2005, NASA Goddard, November 3, 2005 17