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CfA logo 1 In models of the sculpting of planetesimal disks by planets, the planetesimals are often treated as test particles, with their effects on the planet modeled analytically. However, this treatment is insufficient in regimes in which: 1) the disk’s self-gravity cannot be neglected (i.e. early in the disk’s lifetime, it may have mass comparable to the sculpting planet), and/or 2) the back-reaction on the planet by a large number of small planetesimals must be simulated (e.g. for modeling stochastic effects). We are adapting gadget (Springel 2005), a cosmological simulation code, for use in non-collisional debris disks, allowing us to model thousands to millions of planetesimals in a reasonable CPU time through gains in speed from gadget’s parallel processing implementation and tree code for N-body interactions. We will use this adaption, gadgetbelt, to explore planet-disk interactions in regimes in which the debris disk’s mass is comparable to that of the planet. gadgetbelt: a tool for modeling planetary sculpting of massive debris disks Rebekah I. Dawson & Ruth A. Murray-Clay Harvard-Smithsonian Center for Astrophysics Introduction We gratefully acknowledge funding by the Brinson Foundation. We thank Elena D’Onghia, Mark Vogelsberger, and Paul Edmon for helpful discussions. We are grateful to Volker Springel for the use of Gadget-3. A portion of the computations here were run on the Odyssey cluster supported by the FAS Science Division Research Computing Group at Harvard University. Acknowledgements Chambers, J. E. 1999, MNRAS, 304, 793 Dawson, R. & Murray-Clay, R. 2012, ApJ, 750, 43 Dawson, R., Murray-Clay, R., & Fabrycky, D., 2011, ApJL, 743, L17 Hahn, J. M. 2003, ApJ, 595, 531 Ishiyama, T., Nitadori, K., & Makino, J. 2012, arXiv:1211.4406 Murray-Clay, R. & Chiang, E. 2006, ApJ, 651, 1194 Springel, V. 2005, MNRAS, 364, 1105 Wisdom, J., Holman, M., & Touma, J. 1996, Fields Inst. Comm.,10, 217 Wolff, S., Dawson, R. & Murray-Clay R. 2012, ApJ, 746, 171 References Future Work Code development and benchmarking Applications Stochastic migration 0 2 4 6 8 10 Timescale of Migration o (Myr) 0.0 0.2 0.4 0.6 0.8 1.0 Numerical Capture and Retention Fraction Smooth 200km 400km 500km 600km 900km 1600km Murray-Clay & Chiang (2006), Fig. 6 Planetary sculpting of debris disks Example: warped disk 60 40 20 0 20 40 60 6 4 2 0 2 4 6 z (AU) 60 40 20 0 20 40 60 6 4 2 0 2 4 6 z (AU) 60 40 20 0 20 40 60 x (AU) 60 40 20 0 20 40 60 y (AU) 60 40 20 0 20 40 60 60 40 20 0 20 40 60 60 40 20 0 20 40 60 60 40 20 0 20 40 60 Development and benchmarking Treatment of gravitational forces Computational efficiency gadgetbelt mercury Gravitational tree algorithm Ishiyama et al. (2012), Fig. 1 A 20 MEarth inclined planet orbit warps a 20 MEarth planetsimal disk. Planetesimals back- react on the planet, alter its orbit, and self stir. Two viewing angles (top and bottom) of planetesimals’ instantaneous positions (black) and planet’s orbit (red) for different gravitational treatments (columns). Columns 1-3 employ the mercury Bulirsch- Stoer integrator (Chambers 1999) for benchmarking with gadgetbelt. Column 1: planetesimals treated as test particles (appropriate for disk masses << planet, e.g. Beta Pictoris, Dawson et al. 2011) . Column 2: planetesimals treated as “small bodies” (interact with planet but not each other). Column 3: full gravitational treatment. Column 4: Modeled in gadgetbelt. particle node particle force node force We retain the gravitational tree algorithm for planetesimal-planetesimal interactions but compute the forces exerted on and by the planet directly. To do so, we implement a cell- opening criterion in which every cell is opened when computing the forces on the planet and in which the cell containing the planet is always opened. The figure on the left reveals discrepancies between the full gravitational treatment using mercury and the approximate treatment using the unmodified version of gadget. Numerical stochasticity causes the planet to random walk with larger steps, resulting in a large net migration. The change in the planet's semi-major axis in turn changes the secular evolution timescale, resulting in a different period for the precession of the planet's node and the oscillation of its inclination. 1 2 3 4 5 i (deg) 100 200 300 node (deg) 0.0 0.2 0.4 0.6 0.8 1.0 1.2 time (Myr) 29.75 29.80 29.85 29.90 29.95 30.00 a (AU) Evolution of the inclination (top), longitude of ascending node (middle), and semi-major axis (bottom) of an inclined, Neptune-mass planet interacting with an exterior, Neptune-mass planetesimal belt, simulated using mercury Bulirsch– Stoer (Chambers 1999, black dashed line), unmodified gadget (Springel 2005, red dotted line), and modified gadgetbelt (blue solid line). Without (red dotted line) modifications, the planet undergoes a more stochastic random walk that alters the evolution timescale is its inclination and node. 0.00 Myr -60 -40 -20 0 20 40 60 AU -60 -40 -20 0 20 40 60 AU 40 50 60 70 r (AU) 0 100 200 300 angle (deg) 0.50 Myr -60 -40 -20 0 20 40 60 AU -60 -40 -20 0 20 40 60 AU 40 50 60 70 r (AU) 0 100 200 300 angle (deg) 1.50 Myr -60 -40 -20 0 20 40 60 AU -60 -40 -20 0 20 40 60 AU 40 50 60 70 r (AU) 0 100 200 300 angle (deg) 2.00 Myr -60 -40 -20 0 20 40 60 AU -60 -40 -20 0 20 40 60 AU 40 50 60 70 r (AU) 0 100 200 300 angle (deg) 2.35 Myr -60 -40 -20 0 20 40 60 AU -60 -40 -20 0 20 40 60 AU 40 50 60 70 r (AU) 0 100 200 300 angle (deg) 2.35 Myr 40 45 50 55 60 65 70 a (AU) 0 1 2 3 4 5 maximum i (deg) 40 45 50 55 60 65 70 a (AU) 0.00 0.05 0.10 0.15 0.20 maximum e Particle layout Forces on a particle. Distant particles are combined into nodes. Our modified implementation Forces on a planetesimal. Computed using tree except force by planet calculated directly. Forces on a planet. All calculated directly. planetesimal particle mercury mercury planet particle Gravitational softening We are exploring the computational efficiency of the gadgetbelt, including how the computation time scales with the number of processors. 20 MEarth corresponds to one million 500-km planetesimals. We are optimizing the gravitational softening (smoothing) parameter that also sets the maximum timestep. In the regimes we are exploring, it is not necessary to follow close encounters among planetesimals. In a self-gravitating disk, density waves propogate, launched at the disk edge or at resonances. In the latter case, density waves can smear out the excitation of eccentricities and inclinations caused by secular resonances, as explored by Hahn (2003) using the ring approximation. Left: Planetesimals in a 10 MEarth (black) and 0.0001 MEarth (red) Kuiper belt, modeled with gadgetbelt including solar system planets. Top: Density waves smear out the excitation caused by the nu8 secular resonance. Bottom: Planetesimals’ self-gravity stirs up the disk and alters excitation caused by mean motion resonances. Example: density waves Below: Spiral density waves propagate through a 10 MEarth disk [initial density profile proportional to a^(-1.5)]. Top: planetesimal positions, modeled with gadgetbelt including solar system planets.. Bottom: Contoured, smoothed surface density as a function of polar angle and radius. -- Implementation of a higher-order symplectic integrator for planet particles -- Assessment of computational efficiency -- Optimization of gravitational softening parameter -- Implementation of artificial collisional damping force and other user-defined forces Murray-Clay and Chiang (2006) developed analytical models for the stochasticity of planetesimal driven migration, caused by the finite size of Kuiper belt objects (KBOs) entering a planet’s hill sphere, and a test of the planetesimal size distribution based on today’s population of resonant KBOs, but it was not computationally feasible to combine stochastic migration with N-body models of the global dynamics of the Solar System. We will place constraints on the early planetesimal size distribution through global N-body simulations of early Solar System that include both the planetesimal disk and stochastic migration. Previously, we performed a parameter study of Kuiper belt assembly (Wolff et al. 2012, Dawson and Murray-Clay 2012), in which we modeled the KBOs as massless test particles. We will investigate for which masses of the planetesimal disk the constraints we developed hold, accounting for the back- reaction of the disk and self-gravity.
Transcript
Page 1: gadgetbelt: a tool for modeling planetary sculpting of ... · Gadget-3. A portion of the computations here were run on the Odyssey cluster supported by the FAS Science Division Research

CfA logo1

In models of the sculpting of planetesimal disks by planets, the planetesimals are often treated as test particles, with their effects on the planet modeled analytically. However, this treatment is insufficient in regimes in which: 1) the disk’s self-gravity cannot be neglected (i.e. early in the disk’s lifetime, it may have mass comparable to the sculpting planet), and/or 2) the back-reaction on the planet by a large number of small planetesimals must be simulated (e.g. for modeling stochastic effects). We are adapting gadget (Springel 2005), a cosmological simulation code, for use in non-collisional debris disks, allowing us to model thousands to millions of planetesimals in a reasonable CPU time through gains in speed from gadget’s parallel processing implementation and tree code for N-body interactions. We will use this adaption, gadgetbelt, to explore planet-disk interactions in regimes in which the debris disk’s mass is comparable to that of the planet.

gadgetbelt: a tool for modeling planetary sculpting of massive debris disks

Rebekah I. Dawson & Ruth A. Murray-ClayHarvard-Smithsonian Center for Astrophysics

Introduction

We gratefully acknowledge funding by the Brinson Foundation. We thank Elena D’Onghia, Mark Vogelsberger, and Paul Edmon for helpful discussions. We are grateful to Volker Springel for the use of Gadget-3. A portion of the computations here were run on the Odyssey cluster supported by the FAS Science Division Research Computing Group at Harvard University.

Acknowledgements

Chambers, J. E. 1999, MNRAS, 304, 793 Dawson, R. & Murray-Clay, R. 2012, ApJ, 750, 43Dawson, R., Murray-Clay, R., & Fabrycky, D., 2011, ApJL, 743, L17Hahn, J. M. 2003, ApJ, 595, 531 Ishiyama, T., Nitadori, K., & Makino, J. 2012, arXiv:1211.4406 Murray-Clay, R. & Chiang, E. 2006, ApJ, 651, 1194 Springel, V. 2005, MNRAS, 364, 1105Wisdom, J., Holman, M., & Touma, J. 1996, Fields Inst. Comm.,10, 217Wolff, S., Dawson, R. & Murray-Clay R. 2012, ApJ, 746, 171

References

Future WorkCode development and benchmarking

ApplicationsStochastic migration

0 2 4 6 8 10Timescale of Migration o (Myr)

0.0

0.2

0.4

0.6

0.8

1.0

Num

eric

al C

aptu

rean

d Re

tent

ion

Frac

tion

Smooth200km

400km

500km

600km900km

1600km

Murray-Clay & Chiang (2006), Fig. 6

Planetary sculpting of debris disks

Example: warped disk

mercury test particles

−60−40−20 0 20 40 60−6−4−2

0246

z (A

U)

−60−40−20 0 20 40 60−6−4−2

0246

z (A

U)

mercury small

−60−40−20 0 20 40 60x (AU)

−60−40−20 0 20 40 60y (AU)

mercury big

−60−40−20 0 20 40 60

−60−40−20 0 20 40 60

gadget

−60−40−20 0 20 40 60

−60−40−20 0 20 40 60

Development and benchmarkingTreatment of gravitational forces

Computational efficiency

gadgetbeltmercuryGravitational tree algorithmIshiyama et al. (2012), Fig. 1

A 20 MEarth inclined planet orbit warps a 20 MEarth planetsimal disk. Planetesimals back-react on the planet, alter its orbit, and self stir.

Two viewing angles (top and bottom) of planetesimals’ instantaneous positions (black) and planet’s orbit (red) for different gravitational treatments (columns). Columns 1-3 employ the mercury Bulirsch-Stoer integrator (Chambers 1999) for benchmarking with gadgetbelt. Column 1: planetesimals treated as test particles (appropriate for disk masses << planet, e.g. Beta Pictoris, Dawson et al. 2011) . Column 2: planetesimals treated as “small bodies” (interact with planet but not each other). Column 3: full gravitational treatment. Column 4: Modeled in gadgetbelt.

particlenode particle force

node force

We retain the gravitational tree algorithm for planetesimal-planetesimal interactions but compute the forces exerted on and by the planet directly. To do so, we implement a cell-opening criterion in which every cell is opened when computing the forces on the planet and in which the cell containing the planet is always opened. The figure on the left reveals discrepancies between the full gravitational treatment using mercury and the approximate treatment using the unmodified version of gadget. Numerical stochasticity causes the planet to random walk with larger steps, resulting in a large net migration. The change in the planet's semi-major axis in turn changes the secular evolution timescale, resulting in a different period for the precession of the planet's node and the oscillation of its inclination.

1

2

3

45

i (de

g)

100

200

300

node

(deg

)

0.0 0.2 0.4 0.6 0.8 1.0 1.2time (Myr)

29.75

29.80

29.85

29.90

29.95

30.00

a (A

U)

Evolution of the inclination (top), longitude of ascending node (middle), and semi-major axis (bottom) of an inclined, Neptune-mass planet

interacting with an exterior, Neptune-mass planetesimal belt, simulated using mercury Bulirsch–

Stoer (Chambers 1999, black dashed line), unmodified gadget (Springel 2005, red dotted line), and modified gadgetbelt (blue solid line). Without

(red dotted line) modifications, the planet undergoes a more stochastic random walk that alters the evolution

timescale is its inclination and node.

0.00 Myr

-60-40-20 0 20 40 60AU

-60-40-20

0204060

AU

40 50 60 70r (AU)

0

100

200

300

angl

e (d

eg)

0.50 Myr

-60-40-20 0 20 40 60AU

-60-40-20

0204060

AU

40 50 60 70r (AU)

0

100

200

300

angl

e (d

eg)

1.50 Myr

-60-40-20 0 20 40 60AU

-60-40-20

0204060

AU

40 50 60 70r (AU)

0

100

200

300

angl

e (d

eg)

2.00 Myr

-60-40-20 0 20 40 60AU

-60-40-20

0204060

AU

40 50 60 70r (AU)

0

100

200

300

angl

e (d

eg)

2.35 Myr

-60-40-20 0 20 40 60AU

-60-40-20

0204060

AU

40 50 60 70r (AU)

0

100

200

300

angl

e (d

eg)

2.35 Myr

40 45 50 55 60 65 70a (AU)

0

1

2

3

4

5

max

imum

i (d

eg)

40 45 50 55 60 65 70a (AU)

0.00

0.05

0.10

0.15

0.20

max

imum

e

Particle layout Forces on a particle. Distant particles are combined into nodes.

Our modified implementation

Forces on a planetesimal.Computed using tree except force by planet calculated directly.

Forces on a planet. All calculated directly.

planetesimal particle

mercury mercury

planet particle

Gravitational softening

We are exploring the computational efficiency of the gadgetbelt, including how the computation time scales with the number of processors. 20 MEarth corresponds to one million 500-km planetesimals.

We are optimizing the gravitational softening (smoothing) parameter that also sets the maximum timestep. In the regimes we are exploring, it is not necessary to follow close encounters among planetesimals.

In a self-gravitating disk, density waves propogate, launched at the disk edge or at resonances. In the latter case, density waves can smear out the excitation of eccentricities and inclinations caused by secular resonances, as explored by Hahn (2003) using the ring approximation.

Left: Planetesimals in a 10 MEarth (black) and 0.0001 MEarth (red) Kuiper belt, modeled with gadgetbelt

including solar system planets. Top: Density waves smear out the excitation caused by the nu8 secular resonance.

Bottom: Planetesimals’ self-gravity stirs up the disk and alters excitation caused by mean motion resonances.

Example: density waves Below: Spiral density waves propagate through a 10 MEarth disk [initial density profile proportional to a^(-1.5)]. Top: planetesimal positions, modeled

with gadgetbelt including solar system planets.. Bottom: Contoured, smoothed surface density as a function of polar angle and radius.

-- Implementation of a higher-order symplectic integrator for planet particles-- Assessment of computational efficiency-- Optimization of gravitational softening parameter-- Implementation of artificial collisional damping force and other user-defined forces

Murray-Clay and Chiang (2006) developed analytical models for the stochasticity of planetesimal driven migration, caused by the finite size of Kuiper belt objects (KBOs) entering a planet’s hill sphere, and a test of the planetesimal size distribution based on today’s population of resonant KBOs, but it was not computationally feasible to combine stochastic migration with N-body models of the global dynamics of the Solar System. We will place constraints on the early planetesimal size distribution through global N-body simulations of early Solar System that include both the planetesimal disk and stochastic migration.

Previously, we performed a parameter study of Kuiper belt assembly (Wolff et al. 2012, Dawson and Murray-Clay 2012), in which we modeled the KBOs as massless test particles. We will investigate for which masses of the planetesimal disk the constraints we developed hold, accounting for the back-reaction of the disk and self-gravity.

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