2004MNRAS.349..747P


Query : 2004MNRAS.349..747P

2004MNRAS.349..747P - Mon. Not. R. Astron. Soc., 349, 747-756 (2004/April-1)

Dynamical friction in flattened systems: a numerical test of Binney's approach.

PENARRUBIA J., JUST A. and KROUPA P.

Abstract (from CDS):

We carry out a set of self-consistent N -body calculations to investigate how important the velocity anisotropy in non-spherical dark matter haloes is for dynamical friction. For this purpose, we allow satellite galaxies to orbit within flattened and live dark matter haloes (DMHs) and compare the resulting orbit evolution with a semi-analytic code. This code solves the equation of motion of the same satellite orbits with mass loss and assumes the same DMH, but either employs Chandrasekhar's dynamical friction formula, which does not incorporate the velocity anisotropy, or Binney's description of dynamical friction in anisotropic systems. In the numerical and the two semi-analytic models, the satellites are given different initial orbital inclinations and orbital eccentricities, whereas the parent galaxy is composed of a DMH with aspect ratio qh= 0.6.

We find that Binney's approach successfully describes the overall satellite decay and orbital inclination decrease for the whole set of orbits, with an averaged discrepancy of less than 4 per cent in orbital radius during the first three orbits. If Chandrasekhar's expression is used instead, the discrepancy increases to 20 per cent. Binney's treatment therefore appears to provide a significantly improved treatment of dynamical friction in anisotropic systems.

The velocity anisotropy of the DMH velocity distribution function leads to a significant decrease with time of the inclination of non-polar satellite orbits. But, at the same time, it reduces the difference in decay times between polar and coplanar orbits evident in a flattened DMH when the anisotropic DMH velocity distribution function is not taken into account explicitly. Our N -body calculations furthermore indicate that polar orbits survive about 1.6 times longer than coplanar orbits and that the orbital eccentricity e remains close to its initial value if satellites decay slowly towards the galaxy centre. However, orbits of rapidly decaying satellites modelled with the semi-analytic code show a strong orbital circularization (e > O) not present in the N -body computations.


Abstract Copyright: 2004 RAS

Journal keyword(s): stellar dynamics - methods: analytical - methods: N -body simulations - galaxies: dwarf - galaxies: haloes - galaxies: kinematics and dynamics

Simbad objects: 15

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Number of rows : 15
N Identifier Otype ICRS (J2000)
RA
ICRS (J2000)
DEC
Mag U Mag B Mag V Mag R Mag I Sp type #ref
1850 - 2024
#notes
1 2MASX J01385522-0745553 GiC 01 38 55.2336829296 -07 45 55.565640144   15.62       ~ 72 0
2 2E 0150.5-1358 ClG 01 53 00.40 -13 44 18.0           ~ 387 0
3 NGC 720 Sy1 01 53 00.523 -13 44 19.25   12.4   10.36   ~ 523 0
4 NGC 891 H2G 02 22 32.907 +42 20 53.95 11.08 10.81 9.93 7.86   ~ 1670 2
5 NGC 1332 GiP 03 26 17.321 -21 20 07.33   11.45   9.84   ~ 351 0
6 NGC 2841 LIN 09 22 02.6778711696 +50 58 35.737082868 10.43 10.09 9.22     ~ 1073 1
7 NGC 2905 H2G 09 32 10.111 +21 30 02.99 10.44 9.75 9.07 8.68   ~ 1119 3
8 NGC 3198 EmG 10 19 54.990 +45 32 58.88 10.83 10.87 10.33     ~ 906 1
9 NGC 3923 GiG 11 51 01.783 -28 48 22.36 11.41 10.59 9.80 8.88   ~ 439 1
10 NGC 4013 GiG 11 58 31.417 +43 56 49.28   12.4       ~ 423 1
11 NGC 4244 GiG 12 17 29.659 +37 48 25.60   10.71   9.99   ~ 558 1
12 NGC 4565 LIN 12 36 20.804 +25 59 14.61   13.61 12.43     ~ 958 0
13 ESO 322-69 Sy2 12 44 49.0352044176 -40 42 51.691570488   14.12 13.58 13.29 13.9 ~ 197 0
14 NGC 4753 GiG 12 52 22.112 -01 11 58.88 11.26 10.85 9.95     ~ 274 1
15 LEDA 64612 Sy2 20 23 54.9120351168 -50 39 06.848951112   14.72   13.59   ~ 59 0

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