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Home All issues Volume 692 (December 2024) A&A, 692 (2024) A183 Full HTML
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Table 1.

Main parameters of the simulation set-up.

1 2 3 4 5 6 7 8 9 10 11 12 13
Model Simulation Scenario Dwarf DM M300 Initial Offset M ˙ $ \dot{M} $ w Dwarf gas Orbital F.V. Motion Orbit
name name model profile 106 M⊙ Type, PA[°] 10 − 5 M ⊙ yr − 1 $ 10^{-5}\,\mathrm{M}_{\odot} \,\mathrm{yr}^{-1} $  km s−1 component ut,|V| km/s θsky[°] type
M1 S4M4 I D1 Burkert 1.7 – – – WNM 50, 83 52 BA
M2 S4M5 I D1 Burkert 1.7 – – – WNM 100, 120 33 BA–FI
M3 S4M6 I D1 Burkert 1.7 – – – WNM 200, 210 18 FI
M4 S4M7 I D1 Burkert 1.7 – – – WNM 300, 307 12 FI
M5 S4M9 I D1 Burkert 1.7 – – – WNM 100, 120 33 BA–FI+P
M6 S11M12 I D2 Burkert 8.0 – – – WNM 200, 210 18 FI
M7 S11M11 I D2 Burkert 8.0 – – – WNM 300, 307 12 FI
M8 A1M1 II D1 Burkert 1.7 stellar(r), 46 10 20 WNM 200, 210 18 FI
M9 A1M6 II D2 Burkert 8.0 stellar(r), 46 20 30 WNM 200, 210 18 FI
M10 S1M12 II D1t Burkert 1.7 stellar(r), 0 10 20 WNM+CNM 200, 210 18 FI
M11 SZM4 II D3 Burkert 15.5 stellar(r), 46 40 50 WNM 200, 210 18 FI
M12 A1M7 II D4 NFW 8.0 stellar(r), 46 20 30 WNM 200, 210 18 FI
M13 S7M3 II D4 NFW 8.0 stellar(r), 46 10 20 WNM 200, 210 18 FI
M14 S7M4 II D4 NFW 8.0 stellar(c), 46 10 20 WNM 200, 210 18 FI
M15 S10M1 III D1 Burkert 1.7 gas(r), 46 – – WNM 200, 210 18 FI
M16 S10M2 III D2 Burkert 8.0 gas(r), 46 – – WNM 200, 210 18 FI
M17 S10M3 III D4 NFW 8.0 gas(r), 46 – – WNM 200, 210 18 FI
M18 S8M2 III D1t Burkert 1.7 gas(r), 46 – – WNM+CNM 200, 210 18 FI
M19 S8M7 III D2t Burkert 8.0 gas(r), 46 – – WNM+CNM 200, 210 18 FI
M20 S8M8 III D4t NFW 8.0 gas(r), 46 – – WNM+CNM 200, 210 18 FI
M21 S8M6 III D4t NFW 8.0 gas(c), 46 – – WNM+CNM 200, 210 18 FI

Notes. Columns: 1) Model name; 2) Run name; 3) Scenario; 4) Dwarf models with different mass distributions, where the letter ‘t’ indicates a set-up with two gas components; 5) Dark matter profile; 6) Dynamical mass within 300 pc; 7) Offset of stellar or gaseous component, with offset type radial (r), circular (c), or none (–), and the position angle of the initial offset; 8) Stellar winds outflow mass rate; 9) Velocity of stellar winds outflows; 10) Included gaseous components (warm neutral medium WNM, cold neutral medium CNM); 11) FV: magnitude of the final GSR tangential velocity (ut) and total velocity (V) of the orbits; 12) Angle between the LOS and tangential (sky) velocities of the satellite orbit (e.g. θsky = 0° corresponds to a tangential velocity only, with the satellite moving on the plane of the sky); 13) Orbit type as backsplash orbit (BA), first infall (FI), or in the limit between the two solutions (BA–FI), and a comment if a perturbation (+P) is included in the IGM gas density. Videos of the simulations can be found at this link https://www.youtube.com/playlist?list=PLoegIUZ3yJ9FuDldEF-USJWd-ohyLavl.

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