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Table 1.

Simulations presented in this paper.

Name κ α μ δ Zshock ro, FM jet Pjet
K1 0.05 12/16 1.41 50 7.34 2150 0.64 0.94 301 179 0.102 492 0.82
K2 0.1 12/16 1.00 100 6.51 1850 0.67 1.05 323 363 0.096 616 0.81
K2l 0.1 12/16 1.00 100 12.3 2490 0.65 1.02 289 357 0.094 620 0.81
K3 0.2 12/16 0.71 200 10.1 1810 0.69 1.09 368 743 0.093 768 0.80
K4 0.5 12/16 0.45 500 8.67 1150 0.90 1.26 655 2040 0.093 1024 0.81
K5 1.0 12/16 0.32 1000 4.62 700 0.99 1.34 670 4095 0.116 1264 0.96
A1 0.1 10/16 1.00 100 9.08 1900 0.96 1.23 234 195 0.206 551 1.21
A2 0.1 11/16 1.00 100 8.34 1800 0.87 1.15 349 272 0.137 578 0.99
A3 0.1 13/16 1.00 100 5.79 1920 0.59 0.95 566 690 0.047 668 0.66
A4 0.1 14/16 1.00 100 6.26 2050 0.64 0.94 398 1321 0.023 740 0.53
A5 0.1 15/16 1.00 100 1.62 2030 0.50 0.83 1046 3275 0.009 848 0.41
SP 0.1 12/16 1.00 100 3.93 1250 0.82 1.09 506 392 0.097 613 0.98

Notes. All the simulations presented have been performed in the grid described in Sect. 2.2 (e.g., NR = 1408 and Nθ = 266) except K2l, performed in a lower resolution grid (e.g., NR = 704 and Nθ = 144) The parameters κ and α are varied independently, allowing us to compute μ, δ, and MS. The columns , and Pspine/Pjet are outputs of the simulation measured at the final time tend (given in 105Td units). Simulations K1 to A5 were done with a nonrotating spine, namely Ωa = 0 and ea = 2. Simulation SP is done for Ωa = ΩKd and ea = 10 and is discussed in Sect. 4.3. See Sect. 2.5 for the definition of all these quantities.

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