Table 1.
Parameter set used in the numerical simulation model.
| Case | η | K | M | Mr | Lx × Ly × Lz | Nx × Ny × Nz | Pj (erg s−1) |
|---|---|---|---|---|---|---|---|
| A | 10−3 | 1 | 3 | 28 | 240 × 600 × 240 | 500 × 2600 × 500 | 1.5 × 1044 |
| B | 10−4 | 1 | 3 | 28 | 450 × 600 × 450 | 570 × 2600 × 570 | 1.5 × 1043 |
| C | 10−4 | 10 | 1.8 | 15 | 300 × 600 × 300 | 520 × 2600 × 520 | 4.2 × 1043 |
| D | 10−2 | 1 | 3 | 28 | 120 × 600 × 120 | 360 × 2600 × 360 | 1.5 × 1045 |
Notes. The second column refers to density ratio η, the third to the pressure ratio K, the fourth to the classical Mach number, the fifth to the relativistic Mach number, the sixth to the size of the physical domain in units of the jet radius, the seventh to the number of grid points, and the last column to the jet power evaluated according to Eq. (5).
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