| 3 | | || Run1 || || |
| 4 | | || Run2 || || |
| | 3 | {{{ |
| | 4 | |
| | 5 | 1 ev ~ 11604.5 K |
| | 6 | |
| | 7 | points picked on the curve: |
| | 8 | xp=[0.3 0.5 0.7 0.9 1.2] |
| | 9 | yp=xp+log10(11604.5) |
| | 10 | |
| | 11 | T_ps = 10^yp = 1.0e+05*[0.2315 0.3670 0.5816 0.9218 1.8392] |
| | 12 | |
| | 13 | T_ps=0.75*M_H/K_B*Vjet^2 |
| | 14 | |
| | 15 | M_H = 1.6733 * 1e-24; |
| | 16 | KB = 1.380658 * 1e-16; |
| | 17 | |
| | 18 | Vjet = sqrt(4*KB*T_ps/M_H/3); |
| | 19 | |
| | 20 | Vjet = 1.0e+06 *[1.5960 2.0093 2.5295 3.1845 4.4982] cm/s |
| | 21 | = [15.96 20.093 25.295 31.845 44.982] km/s |
| | 22 | mach=[1.1459 1.4426 1.8161 2.2863 3.2295] |
| | 23 | }}} |
| | 24 | |
| | 25 | == Runs to do == |
| | 26 | |
| | 27 | **Common parameters:** |
| | 28 | |
| | 29 | || rho_amb || 1e18 1/cm3 || |
| | 30 | || T_amb || 8.4e4 K || |
| | 31 | || rho_jet || 6e18 1/cm3 || |
| | 32 | || T_jet || 1.4e4 K || |
| | 33 | |
| | 34 | **Runs:** |
| | 35 | |
| | 36 | || || T_ps (K) || Vjet (km/s)|| Mach || |
| | 37 | || Run1 || 23150 || 15.96 || 1.1459 || |
| | 38 | || Run2 || 36700 || 20.093 || 1.4426 || |
| | 39 | || Run3 || 58160 || 25.295 || 1.8161 || |
| | 40 | || Run4 || 92180 || 31.845 || 2.2863 || |
| | 41 | || Run5 || 183920 || 44.982 || 3.2295 || |
| | 42 | |
| | 43 | |
| | 44 | |
| | 45 | ---- |