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Table 2.

Properties of multi-phase gas in the turbulent simulations with cooling.

Run Phase Temperature range vout out p ˙ out c / L AGN $ \dot{p}_{\mathrm{out}} c/L_{\mathrm{AGN}} $ E ˙ k , out / L AGN $ \dot{E}_{\mathrm{k,out}}/L_{\mathrm{AGN}} $ fesc
(km s−1) (M yr−1) (×10−3) %
TurbCoolL0.3 Cold < 3 × 104 K 91.4 92 (11.1) 0.42 (0.05) 0.13 (0.02) 0.0012
TurbCoolL0.3 Intermediate 3 × 104 K–107 K 221 9.2 (4.9) 0.1 (0.05) 0.06 (0.03) 0.54
TurbCoolL0.3 Hot > 107 K 603 15 (33) 0.45 (0.99) 0.95 (2.1) 21

TurbCoolL1.0 Cold < 3 × 104 K 209 495 (160) 1.55 (0.50) 0.83 (0.27) 0.19
TurbCoolL1.0 Intermediate 3 × 104 K–107 K 316 93 (35) 0.44 (0.16) 0.33 (0.12) 3.4
TurbCoolL1.0 Hot > 107 K 691 122 (114) 1.27 (1.19) 2.42 (2.26) 34

Notes. The first column shows the simulation name, the second and third give the name and temperature range of the gas phase. The subsequent columns show the results: mass-weighted outflow velocity, time-averaged mass outflow rate, momentum and energy loading factors, and the fraction of gas reaching escape velocity (Eq. (18)). All numbers are estimated as in Table 1.

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