Table A.2.
[O III]λλ4959,5007 model parameters.
| Param | J1029 | J1228 | J1232 | J1509 | J1510 | J1522 | J1641 |
|---|---|---|---|---|---|---|---|
| (1) Model | 4G | 6G | 6G | 6G | 4G | 4G | 4G |
| (2) fc5007 | 1.25±0.30 | 13.23±0.66 | 2.35±0.42 | 2.84±0.53 | 16.80±0.34 | 4.14±0.87 | 6.61±0.22 |
| (3) fc4959 | 0.42±0.10 | 4.41±0.22 | 0.78±0.14 | 0.54±0.09 | 5.60±0.11 | 1.38±0.29 | 2.20±0.07 |
| (4) Δcc | 31.14±34.73 | 71.25±4.49 | -37.72±30.54 | -60.48±29.94 | 1.20±2.99 | 98.20±77.84 | 38.32±4.19 |
| (5) wc | 145.21±44.91 | 110.69±14.37 | 117.09±35.93 | 144.50±34.73 | 137.64±6.59 | 239.41±116.16 | 239.30±8.98 |
| (6) fw5007 | 0.72±0.30 | 3.21±0.44 | 3.02±0.38 | 0.83±0.55 | 2.23±0.35 | 2.12±0.80 | 1.22±0.22 |
| (7) fw4959 | 0.24±0.10 | 1.07±0.15 | 1.01±0.13 | 0.28±0.18 | 0.74±0.12 | 0.71±0.27 | 0.41±0.08 |
| (8) Δcw1 | -288.01±266.45 | -162.86±32.33 | -411.35±42.51 | -361.06±135.32 | -252.68±50.30 | -648.46±316.15 | -58.08±55.69 |
| (9) ww1 | 343.85±247.29 | 149.58±44.31 | 221.68±37.72 | 153.96±116.76 | 606.28±95.20 | 326.89±283.22 | 770.93±83.83 |
| (10) fw5007 | 2.80±0.25 | 2.79±0.37 | 0.54±0.09 | ||||
| (11) fw4959 | 0.93±0.08 | 0.93±0.12 | 0.18±0.03 | ||||
| (12) Δcw2 | -371.24±35.33 | -595.77±10.78 | -192.80±264.06 | ||||
| (13) ww2 | 497.35±25.15 | 587.48±46.11 | 895.15±16.17 |
Notes. Rows: (1) Fitting model; (2) peak flux density of the [O III]λ5007 core component [× − 10−17 erg s−1 cm−2 Å−1]; (3) peak flux density of the [O III]λ4959 core component [× − 10−17 erg s−1 cm−2 Å−1]; (4) shift of the core component [km s−1]; (5) width of the core component [km s−1]; (6) peak flux density of the first [O III]λ5007 wing component [× − 10−17 erg s−1 cm−2 Å−1]; (7) peak flux density of the first [O III]λ4959 wing component [× − 10−17 erg s−1 cm−2 Å−1]; (8) shift of the first wing component [km s−1]; (9) width of the first wing component [km s−1]; (10) peak flux density of the second [O III]λ5007 wing component [× − 10−17 erg s−1 cm−2 Å−1]; (11) peak flux density of the second [O III]λ4959 wing component [× − 10−17 erg s−1 cm−2 Å−1]; (12) shift of the second wing component [km s−1]; (13) width of the second wing component [km s−1].
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