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Table 1.

Resulting parameters of modeling the values via function (5).

i E/I(a) n1 nK K sp(b) (c) Object d Ref.
70° E 0.47 BF Cyg 3.4 < 3.3 × 10−7(d) (1)
I CI Cyg 1.6 ∼4.4 × 10−7 (2)
80° E 0.35 YY Her 6.3 < 2.9 × 10−7 (3)
I AR Pav 4.9 (4)
90° E 0.43 AX Per 1.7 ∼8.8 × 10−8 (5)
I PU Vul 4.7 < 5.8 × 10−7(d) (6)

Notes. The first part of the table contains the fitting parameters of the wind, n1(1023 cm−2), nK(1025 cm−2), K, cm−2), the corresponding spherical equivalent of the mass-loss rate, sp (M yr−1; see Sect. 3.1), and a minimum of the function for three different orbital inclinations, i (see Sect. 2.2). The second part, to the right of the vertical bar, compares the total mass-loss rates, (M yr−1), derived from radio emission by Seaquist et al. (1993) recalculated for distances d (in kpc) from the literature, listed in the last column, reference.

(a)

From egress (E) or ingress (I) data (see Sect. 2.2).

(b)

For v = 30 km s−1 (see Sect. 5.1. of Paper II).

(c)

Corresponds to 34 degrees of freedom.

(d)

Upper limit due to a contribution from the active hot component.

References. (1) Muerset et al. (1991), (2) Seaquist et al. (1993), (3) Skopal (2005a), (4) Schild et al. (2001), (5) Skopal et al. (2001), and (6) Kato et al. (2012).

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