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Table 3.

Eccentric models.

Num. β0 Vrot E ˙ tot $ \langle\dot{E}_{\mathrm{tot}}\rangle $ E ˙ tot per $ \dot{E}_{\mathrm{tot}}^{\mathrm{per}} $ E ˙ tot ap $ \dot{E}_{\mathrm{tot}}^{\mathrm{ap}} $ Δ E ˙ / L $ \Delta \dot{E}/L_* $
P = 6.0 e = 0.1 rper = 32.15

201 0.20 11 7.60 × 10−1 1.65 4.10 × 10−1 3.10 × 10−3
202 0.40 22 2.30 × 10−1 5.40 × 10−1 1.20 × 10−1 1.05 × 10−3
203 0.60 34 4.80 × 10−2 1.40 × 10−1 2.00 × 10−2 3.00 × 10−4
204 0.80 45 4.20 × 10−3 1.20 × 10−2 1.20 × 10−3 2.70 × 10−5
205 0.88 49 2.50 × 10−3 4.80 × 10−3 2.00 × 10−3 7.00 × 10−6
206 0.95 53 4.20 × 10−3 2.40 × 10−3 5.50 × 10−3 −7.75 × 10−6
207 1.00 56 8.80 × 10−3 3.40 × 10−3 1.10 × 10−2 −1.90 × 10−5
208 1.05 59 1.50 × 10−2 7.10 × 10−3 2.00 × 10−2 −3.22 × 10−5
209 1.20 67 6.30 × 10−2 4.90 × 10−2 7.60 × 10−2 −6.75 × 10−5
210 1.40 79 2.70 × 10−1 2.70 × 10−1 3.00 × 10−1 −7.50 × 10−5
211 1.60 90 9.30 × 10−1 9.30 × 10−1 8.80 × 10−1 1.25 × 10−4
212 1.88 105 3.01 3.48 3.12 9.00 × 10−4
213 1.95 109 4.20 4.84 4.32 1.30 × 10−3

P = 8.73 e = 0.3 rper = 32.1

301 0.20 12 6.50 × 10−1 2.47 1.80 × 10−1 5.73 × 10−3
302 0.40 24 1.80 × 10−1 6.90 × 10−1 3.50 × 10−2 1.64 × 10−3
303 0.60 37 4.90 × 10−2 2.30 × 10−1 1.00 × 10−2 5.50 × 10−4
304 0.80 49 2.40 × 10−2 7.90 × 10−2 1.10 × 10−2 1.70 × 10−4
305 0.88 54 1.60 × 10−2 1.70 × 10−2 9.60 × 10−3 1.85 × 10−5
306 0.95 58 1.30 × 10−4 7.60 × 10−3 1.30 × 10−2 −1.35 × 10−5
307 1.00 61 2.20 × 10−2 6.70 × 10−3 1.60 × 10−2 −2.33 × 10−5
308 1.05 64 2.40 × 10−2 5.60 × 10−3 1.70 × 10−2 −2.85 × 10−5
309 1.20 73 5.30 × 10−2 3.00 × 10−2 3.60 × 10−2 −1.50 × 10−5
310 1.40 86 1.70 × 10−1 2.10 × 10−1 1.20 × 10−1 2.25 × 10−4
311 1.60 98 6.00 × 10−1 9.50 × 10−1 4.80 × 10−1 1.17 × 10−3
312 1.88 115 4.42 5.60 3.64 4.90 × 10−3
313 1.95 119 6.45 8.11 5.53 6.43 × 10−3

P = 14.49 e = 0.5 rper = 32.1

501 0.20 13 5.40 × 10−1 2.83 3.62 −1.97 × 10−3
502 0.40 26 2.20 × 10−1 1.04 3.00 × 10−2 2.52 × 10−3
503 0.60 39 1.30 × 10−1 4.30 × 10−1 6.00 × 10−2 9.25 × 10−4
504 0.80 52 4.30 × 10−2 9.00 × 10−2 2.00 × 10−2 1.75 × 10−4
507 1.00 66 2.40 × 10−2 1.10 × 10−2 4.72 × 10−3 1.57 × 10−5
508 1.05 69 2.50 × 10−2 8.93 × 10−3 5.53 × 10−3 8.50 × 10−6
509 1.10 72 2.80 × 10−2 1.03 × 10−2 6.76 × 10−3 8.85 × 10−6
510 1.20 78 3.90 × 10−2 3.01 × 10−2 8.38 × 10−3 5.43 × 10−5
511 1.40 92 1.10 × 10−1 2.40 × 10−1 3.09 × 10−2 5.23 × 10−4
512 1.60 105 4.30 × 10−1 1.13 1.60 × 10−1 2.43 × 10−3
513 1.88 123 4.65 8.18 3.55 1.16 × 10−2
514 1.95 128 8.80 13.2 7.42 1.44 × 10−2

P = 31.17 e = 0.7 rper = 32.15

701 0.20 14 3.60 × 10−1 3.07 4.96 × 10−3 7.66 × 10−3
702 0.40 28 2.00 × 10−1 1.40 3.86 × 10−2 3.40 × 10−3
703 0.60 42 1.20 × 10−1 5.10 × 10−1 5.89 × 10−2 1.13 × 10−3
704 0.80 56 4.70 × 10−2 1.20 × 10−1 1.12 × 10−2 2.72 × 10−4
707 1.00 70 2.20 × 10−2 2.43 × 10−2 3.02 × 10−3 5.32 × 10−5
708 1.05 73 2.06 × 10−2 2.09 × 10−2 2.87 × 10−3 4.51 × 10−5
709 1.10 77 2.05 × 10−2 2.40 × 10−2 2.69 × 10−3 5.33 × 10−5
711 1.40 98 6.90 × 10−2 4.20 × 10−1 1.11 × 10−2 1.02 × 10−3
712 1.60 112 3.00 × 10−1 2.21 8.33 × 10−2 5.32 × 10−3
713 1.88 131 3.71 16.2 2.24 3.49 × 10−2
714 1.95 136 5.66 22.6 3.70 4.72 × 10−2

Notes. Surface equatorial rotation velocity Vrot is in km s−1; total energy dissipation rate averaged over the orbital cycle, total energy dissipation rate at periastron and at apastron are in units of 1035 ergs s−1. The last column gives ( E ˙ tot per $ \dot{E}_{\mathrm{tot}}^{\mathrm{per}} $ E ˙ tot ap $ \dot{E}_{\mathrm{tot}}^{\mathrm{ap}} $)/L* where L* = 4 × 1037 ergs s−1 is the adopted total luminosity for a 10 M star such as the one we model. A negative value occurs when the brightness at apastron is greater than at periastron. The heading for each set models lists the corresponding orbital period in days, eccentricity, and orbital separation at periastron rper in solar units.

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