Table 3.
Angular-momentum loss.
| Model | ηiso | ⟨η⟩fit | ⟨η⟩orb |
|---|---|---|---|
| Q2e0 | 0.111 | 0.278 | 0.217 |
| Q2e02 | 0.111 | 0.240 | 0.199 |
| Q2e04 | 0.111 | 0.197 | 0.175 |
| Q2e06 | 0.111 | 0.154 | 0.151 |
| Q2e08 | 0.111 | 0.123 | 0.130 |
| Q2e06v1 | 0.111 | 0.411 | 0.198 |
| MMe05 | 0.111 | 0.402 | 0.494 |
Notes. ηiso corresponds to the specific angular-momentum loss in units of J/μ for the isotropic-wind case. ⟨η⟩fit corresponds to the average angular-momentum loss as derived by computing the average orbital velocity during one orbit and applying the fit for η(q, vw/vorb) obtained in Paper II. ⟨η⟩orb is the average angular-momentum loss per orbit for the numerical models presented in this paper, computed over the last five orbits.
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