Table 2.

Averaged values of the common-envelope efficiency parameter αλ over about 100 orbits. The error estimates are derived from the temporal variations. Column 1 gives the name of the simulated triple; column 2 the relative inclination; column 3 the measured value of αλ.

Object nameiαλ
ξ Tau5.8 ± 0.8
ξ Tau20°5.0 ± 0.6
ξ Tau40°3.7 ± 0.3
ξ Tau69°2.9 ± 0.3
HD 971316.8 ± 0.9
Object nameiαλ
ξ Tau5.8 ± 0.8
ξ Tau20°5.0 ± 0.6
ξ Tau40°3.7 ± 0.3
ξ Tau69°2.9 ± 0.3
HD 971316.8 ± 0.9
Table 2.

Averaged values of the common-envelope efficiency parameter αλ over about 100 orbits. The error estimates are derived from the temporal variations. Column 1 gives the name of the simulated triple; column 2 the relative inclination; column 3 the measured value of αλ.

Object nameiαλ
ξ Tau5.8 ± 0.8
ξ Tau20°5.0 ± 0.6
ξ Tau40°3.7 ± 0.3
ξ Tau69°2.9 ± 0.3
HD 971316.8 ± 0.9
Object nameiαλ
ξ Tau5.8 ± 0.8
ξ Tau20°5.0 ± 0.6
ξ Tau40°3.7 ± 0.3
ξ Tau69°2.9 ± 0.3
HD 971316.8 ± 0.9
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