All Tables
- Table 1:
Inclination-independent errors for the
underdense jet simulation. The total swept-up mass, the molecular swept-up
mass, the mass inferred assuming T=10 K, and the mass inferred
assuming T=100 K for the simulation at t=1500 yrs. The numbers
in parentheses represent the fraction of the actual mass in the outflow.
Also shown are the same quantities for momentum and kinetic energy.
- Table 2:
Inclination-independent errors for the
density-matched
simulation. Content as in Table 1.
- Table 3:
Masses and momenta of the outflows calculated from the
relation using the velocity ranges 2-40 km s-1 and
7-40 km s-1 with
a bin width of 1 km s-1. Also shown are
and
,
the latter chosen as the velocity at which
is 1/100 that at
(see text).
- Table 4:
Inferred ages and thrusts of the outflow using the global
method and using the velocity ranges 2-40 km s-1 and 7-40 km s-1.
The quantities are normalized to the true age and molecular
thrust of the outflow. Errors on the total
(molecular+atomic) thrust may be obtained by
multiplying the relevant numbers by 0.45 (
)
or 0.26 (
).
- Table 5:
Inferred ages and thrusts of the outflow using the local
method of Lada & Fich (1996) with the velocity ranges 2-40 km s-1 and
7-40 km s-1. The quantities are normalized to the true
age and molecular thrust of the outflow. Errors on the total
(molecular+atomic) thrust may be obtained by
multiplying the relevant numbers by 0.45 (
)
or 0.26 (
).
- Table 6:
Inferred ages and thrusts of the outflow using the
method of Cabrit & Bertout (1992) and using the velocity ranges
2-40 km s-1 and 7-40 km s-1. The quantities are normalized to the
true age and molecular thrust of the outflow. Errors on the total
(molecular+atomic) thrust may be obtained by
multiplying the relevant numbers by 0.45 (
)
or 0.26 (
).
- Table 7:
Inferred ages and thrusts of the outflow using the
perpendicular method and using the velocity ranges 2-40 km s-1 and 7-40 km s-1. The quantities are normalized to the true
age and molecular thrust of the outflow. Errors on the total
(molecular+atomic) thrust may be obtained by
multiplying the relevant numbers by 0.45 (
)
or 0.26 (
).