An Analytic Flow Solution for YSO Jets

Kurt Liffman, PASA, 15 (2), 259
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Title/Abstract Page: An Analytic Flow Solution
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Contents Page: Volume 15, Number 2

YSO Jets

Consider a YSO where the poloidal dipole field of the YSO has been wrapped up into a toroidal field (tex2html_wrap_inline804) in the accretion disk surrounding the young stellar object (Fig. 2). The sign of the field changes as one passes through the disk. This magnetic structure suggests that the midplane of the inner accretion disk can become a zone of magnetic reconnection (Freeman 1977, Grosso et al. 1997). As the dipole field sweeps across the disk it generates a radial Freeman current in the disk. The Lorentz force generated from the Freeman current tends to compress the disk. The electric field in the disk's corona interacts with the toroidal field to drive the flow via tex2html_wrap_inline740 drift.

  figure99
Figure 2: Interaction of the dipole magnetic field from a YSO with its accretion disk.

To put this scenario on a slightly more quantitative basis, and to show how the toroidal field is created, we assume that the magnetic field rotates rigidly with the star, so at the disk surface, the velocity of the object's B field (tex2html_wrap_inline810) is
equation390
where r is the distance, in the plane of the disk, from the centre of the star and tex2html_wrap_inline814 is the angular rotational frequency of the star. If the disk rotates with a Keplerian velocity, then the disk surface has an angular velocity
equation392
where G is the gravitational constant, and tex2html_wrap_inline818 is the mass of the central object.

The magnetic field velocity relative to the disk is simply
 equation394
So when tex2html_wrap_inline820, we have reached the corotation radius tex2html_wrap_inline822, where the angular velocity of the stellar magnetic field matches the Keplerian velocity of the disk, and tex2html_wrap_inline824 has the form
 equation396
with G being the gravitational constant, tex2html_wrap_inline818 the mass of the star and tex2html_wrap_inline830 the rotation period of the star, where we have taken the typical rotation period of a YSO as our normalization value.

For tex2html_wrap_inline832 the magnetic field will induce an electric field (E), in the disk, of the form
 equation398
where tex2html_wrap_inline842 is the strength of the star's magnetic field, in the plane of the disk, at distance r from the centre of the object

Combining Eqs (10), and (12) gives
 equation403
For a disk with finite conductivity (tex2html_wrap_inline850), the induced electric field drives a Freeman current in the disk with a current density of the form
 equation407
This current, in turn, induces a toroidal field. The form of which can be deduced from Ampere's Law
 equation412
where tex2html_wrap_inline764 is the permeability of free space.

  figure132
Figure 3: Current density and toroidal field in the top half of the disk.

We integrate Eq. (15) over the section of cylindrical surface shown in figure 3. The bottom of this surface lies on the midplane of the accretion disk, where the toroidal field (tex2html_wrap_inline804) has zero magnitude. The top line lies at a height z above the midplane of the disk, where the toroidal field has a non-zero magnitude. The disk current flows in a direction perpendicular to the integration surface, so the magnitude of the toroidal field is simply:
 equation418

Equations (14) and (16) were first obtained by Bardou and Hayvaerts (1996), (see also Bardou 1997). These authors deduced these equations by analyzing the electric circuit made up of the disk, star and the magnetic fields. We have given an alternative derivation to illustrate the veracity of these results.

With our toroidal field in place, our hypothetical flow scenario is shown in Fig. 4. The wind arises from the toroidal magnetic field embedded in the disk, and expands in a roughly conical shape. Our domain of investigation is a flow-tube with a variable thickness tex2html_wrap_inline868 and initial radius tex2html_wrap_inline870, where the surface of this tube is constituted from neighbouring streamlines.

  figure146
Figure 4: The jet flow equation is derived for a thin, approximately, conical sheet, which is embedded within the jet flow.

For a flow tube of fixed average radius and variable thickness, one can show (Liffman and Siora 1997) that
 equation421
where G is the gravitational constant and M is the mass of the star. We concentrate on the case tex2html_wrap_inline876 and tex2html_wrap_inline878, so Eq. (17) has the simple form
 equation429
which is again the MHD nozzle equation, Eq. (1). So, the results for the one-dimensional flow hold for this astrophysical case. Note that the Alfvtex2html_wrap_inline758n speed at the throat tex2html_wrap_inline882 and from Eq. (6) the exhaust velocity for the jet is simply
equation437

For a magnetically confined plasma one can show (see Appendix A) that tex2html_wrap_inline884, in which case Eqs (18) and (5) integrate to an analytic flow solution:
 equation439
where we have replaced tex2html_wrap_inline886 by u, with tex2html_wrap_inline890, and tex2html_wrap_inline892, tex2html_wrap_inline894 and tex2html_wrap_inline896 being, respectively, the values of tex2html_wrap_inline748 and tex2html_wrap_inline868 at the throat. This equation is also true in the cold plasma limit tex2html_wrap_inline902 ( see Schoenberg et al. 1991).

In Fig. 5(a) we show the shape of the nozzle as given by Eq. (20). At the start of the flow tex2html_wrap_inline904, which gives tex2html_wrap_inline906. An infinitely wide nozzle is clearly unphysical, so we can expect that the initial value of tex2html_wrap_inline908 will be greater than zero in a real jet, i.e., gas has to be injected into the magnetic nozzle for it to work. At the throat tex2html_wrap_inline910 and tex2html_wrap_inline912, as expected. Finally, at the exit, tex2html_wrap_inline914 tex2html_wrap_inline916 tex2html_wrap_inline918, i.e., to obtain the maximum possible jet speed, we again require the nozzle to have infinite width. Because this is impossible, we should expect that a real jet will have a normalized exit speed somewhere between 1 and tex2html_wrap_inline920.

From Eqs (3) and (4) we have
 equation444
and
 equation446
where tex2html_wrap_inline922, tex2html_wrap_inline924, tex2html_wrap_inline926, and tex2html_wrap_inline928 are the values of tex2html_wrap_inline766, B, tex2html_wrap_inline756, and tex2html_wrap_inline752 normalized by their values at the throat of the nozzle.

At the exit of an ideal nozzle, tex2html_wrap_inline918 tex2html_wrap_inline916 tex2html_wrap_inline922, tex2html_wrap_inline924, tex2html_wrap_inline926, and tex2html_wrap_inline948. The behaviour of tex2html_wrap_inline922 and tex2html_wrap_inline924 is shown in Fig. 5(b). The magnetic field and gas density start with an initial normalized value of 1.5. The values of tex2html_wrap_inline922 and tex2html_wrap_inline924 decrease to a value of 1 at the throat of the nozzle and to a value of 0 at the end of the nozzle. Thus, an ideal MHD nozzle will produce a gas flow with a very small magnetic field and a very low gas density. This result calls into question the popular idea that toroidal fields collimate jet flows, since we may produce a jet with little or no magnetic field. We also note that a nearly ``ideal'' YSO jet may be difficult to observe, because the low density of the exhaust gas may cause the jet to fall below detection limits.

  figure212
Figure 5: (a) The width of the nozzle, tex2html_wrap_inline960, in terms of the flow speed tex2html_wrap_inline908. (b) Gas density (tex2html_wrap_inline922) and magnetic field strength (tex2html_wrap_inline924) in terms of the flow speed.

In recent years, some authors have made the suggestion that dust and small silicaceous spheres may be ejected by YSO jets (e.g., Liffman and Brown 1996). As a first step to investigate the plausibility of such a hypothesis, we take a macroscopic test particle, e.g., a small silicate sphere, and place the test particle into the flow at different places along the nozzle. In this way, we can map out the initial drag force experienced by a macroscopic particle that is simply dropped into the flow at various points along the nozzle.

The drag force (tex2html_wrap_inline968) experienced by our test particle is given by
equation450
where tex2html_wrap_inline970 is the drag coefficient and A is the cross sectional area of the test particle. If we divide the value of tex2html_wrap_inline968 by its value at the throat of the nozzle (tex2html_wrap_inline976), we obtain the normalized drag force (tex2html_wrap_inline978) which (using Eqs (20) and (21)) has the form
 equation452
where we have assumed that tex2html_wrap_inline980. From Eq. (24), tex2html_wrap_inline978 obtains a maximum value of 9/8 when tex2html_wrap_inline984. The behaviour of tex2html_wrap_inline978 is shown in Fig. 6, where we see, as expected, that the maximum drag occurs for tex2html_wrap_inline988. Since the gas speed at the throat of the nozzle is tex2html_wrap_inline990 the Keplerian speed, it is possible that a particle carried by the flow may reach escape speed and be ejected from the YSO system.

  figure242
Figure 6: The normalized drag force on a macroscopic particle placed in the MHD nozzle flow.

In the discussion so far, we have explored some of the properties of the MHD nozzle flow, but what produces the nozzle in the first place? We believe the nozzle width, tex2html_wrap_inline868, is primarily determined by the balance between the centrifugal force of the gas in the disk and the magnetic pressure gradient in the toroidal field, tex2html_wrap_inline804. To see how this could arise, we consider the steady state form of the MHD momentum equation:
 equation455
where p is the pressure and tex2html_wrap_inline1008 the acceleration due to gravity. In cylindrical coordinates, the r component of Eq. (25) is simply
 equation463
From Liffman and Siora (1997), we know that
equation471
where tex2html_wrap_inline870 is the initial value of r for a parcel of gas that starts its journey from the midplane of the accretion disk. Sample calculations suggest that tex2html_wrap_inline1016 is small relative to the other terms, so we neglect this term. The magnitude of tex2html_wrap_inline804 is given by Eq. (16), except we now have
 equation476
where
 equation478

We are required to modulate tex2html_wrap_inline804 by Eq. (29), because in the disk, tex2html_wrap_inline1026. Above the disk, however, we have a perfectly conducting corona and so the radial current that generates tex2html_wrap_inline804 in the finitely conducting disk cannot do the same in the corona. Thus, we should expect tex2html_wrap_inline804 to decrease as some function of z. In this purely illustrative example, we assume that tex2html_wrap_inline804 decreases linearly with z and disappears completely when we reach z = H + l. In the illustrative example that we give below, we have set l = H.

We can now differentiate Eq. (28) with respect to r (assuming tex2html_wrap_inline1044) and obtain
 equation480

From Eqs (28) and (30), we see that the toroidal field starts its wind-up at the corotation radius, tex2html_wrap_inline824, and the magnitude of tex2html_wrap_inline804 increases with distance from the star until it reaches a certain distance tex2html_wrap_inline1050. The exact value of tex2html_wrap_inline1050 is dependent on the r dependence of tex2html_wrap_inline842, but we have assumed a stellar dipole field (i.e., tex2html_wrap_inline1044) and so, from Eq. (30), tex2html_wrap_inline1050 has the form
equation486

Between tex2html_wrap_inline824 and tex2html_wrap_inline1050 the magnetic pressure gradient is pointing towards the star. If an element of gas, located in this region, moves away from the central (z = 0) plane of the disk. This gas element, initially, feels no magnetic force, because the central plane is a magnetic reconnection region and will have no toroidal field. However, as the particle approaches the surface of the disk, it will feel the magnetic force from the gradient in the toroidal field and move inwards towards the star until the centrifugal force balances the magnetic and gravitational forces.

A gas element that initially has tex2html_wrap_inline1068 will move only slightly towards the star, since in the near neighbourhood of the corotation orbit, tex2html_wrap_inline1070. A gas element with tex2html_wrap_inline1072, will have a tex2html_wrap_inline804 near its maximum value and the motion of the gas element will be perturbed significantly towards the star. Above the plane of the disk, tex2html_wrap_inline804 decreases with distance along the nozzle, allowing the nozzle to expand. This flow property is shown in Fig. 7, illustrating the formation of the nozzle. We obtained Fig. 7 by finding the values of r such that Eq. (26) was satisfied. The parameter values used in this simulation were, H = 0.0001 AU, tex2html_wrap_inline1082 Siemens, stellar radius tex2html_wrap_inline1084 AU, and tex2html_wrap_inline1086 Teslas.

  figure306
Figure 7: Path of a gas particle in the jet flow. z is in units of ``magnetic scale height'' (H), where tex2html_wrap_inline1090. Two elements of gas are released from the central plane of the disk (z = 0) at distances of 0.042 and 0.057 AU from the star. Magnetic pressure from the toroidal field causes these gas elements to move in towards the star. The toroidal field decreases in magnitude for z > H allowing the gas elements to return to their initial r positions, thereby producing the jet nozzle.

As is well known, toroidal magnetic fields are intrinsically unstable. This would tend to limit the applicability of toroidal fields as a driving mechanism for YSO jet flows. However, a simple analysis suggests that the ram pressure of the jet may ensure the stability of the toroidal magnetic fields (Liffman and Siora 1997).


Next Section: References
Title/Abstract Page: An Analytic Flow Solution
Previous Section: The Magnetic Nozzle
Contents Page: Volume 15, Number 2

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