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首页> 外文期刊>The Astrophysical journal >Magnetocentrifugal Launching of Jets from Accretion Disks. II. Inner Disk-driven Winds
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Magnetocentrifugal Launching of Jets from Accretion Disks. II. Inner Disk-driven Winds

机译:从吸积盘进行磁离心发射。二。内部磁盘驱动的风

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We numerically follow the time evolution of axisymmetric outflows magnetocentrifugally driven from the inner portion of accretion disks from their launching surface to large observable distances. Special attention is paid to the collimation of part of the outflow into a dense, narrow jet around the rotation axis after a steady state has been reached. For parameters typical of T Tauri stars, we define a fiducial "jet" as that outlined by the contour of constant density at 104 cm-3. We find that the jet, so defined, appears nearly cylindrical well above the disk, in agreement with previous asymptotic analyses. Closer to the equatorial plane, the density contour can either bulge outward or pinch inward, depending on the conditions at the launching surface, particularly the mass flux distribution. We find that even though a dense, jetlike feature is always formed around the axis, there is no guarantee that the high-density axial jet would dominate the more tenuous, wide-angle part of the wind. Specifically, on the 100 AU scale, resolvable by the Hubble Space Telescope and ground-based adaptive optics for nearby T Tauri winds, the fraction of the wind mass flux enclosed by the fiducial jet can vary substantially, again depending on the launching conditions. We show two examples in which the fraction is ~20% and ~45%. These dependences may provide a way to constrain the conditions at the launching surface, which are poorly known at present.
机译:我们从数值上跟踪从吸积盘的内部从其发射表面到大可观察距离的磁离心驱动的轴对称流出的时间演变。在达到稳定状态后,应特别注意将一部分流出的水准直成围绕旋转轴的密集而狭窄的射流。对于T Tauri恒星的典型参数,我们定义了基准“射流”,即由在104 cm-3处的恒定密度轮廓所概述的基准。我们发现,如此定义的射流在圆盘上方几乎呈圆柱形,这与先前的渐近分析一致。靠近发射赤道平面的密度轮廓可能会向外凸出或向内收缩,这取决于发射表面的情况,尤其是质量通量分布。我们发现,即使始终围绕轴形成密集的,类似喷射的特征,也不能保证高密度的轴向喷射将主导风的更微弱的广角部分。具体来说,在100 AU尺度上,哈勃太空望远镜和地面自适应光学器件可以解决附近的T Tauri风,这取决于基准喷射条件,基准射流所包围的风量通量的比例可能会发生很大变化。我们显示了两个示例,其中比例为〜20%和〜45%。这些依赖性可以提供一种方法来约束发射表面的条件,目前尚不清楚。

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