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Non-radial instabilities of isothermal Bondi accretion with a shock: vortical-acoustic cycle vs post-shock acceleration

机译:冲击产生的等温邦迪积聚的非径向不稳定性:涡声循环与震后加速度

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摘要

The linear stability of isothermal Bondi accretion with a shock is studied analytically in the asymptotic limit of high incident Mach number M_1. The flow is unstable with respect to radial perturbations as expected by Nakayama (1993), due to post-shock acceleration. Its growth time scales like the advection time from the shock r_sh to the sonic point r_son. The growth rate of non-radial perturbations l=1 is higher by a factor M_1^{2/3}, and is therefore intermediate between the advection and acoustic frequencies. Besides these instabilities based on post-shock acceleration, our study revealed another generic mechanism based on the cycle of acoustic and vortical perturbations between the shock and the sonic radius, independently of the sign of post-shock acceleration. The vortical-acoustic instability is fundamentally non-radial. It is fed by the efficient excitation of vorticity waves by the isothermal shock perturbed by acoustic waves. The growth rate exceeds the advection rate by a factor log M_1. Unstable modes cover a wide range of frequencies from the fundamental acoustic frequency ~c/r_sh up to a cut-off ~c/r_son associated with the sonic radius. The highest growth rate is reached for l=1 modes near the cut-off. The additional cycle of acoustic waves between the shock and the sonic radius is responsible for variations of the growth rate by a factor up to 3 depending on its phase relative to the vortical-acoustic cycle. The instability also exists, with a similar growth rate, below the fundamental acoustic frequency down to the advection frequency, as vorticity waves are efficiently coupled to the region of pseudosound. These results open new perspectives to address the stability of shocked accretion flows.
机译:在高入射马赫数M_1的渐近极限中,对具有冲击的等温邦迪积生的线性稳定性进行了分析研究。由于震后加速,如Nakayama(1993)所预期的,流动相对于径向扰动是不稳定的。它的生长时间像从对冲r_sh到声波点r_son的平流时间一样缩放。非径向扰动l = 1的增长速率高出M_1 ^ {2/3}倍,因此处于对流和声频之间。除了这些基于震后加速度的不稳定性之外,我们的研究还揭示了另一种基于震荡和声波半径之间的声学​​和旋涡扰动循环的通用机制,与震后加速度的信号无关。涡旋声不稳定性从根本上说是非径向的。它是由声波所扰动的等温激波有效激发涡旋波来提供的。增长率超过对流速率一个因子对数M_1。不稳定模式覆盖的频率范围很广,从基本声学频率〜c / r_sh到与声波半径相关的截止〜c / r_son。截止附近的l = 1个模式达到了最高的增长率。冲击波和声波半径之间的附加声波周期决定了增长率相对于涡旋-声波周期的相位变化高达3倍。当涡旋波有效地耦合到伪声音区域时,不稳定性也以相似的增长率存在,低于基本声频率,直到对流频率。这些结果为解决激增流的稳定性开辟了新的前景。

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    Foglizzo, T;

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  • 年度 2002
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  • 原文格式 PDF
  • 正文语种 eng
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