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

机译:具有冲击的等温邦迪增生的非径向不稳定性:   旋涡声学循环与震后加速

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摘要

The linear stability of isothermal Bondi accretion with a shock is studiedanalytically in the asymptotic limit of high incident Mach number M_1. The flowis unstable with respect to radial perturbations as expected by Nakayama(1993), due to post-shock acceleration. Its growth time scales like theadvection time from the shock r_sh to the sonic point r_son. The growth rate ofnon-radial perturbations l=1 is higher by a factor M_1^{2/3}, and is thereforeintermediate between the advection and acoustic frequencies. Besides theseinstabilities based on post-shock acceleration, our study revealed anothergeneric mechanism based on the cycle of acoustic and vortical perturbationsbetween the shock and the sonic radius, independently of the sign of post-shockacceleration. The vortical-acoustic instability is fundamentally non-radial. Itis fed by the efficient excitation of vorticity waves by the isothermal shockperturbed by acoustic waves. The growth rate exceeds the advection rate by afactor log M_1. Unstable modes cover a wide range of frequencies from thefundamental acoustic frequency ~c/r_sh up to a cut-off ~c/r_son associated withthe sonic radius. The highest growth rate is reached for l=1 modes near thecut-off. The additional cycle of acoustic waves between the shock and the sonicradius is responsible for variations of the growth rate by a factor up to 3depending on its phase relative to the vortical-acoustic cycle. The instabilityalso exists, with a similar growth rate, below the fundamental acousticfrequency down to the advection frequency, as vorticity waves are efficientlycoupled to the region of pseudosound. These results open new perspectives toaddress the stability of shocked accretion flows.
机译:在高入射马赫数M_1的渐近极限条件下,对具有冲击的等温邦迪积体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。它的增长时间像从冲击r_sh到声波点r_son的平流时间一样缩放。非径向扰动l = 1的增长率较高,为M_1 ^ {2/3}倍,因此介于对流频率和声频之间。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​​和涡旋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。它是由等温冲击波有效地激发声波所激发的。增长率超过对流速率一个因子日志M_1。不稳定模式覆盖从基本声学频率〜c / r_sh到与声波半径相关的截止〜c / r_son的宽范围频率。截止点附近的l = 1个模式达到最高的增长率。冲击波和声波半径之间的附加声波周期决定了增长率的变化,取决于其相对于涡旋-声波周期的相位,其变化高达3倍。当涡旋波有效地耦合到伪声波区域时,不稳定性也以相似的增长率存在,低于基本声波频率直至平流频率。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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