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Validity of sound-proof approaches in rapidly-rotating compressible convection: marginal stability versus turbulence

机译:迅速旋转可压缩对流中防腐方法的有效性:边缘稳定性与湍流

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The validity of the anelastic approximation has recently been questioned in the regime of rapidly-rotating compressible convection in low Prandtl number fluids (Calkins, Julien and Marti, Proc. R. Soc. A, 2015, vol. 471, 20140689). Given the broad usage and the high computational efficiency of sound-proof approaches in this astrophysically relevant regime, this paper clarifies the conditions for a safe application. The potential of the alternative pseudo-incompressible approximation is investigated, which in contrast to the anelastic approximation is shown to never break down for predicting the point of marginal stability. Its accuracy, however, decreases close to the parameters corresponding to the failure of the anelastic approach, which is shown to occur when the sound-crossing time of the domain exceeds a rotation time scale, i.e. for rotational Mach numbers greater than one. Concerning the supercritical case, which is naturally characterised by smaller rotational Mach numbers, we find that the anelastic approximation does not show unphysical behaviour. Growth rates computed with the linearised anelastic equations converge toward the corresponding fully compressible values as the Rayleigh number increases. Likewise, our fully nonlinear turbulent simulations, produced with our fully compressible and anelastic models and carried out in a highly supercritical, rotating, compressible, low Prandtl number regime show good agreement. However, this nonlinear test example is for only a moderately low convective Rossby number of 0.14.
机译:近似近似的Anelastic近似的有效性在低Prandtl数流体(Calkins,Julien和Marti,Proc中的快速旋转可压缩对流制度中受到质疑。R. Soc。A,2015,Vol.471,20140689)。鉴于这种天体物理相关的制度中的宽泛使用和耐妆方法的高计算效率,本文阐明了安全申请的条件。研究了替代的伪不可压缩近似的电位,与插孔近似相反,显示出从未分解以预测边缘稳定性的点。然而,其精度靠近与Anelastic方法的失败相对应的参数减小,当域的辐射时间超过旋转时间尺度时,即旋转马赫数大于1的旋转马赫数。关于超临界壳体,其自然是较小的旋转马赫数,我们发现Anelastic近似不显示不存在的行为。随着瑞利数增加,用线性化的内心式方程计算的生长速率会聚朝向相应的完全可压缩值。同样,我们的完全非线性湍流模拟,采用完全可压缩和凹凸式模型生产,并在高度超临界,旋转,可压缩,低普朗特号码方面进行了良好的一致性。然而,该非线性测试示例仅用于中等低对流rossby rossby 0.14。

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