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Linear stability of magnetohydrodynamic flow in a square duct with thin conducting walls

机译:导电壁薄的方管中磁流体动力流动的线性稳定性

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摘要

This study is concerned with the numerical linear stability analysis of liquid-metal flow in a square duct with thin electrically conducting walls subject to a uniform transverse magnetic field. We derive an asymptotic solution for the base flow that is valid for not only high but also moderate magnetic fields. This solution shows that, for low wall conductance ratios c≪1, an extremely strong magnetic field with Hartmann number Ha∼c−4 is required to attain the asymptotic flow regime considered in previous studies. We use a vector streamfunction–vorticity formulation and a Chebyshev collocation method to solve the eigenvalue problem for three-dimensional small-amplitude perturbations in ducts with realistic wall conductance ratios c=1, 0.1 and 0.01 and Hartmann numbers up to 104. As for similar flows, instability in a sufficiently strong magnetic field is found to occur in the sidewall jets with characteristic thickness δ∼Ha−1/2. This results in the critical Reynolds number and wavenumber increasing asymptotically with the magnetic field as Rec∼110Ha1/2 and kc∼0.5Ha1/2. The respective critical Reynolds number based on the total volume flux in a square duct with c≪1 is Re¯¯¯¯c≈520. Although this value is somewhat larger than Re¯¯¯¯c≈313 found by Ting et al. (Intl J. Engng Sci., vol. 29 (8), 1991, pp. 939–948) for the asymptotic sidewall jet profile, it still appears significantly lower than the Reynolds numbers at which turbulence is observed in experiments as well as in direct numerical simulations of this type of flow.
机译:这项研究涉及在具有均匀的横向磁场的薄壁导电壁的方管中液态金属流动的数值线性稳定性分析。我们导出了基本流的渐近解,该解不仅适用于高磁场,而且适用于中等磁场。该解决方案表明,对于低壁电导率c≪1,需要具有哈特曼数Ha〜c-4的极强磁场,才能获得先前研究中考虑的渐近流动状态。我们使用矢量流函数-涡度公式和Chebyshev搭配方法来解决导管壁电导率为c = 1、0.1和0.01且Hartmann数高达104的三维小振幅扰动的特征值问题。流动时,发现具有特征厚度δ〜Ha-1 / 2的侧壁射流中发生了在足够强的磁场中的不稳定性。这导致临界雷诺数和波数随着磁场Rec〜110Ha1 / 2和kc〜0.5Ha1 / 2渐近增加。基于具有c≪1的方管中的总体积通量的临界雷诺数为Re¯¯c≈520。尽管该值比Ting等人发现的Re¯¯c≈313大一些。 (Intl J. Engng Sci。,vol。29(8),1991,pp。939-948)的渐近侧壁射流轮廓,它仍然显着低于在实验以及这种类型的流动的直接数值模拟。

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    Priede J.; Arlt T.; Bühler L.;

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  • 年度 2015
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  • 正文语种 {"code":"en","name":"English","id":9}
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