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首页> 外文期刊>The Astrophysical journal >Effect of Thermal Conduction on Acoustic Waves in Coronal Loops
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Effect of Thermal Conduction on Acoustic Waves in Coronal Loops

机译:导热对冕环中声波的影响

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The influence of classical (Spitzer) thermal conduction on longitudinal acoustic waves in a coronal loop is determined through an idealized but exactly solvable model. The model consists of an isothermal, stratified (constant gravity) atmosphere in which a monochromatic acoustic wave, traveling in the direction of decreasing density, is imposed throughout the lower half of the atmosphere. Based on the linearized equations of motion, the complete steady state (t → ∞) solution is obtained. In addition to the imposed driving wave, the solution also contains reflected and transmitted acoustic and thermal conduction waves. The mode transformation and mixing occurs in the vicinity of the atmospheric layer where the gas pressure passes through a critical value set by the magnitude of the thermal conduction and other model parameters. For 5 minute waves in a million degree loop, this critical pressure is on the order of 8 × 10-4 in cgs units. Since the apex gas pressure of many coronal loops of current interest is thought to be comfortably in excess of this value, mode mixing and transformation is not likely to be a relevant factor for understanding acoustic waves in these structures. On the other hand, enhanced thermal conductivity as a result of plasma instabilities, for example, could revive the importance of this mechanism for coronal loops. If this mixing layer is present, the calculations show that the pair of thermal conduction waves invariably gains the overwhelming majority of the energy flux of the incoming acoustic wave. This energy is rapidly dissipated in the neighborhood of the mixing layer.
机译:经典(Spitzer)热传导对冠状环中纵向声波的影响是通过理想化但可精确求解的模型确定的。该模型由等温的分层(恒重力)大气组成,其中在整个大气的下半部分施加了沿密度减小的方向传播的单色声波。基于运动的线性化方程,可以获得完整的稳态(t→∞)解。除了施加的驱动波之外,解决方案还包含反射和透射的声波和导热波。模式转换和混合发生在大气层附近,在该大气层中,气压通过由热传导大小和其他模型参数设置的临界值。对于一百万度环路中的5分钟波,该临界压力约为8×10-4(以cgs为单位)。由于当前感兴趣的许多冠状环的顶点气压被舒适地超过了该值,因此模式混合和变换不太可能成为理解这些结构中声波的相关因素。另一方面,例如,由于等离子体的不稳定性,增强的热导率可能会重新激发这种机制对冠状环的重要性。如果存在该混合层,则计算表明该对导热波始终获得入射声波的绝大多数能量通量。该能量在混合层附近迅速消散。

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