非麦克斯韦分布函数下碰撞对尾翼不稳定性的线性分析

IF 1.3 Q3 ORTHOPEDICS
N. Noreen, A. Shiekh, I. Habumugisha, S. Zaheer, H. Shah
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引用次数: 0

摘要

导出了在未磁化等离子体中传播的凸点-尾不稳定性的增长率。已经表征了具有谱指数r和q的(r,q)分布函数的色散关系,其最终有助于分布函数的尾部和肩部。利用太阳风数据以及指数r和q的变化值,对不同温度和数量密度比的尾部碰撞不稳定性的增长率进行了数值估计。q的较高值起到降低生长速率的作用,其中当凸块中的超热电子的数量密度较高且温度较低时,不稳定性具有较高值。最大生长速率随着电子数密度的增加而增加,并且随着凸块中温度的升高而减小。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Linear analysis of bump on tail instability with non-Maxwellian distribution function
The growth rate of bump on tail instability propagating in unmagnetized plasma has been derived. The dispersion relation has been characterized for (r, q) distribution function with spectral indices r and q which ultimately contributes towards tails and shoulder of distribution function. The growth rate of the bump on tail instability has been estimated numerically for different ratios of temperature and number density using solar wind data and also by varying values of indices r and q . The higher value of q play the role towards decreasing the growth rate where the instability has the higher value when the number density of the superthermal electrons in the bump is higher and the temperature is low. The maximum growth rate increases with the increase in number density of electrons and decreases with the increasing temperature in the bump.
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来源期刊
Plasma Research Express
Plasma Research Express Energy-Nuclear Energy and Engineering
CiteScore
2.60
自引率
0.00%
发文量
15
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