关于法拉第MHD发电通道内流动特性的数值分析

青木 俊之, 松尾 一泰, 近藤 信昭, 池田 利弘
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引用次数: 0

摘要

采用准一维理论,对亚音速和超音速法拉第型MHD发电机中的呛阻现象和激波的发生进行了数值分析和预测。本研究旨在为大型MHD发电机提供数据基础之一。结合安培定律和广义欧姆定律,求解了稳态一维守恒方程。结果表明,在加载系数一定的情况下,通道的极限长度随着相互作用参数的增加而减小。在一定的相互作用参数范围内,激波出现在发散通道中。最小值随加载系数的增大和摩擦系数的减小而增大,但几乎与通道入口马赫数无关。另一方面,该最大值随着加载系数和进气道马赫数的增大而增大,但几乎与摩擦系数无关。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
ファラデー型 MHD 発電チャネル内の流動特性に関する数値解析
Numerical analysis has been carried out to explain and predict the choking phenomena and the occurence of a shock wave in subsonic and supersonic Faraday type MHD generators, using a quasi-one-dimensional theory. This study is intended to provide one of data bases for a large-scale MHD generator. The steady one-dimensional conservation equations, coupled with the Ampere's law and the generalized Ohm's law, are solved. It has been shown that, in the case of a divergent channel and that a loading factor is constant, the limiting length of channel for choking decreases with an increase in an interaction parameter. A shock wave appears in a divergent channel for a certain range of the interaction parameter. The minimum value increases with an increase in the loading factor and with a decrease in the friction coefficient, but it is almost independent of the inlet Mach number of the channel. On the other hand, the maximum value increases with increases in the loading factor and in the inlet Mach number, but it is almost independent of the friction coefficient.
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