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高超声速等截面磁流体发电机性能研究

黄浩 黄护林 张义宁 刘振德

黄浩, 黄护林, 张义宁, 刘振德. 高超声速等截面磁流体发电机性能研究[J]. 航空动力学报, 2013, 28(3): 573-582.
引用本文: 黄浩, 黄护林, 张义宁, 刘振德. 高超声速等截面磁流体发电机性能研究[J]. 航空动力学报, 2013, 28(3): 573-582.
HUANG Hao, HUANG HU-lin, ZHANG Yi-ning, LIU Zhen-de. Performance investigation of hypersonic rectangular MHD generator[J]. Journal of Aerospace Power, 2013, 28(3): 573-582.
Citation: HUANG Hao, HUANG HU-lin, ZHANG Yi-ning, LIU Zhen-de. Performance investigation of hypersonic rectangular MHD generator[J]. Journal of Aerospace Power, 2013, 28(3): 573-582.

高超声速等截面磁流体发电机性能研究

基金项目: 高超声速冲压发动机技术重点实验室基金(20110101010);江苏高校优势学科建设工程资助

Performance investigation of hypersonic rectangular MHD generator

  • 摘要: 采用三维低磁雷诺数磁流体动力学五方程模型,对等截面管道法拉第型分段电极磁流体发电机内的流动进行数值模拟,研究了负载系数、磁场强度、电极-绝缘壁宽度比对发电通道性能的影响.结果表明:当负载系数为0.50时电功率密度达到最大,并且随着负载系数的增大发生器的减速能力降低;当磁场强度为8T时,500mm的管道长度即可将来流马赫数从6降低到3以下,温度保持在800K以下,并且每立方米的管道发电量能够达到兆瓦级的水平.

     

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出版历程
  • 收稿日期:  2012-04-04
  • 刊出日期:  2013-03-28

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