Use of MHD systems in hypersonic aircraft

被引：0
|
作者：
V. L. Fraishtadt
A. L. Kuranov
E. G. Sheikin
机构：
[1] O.A.O. Scientific-Research Enterprise for Hypersonic Systems,
来源：
Technical Physics | 1998年 / 43卷
关键词：
Mathematical Model; Distinctive Feature; Flow Path; Engine System; Specific Impulse;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The possibilities of using magnetohydrodynamic (MHD) systems on hypersonic aircraft are discussed. The distinctive features of using MHD systems in the flow path of ramjet engines are examined. A quasi-one-dimensional mathematical model for the engine is presented which includes the MHD interaction with the flow. It is shown that the specific impulse of an engine system can be raised by using MHD systems.
引用
收藏
页码：1309 / 1313
页数：4
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