Numerical modelling of the MHD interaction in hypersonic flows

被引：0

作者：

Borghi, CA ^{[1
]}

Carraro, MR ^{[1
]}

Cristofolini, A ^{[1
]}

机构：

[1] Univ Bologna, Dept Elect Engn, I-40136 Bologna, Italy

来源：

2002 37TH INTERSOCIETY ENERGY CONVERSION ENGINEERING CONFERENCE (IECEC) | 2002年

关键词：

D O I：

暂无

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

A model for the analysis of the magneto-plasmadynamic regime, devoted to MHD systems in a hypersonic flight vehicle, is presented. In the model the discrete formulation of fluid dynamics and electrodinamics are coupled. The Navier-Stokes equations are discretised by means of a finite volume formulation. The electrodynamics is discretisd by means of a finite element method. The model has been utilised for the analysis of MHD interaction for the fluid control over an hypersonic body. Calculations has shown that MHD interaction can strongly affect the boundary layer fluid dynamic regime.

引用

页码：480 / 484

页数：5

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