Numerical modelling of the MHD interaction in hypersonic flows

Author

Borghi, Carlo A. ; Carraro, Mario R. ; Cristofolini, Andrea

Author_Institution

Dept. of Electr. Eng., Bologna Univ., Italy

fYear

2004

fDate

29-31 July 2004

Firstpage

480

Lastpage

484

Abstract

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 electrodynamics are coupled. The Navier-Stokes equations are discretised by means of a finite volume formulation. The electrodynamics is discretised by means of a finite element method. The model has been utilised for the analysis of MHD interaction for the fluid control over a hypersonic body. Calculations have shown that MHD interaction can strongly affect the boundary layer fluid dynamic regime.

Keywords

Navier-Stokes equations; electrodynamics; finite element analysis; finite volume methods; flow control; hypersonic flow; plasma boundary layers; plasma magnetohydrodynamics; MHD interaction; Navier-Stokes equations; discrete formulation; electrodynamics; finite element method; finite volume formulation; fluid control; fluid dynamic regime; hypersonic flight vehicle; hypersonic flows; magneto-plasmadynamic regime; numerical modelling; DC generators; Equations; Fluid dynamics; Fluid flow control; Ionization; Magnetic analysis; Magnetohydrodynamics; Numerical models; Space vehicles; Temperature control;

fLanguage

English

Publisher

ieee

Conference_Titel

Energy Conversion Engineering Conference, 2002. IECEC '02. 2002 37th Intersociety

Print_ISBN

0-7803-7296-4

Type

conf

DOI

10.1109/IECEC.2002.1392087

Filename

1392087