The MHD interaction around a conical test body in a hypersonic argon flow is experimentally investigated. The aim of the experiment is to produce a data base to be used for the validation of numerical codes for the analysis and the simulation of the magneto-fluid dynamics in hypersonic flows. In these experiments the flow is realized in the high-enthalpy arc-heated hypersonic wind tunnel - HEAT - of Alta (Pisa-Italy). Speeds at Mach 6 have been realized. In the present experiment the flow and the plasma characteristics have been determined. The MHD interaction is obtained in the shock layer of a conical test body placed at the exit of the hypersonic nozzle. The electrical configuration realized, allows enhancing the effect of the MHD interaction on the plasma parameters. This is done by utilizing the Hall field to generate the MHD interaction and by short-circuiting the Faraday current inside the%

MHD Iteraction on Sharp Bodies in Hypersonic Flows / A. Cristofolini; C. A. Borghi; M. R. Carraro; G. Neretti; A. Passaro; G. Fantoni; L. Biagioni. - ELETTRONICO. - (2007), pp. AIAA-2007-4136-AIAA-2007-4136. (Intervento presentato al convegno 38th AIAA Plasmadynamics and Lasers Conference In conjunction with the 16th International Conference on MHD Energy Conversion tenutosi a Miami, FL, USA nel 25-28 giugno 2007).

MHD Iteraction on Sharp Bodies in Hypersonic Flows

CRISTOFOLINI, ANDREA;BORGHI, CARLO ANGELO;CARRARO, MARIO ROBERTO;NERETTI, GABRIELE;
2007

Abstract

The MHD interaction around a conical test body in a hypersonic argon flow is experimentally investigated. The aim of the experiment is to produce a data base to be used for the validation of numerical codes for the analysis and the simulation of the magneto-fluid dynamics in hypersonic flows. In these experiments the flow is realized in the high-enthalpy arc-heated hypersonic wind tunnel - HEAT - of Alta (Pisa-Italy). Speeds at Mach 6 have been realized. In the present experiment the flow and the plasma characteristics have been determined. The MHD interaction is obtained in the shock layer of a conical test body placed at the exit of the hypersonic nozzle. The electrical configuration realized, allows enhancing the effect of the MHD interaction on the plasma parameters. This is done by utilizing the Hall field to generate the MHD interaction and by short-circuiting the Faraday current inside the%
2007
AIAA Meeting Papers on disc, 38th AIAA Plasmadynamics and Lasers Conference
AIAA-2007-4136
AIAA-2007-4136
MHD Iteraction on Sharp Bodies in Hypersonic Flows / A. Cristofolini; C. A. Borghi; M. R. Carraro; G. Neretti; A. Passaro; G. Fantoni; L. Biagioni. - ELETTRONICO. - (2007), pp. AIAA-2007-4136-AIAA-2007-4136. (Intervento presentato al convegno 38th AIAA Plasmadynamics and Lasers Conference In conjunction with the 16th International Conference on MHD Energy Conversion tenutosi a Miami, FL, USA nel 25-28 giugno 2007).
A. Cristofolini; C. A. Borghi; M. R. Carraro; G. Neretti; A. Passaro; G. Fantoni; L. Biagioni
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11585/57936
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