Method for calculating supersonic flows in plasmas without using artificial viscosity

In several problems related to the propagation of shock waves it was found that at the beginning the shock wave propagates in a resting cold material, and after reaching the axis (or center) of symmetry the shock wave is reflected and flows in the previously heated plasma. The shock wave can be thou...

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Detalles Bibliográficos
Autor principal: Bilbao, Luis Ernesto
Publicado: 1988
Materias:
Computer Aided Analysis
Flow of Fluids > Supersonic
Shock Waves
Abstract Only
Eulerian-Lagrangian Method
Ion Temperature
PlasmasPB - Publ by IEEECP - Piscataway, NJ, United States
Acceso en línea:https://bibliotecadigital.exactas.uba.ar/collection/paper/document/paper_NIS00744_v_n_p144_Bilbao
http://hdl.handle.net/20.500.12110/paper_NIS00744_v_n_p144_Bilbao
Aporte de:
Biblioteca Digital - Facultad de Ciencias Exactas y Naturales (UBA) de Universidad de Buenos Aires

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