Numerical simulation of argon fuelled self-field magnetoplasmadynamic thrusters using the central-upwind scheme flux interpolations
DOI10.1016/j.euromechflu.2018.07.010zbMath1408.76571OpenAlexW2883206953WikidataQ129488615 ScholiaQ129488615MaRDI QIDQ1784674
Charles Chelem Mayigué, Rodion Groll
Publication date: 27 September 2018
Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.euromechflu.2018.07.010
Lorentz forcecompressible flowmagnetohydrodynamicelectrical conductivitycentral-upwind schemesmagnetoplasmadynamic
Finite volume methods applied to problems in fluid mechanics (76M12) Magnetohydrodynamics and electrohydrodynamics (76W05) Ionized gas flow in electromagnetic fields; plasmic flow (76X05)
Cites Work
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- A pressure-based high resolution numerical method for resistive MHD
- An upwind differencing scheme for the equations of ideal magnetohydrodynamics
- The effect of nonzero \(\bigtriangledown\cdot B\) on the numerical solution of the magnetohydrodynamic equations
- A survey of several finite difference methods for systems of nonlinear hyperbolic conservation laws
- Hyperbolic divergence cleaning for the MHD equations
- A solution-adaptive upwind scheme for ideal magnetohydrodynamics
- New high-resolution central schemes for nonlinear conservation laws and convection-diffusion equations
- Computational Methods for Fluid Dynamics
- Semidiscrete Central-Upwind Schemes for Hyperbolic Conservation Laws and Hamilton--Jacobi Equations
- Fundamental Fluid Mechanics and Magnetohydrodynamics
- Implementation of semi-discrete, non-staggered central schemes in a colocated, polyhedral, finite volume framework, for high-speed viscous flows
- A pressure‐based method with AUSM‐type fluxes for MHD flows at arbitrary Mach numbers
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