2011
DOI: 10.4208/cicp.250509.210610a
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A Discontinuous Galerkin Method for Ideal Two-Fluid Plasma Equations

Abstract: Abstract.A discontinuous Galerkin method for the ideal 5 moment two-fluid plasma system is presented. The method uses a second or third order discontinuous Galerkin spatial discretization and a third order TVD Runge-Kutta time stepping scheme. The method is benchmarked against an analytic solution of a dispersive electron acoustic square pulse as well as the two-fluid electromagnetic shock [1] and existing numerical solutions to the GEM challenge magnetic reconnection problem [2]. The algorithm can be generali… Show more

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Cited by 55 publications
(51 citation statements)
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“…The discontinuous Galerkin method is selected for its robustness to work well for kinetic equations in phase space, Maxwell's electromagnetic equations, and fluid equations in physical space with multiple contemporary examples for these application areas [12,13,14,15,16,17,18]. Additionally, the explicit method is straightforward to implement and well suited for emerging high performance computing architectures as described in Chapters 4 and 9.…”
Section: Methodsmentioning
confidence: 99%
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“…The discontinuous Galerkin method is selected for its robustness to work well for kinetic equations in phase space, Maxwell's electromagnetic equations, and fluid equations in physical space with multiple contemporary examples for these application areas [12,13,14,15,16,17,18]. Additionally, the explicit method is straightforward to implement and well suited for emerging high performance computing architectures as described in Chapters 4 and 9.…”
Section: Methodsmentioning
confidence: 99%
“…With fluctuations in physical space propagating only as perturbation of these macroscopic parameters, a fluid model is appropriate [2,10,11,12]. The Euler-fluid plasma model equations adequately describe compressible inviscid fluid,…”
Section: Euler -Maxwell Fluid Modelmentioning
confidence: 99%
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“…1(a) and 1(b) with the letters denoting the types of shocks/waves. 6,20,21,36 The part denoted by "SS" is slow shock. As observed, the slow shock structure is greatly altered in the XMHD results.…”
Section: A Brio-wu Shock Tube Testmentioning
confidence: 99%
“…Simulations were performed using the USim code (formerly called Nautilus) [42,43]. Algorithms on which USim is based have been verified against shock-relevant problems [44,45]. In the simulations, the jets are assumed to be 100% Ar ii with initial n e = n i = 10 14 cm −3 , T e = T i = 1.4 eV, and velocities of ±6.2 km/s (i.e., transverse component of V jet ≈ 30 km/s).…”
mentioning
confidence: 99%