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A Unified Hyperbolic Model for Coupled Fluid Dynamics and Electromagnetics in Aerospace Applications

机译:航空航天应用中流体动力学和电磁耦合的统一双曲模型

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This paper details the development a unified hyperbolic model for fluid dynamics coupled to electromagnetics. The advantage to the model presented is that it includes the accurate physical behavior for several plasmas of aerospace interest; it can effectively capture both magnetohydrodynamic and electrohydrodynamic limits of the plasma, in addition to low-conductivity effects that expose the wave nature of the electromagnetic field. The approach is useful because of its potential for simplifying existing implementations towards multiphysics simulations of aerospace plasmas, eliminating the need for multiple implementations for different plasma models. In previous work, a Riemann solver approach and a flux-splitting approach have been introduced for this model. Here, we review their individual merits, present some assessment simulation results using both approaches, and compare them.
机译:本文详细介绍了如何为耦合到电磁的流体动力学建立统一的双曲模型。所提出的模型的优点在于,它包括针对航空航天领域的几种等离子体的精确物理行为;除了可以暴露电磁场波动特性的低电导率效应外,它还可以有效地捕获等离子体的磁流体动力学和电流体动力学极限。该方法之所以有用,是因为它有可能简化现有的实现方法,以简化航空等离子体的多物理场模拟,从而消除了针对不同等离子体模型的多种实现方法的需求。在以前的工作中,已经为该模型引入了黎曼求解器方法和通量分裂方法。在这里,我们回顾了它们的优点,提出了使用这两种方法的评估模拟结果,并进行了比较。

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