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Simulation of plasma flows in self-field Lorentz force accelerators.

机译:在自场洛伦兹力加速器中模拟等离子体流动。

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A characteristics-based scheme for the solution of ideal MHD equations was developed, and its ability to capture time-dependent discontinuities monotonically, as well as maintain force-free equilibrium, was demonstrated. Detailed models of classical transport, real equations of state, multi-level ionization models, anomalous transport, and multi-temperature effects for argon and lithium plasmas were implemented in this code. The entire set of equations was solved on non-orthogonal meshes, using parallel computers, to provide realistic description of flowfields in various thruster configurations. The calculated flowfield in gas-fed magnetoplasmadynamic thrusters (MPDT), such as the full-scale benchmark thruster (FSBT), compared favorably with measurements. These simulations provided insight into some aspects of FSBT operation, such as the weak role of the anode geometry in affecting the coefficient of thrust, the predominantly electromagnetic nature of the thrust at nominal operating conditions, and the importance of the near-cathode region in energy dissipation. Furthermore, the simulated structure of the flow embodied a number of photographically-recorded features of the FSBT discharge. Based on the confidence gained from its success with gas-fed MPDT flows, this code was then used to study a promising high-power spacecraft thruster, the lithium Lorentz force accelerator (LiLFA), in order to uncover its interior plasma properties and to obtain insight into underlying physical processes that had been poorly understood. The simulated flowfields of density, velocity, ionization, and anomalous resistivity were shown to change qualitatively with the total current. The simulations show the presence of a velocity reducing shock at low current, which disappeared as the current was increased above the value corresponding to nominal operation. The breakdown and scaling of the various components of thrust and power were revealed. The line on which the magnetic pressure equaled the gasdynamic pressure, and its motion with increasing current, was shown to provide a clear illustration of the anode starvation mechanism that leads to the current conduction crisis called onset.
机译:提出了一种基于特征的理想MHD方程求解方案,并证明了其能够单调捕获时间相关的不连续性以及保持无力平衡的能力。在此代码中实现了经典输运的详细模型,真实的状态方程,多级电离模型,异常输运以及氩和锂等离子体的多温度效应。使用并行计算机在非正交网格上求解了整个方程组,以提供各种推进器配置中流场的真实描述。气源磁等离子体动力推进器(MPDT)(例如满量程基准推进器(FSBT))中的计算流场与测量结果相比具有优势。这些模拟为FSBT操作的某些方面提供了见识,例如阳极几何形状在影响推力系数方面的弱作用,在正常工作条件下推力的主要电磁性质以及近阴极区在能量中的重要性耗散。此外,流动的模拟结构体现了FSBT放电的许多照相记录特征。基于成功使用气体馈送MPDT流程获得的信心,此代码随后用于研究有前途的大功率航天器推进器,即洛伦兹力加速器锂(LiLFA),以发现其内部等离子体特性并获得深入了解尚未了解的基本物理过程。结果表明,密度,速度,电离和反常电阻率的模拟流场随总电流发生质的变化。仿真显示在低电流下存在降低速度的冲击,当电流增加到对应于标称运行的值以上时,该冲击消失。揭示了推力和动力各组成部分的分解和定标。磁力线等于气体动力压力的线及其随电流增加而运动的线,清楚地说明了导致电流传导危机(称为开始)的阳极饥饿机制。

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