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Magnetohydrodynamic simulation study of plasma jets and plasma-surface contact in coaxial plasma accelerators

Journal Article · · Physics of Plasmas
DOI:https://doi.org/10.1063/1.4985320· OSTI ID:1363884
 [1];  [2]
  1. Univ. of Texas, Austin, TX (United States). Dept. of Aerospace Engineering and Engineering Mechanics; NNSA
  2. Univ. of Texas, Austin, TX (United States). Dept. of Aerospace Engineering and Engineering Mechanics

Recent experiments by Loebner et al. [IEEE Trans. Plasma Sci. 44, 1534 (2016)] studied the effect of a hypervelocity jet emanating from a coaxial plasma accelerator incident on target surfaces in an effort to mimic the transient loading created during edge localized mode disruption events in fusion plasmas. In this study, we present a magnetohydrodynamic (MHD) numerical model to simulate plasma jet formation and plasma-surface contact in this coaxial plasma accelerator experiment. The MHD system of equations is spatially discretized using a cell-centered finite volume formulation. The temporal discretization is performed using a fully implicit backward Euler scheme and the resultant stiff system of nonlinear equations is solved using the Newton method. The numerical model is employed to obtain some key insights into the physical processes responsible for the generation of extreme stagnation conditions on the target surfaces. Simulations of the plume (without the target plate) are performed to isolate and study phenomena such as the magnetic pinch effect that is responsible for launching pressure pulses into the jet free stream. The simulations also yield insights into the incipient conditions responsible for producing the pinch, such as the formation of conductive channels. The jet-target impact studies indicate the existence of two distinct stages involved in the plasma-surface interaction. A fast transient stage characterized by a thin normal shock transitions into a pseudo-steady stage that exhibits an extended oblique shock structure. A quadratic scaling of the pinch and stagnation conditions with the total current discharged between the electrodes is in qualitative agreement with the results obtained in the experiments. Finally, this also illustrates the dominant contribution of the magnetic pressure term in determining the magnitude of the quantities of interest.

Research Organization:
Univ. of Texas, Austin, TX (United States)
Sponsoring Organization:
USDOE National Nuclear Security Administration (NNSA)
Grant/Contract Number:
NA0002011
OSTI ID:
1363884
Alternate ID(s):
OSTI ID: 1363706
OSTI ID: 1485499
Journal Information:
Physics of Plasmas, Journal Name: Physics of Plasmas Journal Issue: 6 Vol. 24; ISSN 1070-664X
Publisher:
American Institute of Physics (AIP)Copyright Statement
Country of Publication:
United States
Language:
English

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  • Sitaraman, Hariswaran; Raja, Laxminarayan
  • 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition https://doi.org/10.2514/6.2013-207
conference January 2013

Cited By (4)

Optical emission spectroscopy investigation of the current sheet in a small-bore parallel-plate electromagnetic plasma accelerator journal November 2018
Modeling of thermalization phenomena in coaxial plasma accelerators journal April 2018
Fully coupled modeling of nanosecond pulsed plasma assisted combustion ignition journal December 2018
Computational and experimental investigation of plasma deflagration jets and detonation shocks in coaxial plasma accelerators journal February 2018

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