skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: 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:1485499
 [1];  [1]
  1. 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:
Stanford Univ., CA (United States); Univ. of Texas, Austin, TX (United States)
Sponsoring Organization:
USDOE National Nuclear Security Administration (NNSA)
Grant/Contract Number:
NA0002011
OSTI ID:
1485499
Alternate ID(s):
OSTI ID: 1363706; OSTI ID: 1363884
Journal Information:
Physics of Plasmas, Vol. 24, Issue 6; ISSN 1070-664X
Publisher:
American Institute of Physics (AIP)Copyright Statement
Country of Publication:
United States
Language:
English
Citation Metrics:
Cited by: 8 works
Citation information provided by
Web of Science

References (27)

Compact toroid formation, compression, and acceleration journal August 1993
Plasma deflagration and the properties of a coaxial plasma deflagration gun journal September 1970
Recent research in magneto-aerodynamics journal January 2001
Introduction to Plasma Physics book January 1995
Current distribution measurements inside an electromagnetic plasma gun operated in a gas-puff mode journal December 2010
Magneto-hydrodynamics simulation study of deflagration mode in co-axial plasma accelerators journal January 2014
Hyperbolic Divergence Cleaning for the MHD Equations journal January 2002
Magnetic nozzle design for coaxial plasma accelerators journal June 1995
A matrix free implicit scheme for solution of resistive magneto-hydrodynamics equations on unstructured grids journal October 2013
Finite Volume Methods for Hyperbolic Problems book January 2002
Global simulation of the solar wind-magnetosphere interaction: The importance of its numerical validity journal January 1990
Sheared Flow Stabilization of the m = 1 Kink Mode in Z Pinches journal October 1995
Radial magnetic compression in the expelled jet of a plasma deflagration accelerator journal February 2016
Performance of a Hydromagnetic Plasma Gun journal January 1960
Evidence of Stabilization in the Z -Pinch journal October 2001
Accurate and Efficient Discretization of Navier-Stokes Equations on Mixed Grids journal November 2000
Simplified Second-Order Godunov-Type Methods journal May 1988
On Godunov-type methods near low densities journal February 1991
Transport Phenomena in a Completely Ionized Gas journal March 1953
A flux-limited numerical method for solving the MHD equations to simulate propulsive plasma flows journal January 2001
Observation of current sheath transition from snowplow to deflagration journal February 1985
Applied-Field Magnetoplasmadynamic Thrusters, Part 1: Numerical Simulations Using the MACH2 Code journal September 2000
Sheared flow stabilization experiments in the ZaP flow Z pinch journal May 2003
Introduction to Plasma Physics journal January 1996
Magneto-hydrodynamics simulation study of deflagration mode in co-axial plasma accelerators
  • 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
Introduction to Plasma Physics journal October 1976
Evidence of Stabilization in the Z-Pinch text January 2001

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

Figures / Tables (7)