TY - GEN
T1 - Modeling three-dimensional magneto-hydrodynamic phenomena in inductively coupled plasma discharges
AU - Kumar, Sanjeev
AU - Munafò, Alessandro
AU - Stephani, Kelly
AU - Bodony, Daniel J.
AU - Panesi, Marco
N1 - This work is funded by the Vannevar Bush Faculty Fellowship OUSD(RE) Grant No: N00014-21-1-295 with M. Panesi as the Principal Investigator. The work is also supported by the Center for Hypersonics and Entry Systems Studies (CHESS) at UIUC. Computations were performed on Frontera, an HPC resource provided by the Texas Advanced Computing Center (TACC) at The University of Texas at Austin, on allocation CTS20006.
PY - 2024
Y1 - 2024
N2 - The purpose of the present work is to investigate the plasma characteristics (e.g., threedimensionality, stability, turbulence) of the Plasmatron X facility using a state-of-the-art multi-physics computational framework developed at The Center for Hypersonics and Entry Systems Studies (CHESS) at the University of Illinois at Urbana-Champaign. The plasma is modeled under the Local Thermodynamic Equilibrium assumption. The flow governing equations (i.e., Navier-Stokes) are discretized in space based on a cell-centered finite volume method. Electromagnetic equations are solved in a mixed finite-element solver. The plasma and the electromagnetic solvers are coupled via the Joule heating and Lorentz forces in the energy and momentum equations and the electrical conductivity in the Maxwell equation. The steadystate simulation of the Plasmatron X torch shows that the plasma flowfield is non-axisymmetric as a result of the three-dimensional nature of the electromagnetic field induced by the helical coil. Further, a time-resolved simulation of the facility (torch along with the chamber region) reveals a significant unsteadiness in the plasma jet due to the shear layer instabilities between the hot plasma core and the cold ambient gas. These instabilities quickly break into smaller eddies and lead to a 3-dimensional flowfield in the jet region which may significantly impact the response of the material being tested in the facility.
AB - The purpose of the present work is to investigate the plasma characteristics (e.g., threedimensionality, stability, turbulence) of the Plasmatron X facility using a state-of-the-art multi-physics computational framework developed at The Center for Hypersonics and Entry Systems Studies (CHESS) at the University of Illinois at Urbana-Champaign. The plasma is modeled under the Local Thermodynamic Equilibrium assumption. The flow governing equations (i.e., Navier-Stokes) are discretized in space based on a cell-centered finite volume method. Electromagnetic equations are solved in a mixed finite-element solver. The plasma and the electromagnetic solvers are coupled via the Joule heating and Lorentz forces in the energy and momentum equations and the electrical conductivity in the Maxwell equation. The steadystate simulation of the Plasmatron X torch shows that the plasma flowfield is non-axisymmetric as a result of the three-dimensional nature of the electromagnetic field induced by the helical coil. Further, a time-resolved simulation of the facility (torch along with the chamber region) reveals a significant unsteadiness in the plasma jet due to the shear layer instabilities between the hot plasma core and the cold ambient gas. These instabilities quickly break into smaller eddies and lead to a 3-dimensional flowfield in the jet region which may significantly impact the response of the material being tested in the facility.
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U2 - 10.2514/6.2024-1648
DO - 10.2514/6.2024-1648
M3 - Conference contribution
AN - SCOPUS:85194086544
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -