Theory for the Equilibrium Discharges Interface
Equilibrium discharges (thermal plasmas) have nowadays a large range of industrial applications including cutting, welding, spraying, waste destruction, and surface treatment (Ref. 1).The current methods used for producing thermal plasmas generally employ high-intensity arcs, inductively coupled high-frequency discharges, or microwave discharges. The purpose of the Equilibrium Discharge interface is to help users model thermal plasmas generated by the first two methods (that is, arcs or inductively coupled discharges). Accordingly, the targeted applications are primarily DC and inductively coupled plasma torches as well as arc welding devices and circuit breakers.
Thermal plasmas are assumed to be under partial to complete local thermodynamic equilibrium (LTE) conditions (Ref. 1). At a macroscopic level, these kind of plasma can be considered as conductive fluid mixtures, which leads to the magnetohydrodynamics (MHD) equations. The latter combine the Navier–Stokes, heat, and Maxwell’s equations to describe the motion of the conducting fluid in an electromagnetic field.
The Equilibrium Discharge interfaces are based on a set of assumptions that lead to simplifications of the MHD equations:
The plasma is under local thermodynamic equilibrium (LTE) conditions (the electron temperature Te is approximately equal to the heavy particle temperature, Th).
Domain equations
Considering the assumptions stipulated above, the Equilibrium discharges can be described by a set of equations defined in the physics interfaces constituting the different multiphysics interfaces. Note that all the physics features available in the individual physics interfaces are also available to the multiphysics interface in use.
Energy Conservation (Heat Transfer in Fluids Interface and Equilibrium Discharge Heat Source Multiphysics Coupling Feature)
The energy conservation equation is used for all the Equilibrium Discharge interfaces.
(7-5)
The source Q (W/m3) defined in the Equilibrium Discharge Heat Source multiphysics coupling feature includes three source/sink components:
(7-6)
The definition of the electric field differs following the physics interface in use.
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(7-7)
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(7-8)
Volumetric net radiation loss Qrad defined by the total volumetric emission coefficient, which is a material property from Ref. 1.
(7-9)
Note that the enthalpy transport term prevails, for example, in the boundary layers close to electrodes in a fully ionized electric discharge, Ref. 1.
Momentum Conservation (Laminar Flow Interface)
The momentum conservation equation is used for the Equilibrium Inductively Coupled Plasma and Combined Inductive/DC Discharge interfaces.
(7-10)
Where μ is the dynamic viscosity of the fluid, I is the identity matrix and
the Lorentz force acting on the fluid defined in the magnetic field interface.
Ampère’s Law and Current Conservation (Magnetic and Electric Fields Interface)
Ampère’s law and the current conservation equations are used for the Equilibrium Discharges, In-Plane Currents interface and Equilibrium Discharges interfaces.
(7-11)
(7-12)
Where the total current density is expressed as
(7-13)
Ampère’s Law (Magnetic Fields Interface)
Ampère’s law is used for the Equilibrium Discharges, Out-of-Plane Currents interfaces. It does not solve the current conservation equation and the total current density is expressed as
(7-14)
transport properties
The above equations require specification of material properties, which are functions of temperature. The Equilibrium Discharge folder in the Material Browser contains properties for density, specific heat, viscosity, thermal conductivity and electric conductivity as a function of temperature up to 24,000 K. Available gases include air, argon, helium, hydrogen, nitrogen, and oxygen. The data is taken from the tables in the Appendix of Ref. 1.
Boundary equations
The Equilibrium Discharge interfaces include by default cooling/heating of electrodes in contact with the equilibrium discharge Ref. 2.
Ion Bombardment and Thermionic Emission at the Cathode
Positive ions from the plasma are accelerated toward the cathode and generates heat at the electrode surface. As the electrode heats up, more electrons are emitted by thermionic emission, which cause cooling of the cathode. The associated cathode heat flux is defined as:
(7-15)
Where k is the thermal conductivity (W/(m·K)), ϕs is the surface work function of the electrode (V), and Vion is the ionization potential of the plasma (V). The ion current density norm is defined by
(7-16)
where
is the normal current density at the interface and where
(7-17)
is the electron current density norm. The latter is defined by Richardson-Dushman current density if the total normal current density is larger than
(7-18)
Where AR is the Richardson’s constant (A/(m2·K2)), q is the electronic charge (C), kB is the Boltzmann’s constant (J/K), and ϕeff is the effective work function of the surface (V). Note that the ion current density norm Jion = 0 if the Richardson-Dushman current density is larger than the total normal current at the interface.
Resistive Heating at the Anode
Electron entering the anode generates heat. Following the approach presented in Ref. 2, you can assume that there is no ion current and hence no ion heating at the anode. Accordingly the anode heat flux is defined as:
(7-19)
Where
is the normal current density at the interface, k is the thermal conductivity, and ϕs is the surface work function of the anode. Note that all the physics features available in the individual interfaces are also available to the multiphysics interface in use. This include, for instance, radiation heat losses, and wall boundary conditions.