Publication | Closed Access
Modelling of plasma aerodynamic actuation driven by nanosecond SDBD discharge
84
Citations
33
References
2013
Year
EngineeringGlow DischargeFluid MechanicsPlasma PhysicsPlasma CombustionEnergy ReleasePlasma SimulationPlasma TheoryPlasma ComputationTransport PhenomenaPlasma ConfinementPulse PowerElectrical EngineeringPhysicsEnergy EquationsPropulsionAerospace EngineeringApplied PhysicsPlasma Aerodynamic ActuationAerodynamicsGas Discharge PlasmaKinetics Model
A two-dimensional air plasma kinetics model (16 species and 44 processes) for nanosecond discharge under atmospheric pressure was developed to reveal the spatial and temporal distribution of discharge characteristics of a surface dielectric barrier discharge (SDBD) actuator. An energy transfer model, including two channels for energy release from external power source to gas, was developed to couple plasma with hydrodynamics directly in the same dimension. The governing equations included the Poisson equation for the electric potential, continuity equations for each species, electron energy equations for electrons taking part in reactions, and Navier–Stokes equations for non-isothermal fluid. The model was validated through current–voltage profile and electron temperature obtained from experiments.
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