2020
DOI: 10.1088/1361-6463/ab6517
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Nanosecond-pulsed dielectric barrier discharge-based plasma-assisted anti-icing: modeling and mechanism analysis

Abstract: The characteristics of nanosecond-pulsed dielectric barrier discharge (nSDBD) in an anti-icing configuration is studied. The mechanisms and energy characteristics of the nSDBD-based plasma-assisted anti-icing are analyzed using a numerical model and existing experimental data. Two-dimensional simulations based on PASSKEy (PArallel Streamer Solver with KinEtics) code are conducted. The code couples a self-consistent fluid model with detailed kinetics, an efficient photo-ionization model, Euler equations and a h… Show more

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Cited by 52 publications
(38 citation statements)
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“…It is clearly seen that, at a high actuator's pulse repetition rate, practically no ice accretion on the surface occurs. In [244,245], the results of [242,243] were confirmed using the longitudinal arrangement of the electrodes of a nanosecond actuator, similar to that used in [212] to control the boundary layer separation in transonic regimes (Fig. 74).…”
Section: De-icing Plasma Systemssupporting
confidence: 54%
See 1 more Smart Citation
“…It is clearly seen that, at a high actuator's pulse repetition rate, practically no ice accretion on the surface occurs. In [244,245], the results of [242,243] were confirmed using the longitudinal arrangement of the electrodes of a nanosecond actuator, similar to that used in [212] to control the boundary layer separation in transonic regimes (Fig. 74).…”
Section: De-icing Plasma Systemssupporting
confidence: 54%
“…74). The results obtained in [242][243][244][245] show, first of all, a significant stability of the operation of ns-SDBD plasma actuators in the presence of a large amount of water and ice and snow particles in the incoming flow, as well as the prospects for the development of new plasma-assisted strategies of de-icing, specially designed to reduce the icing of aircraft in flight conditions.…”
Section: De-icing Plasma Systemsmentioning
confidence: 99%
“…Triboelectric plasma simulation was performed using 2D PASSKEy code (PArallel Streamer Solver with KinEtics), which was used in modelling nanosecond surface discharges and proved by discharge morphology, propagation velocity, voltage-current curves of triboelectric plasma, and a point-to-plane configuration generated from the experiments [37][38][39][40]. Moreover, 0D model global plasma chemistry code ZDPlasKin was also utilized in a house parameter reconstruction module [41].…”
Section: Triboelectric Plasma Simulationmentioning
confidence: 99%
“…The 2D PASSKEy (PArallel Streamer Solver with KinEtics) code is used. The code was used in modeling of nanosecond pulsed surface discharges [30][31][32] and validated by measured discharge morphology, propagation velocity, voltage-current curves of experiments, and by a point-to-plane model benchmark [33]. Detailed mathematical formulations and validations can be found in paper [30,32].…”
Section: Model Descriptionmentioning
confidence: 99%
“…The code was used in modeling of nanosecond pulsed surface discharges [30][31][32] and validated by measured discharge morphology, propagation velocity, voltage-current curves of experiments, and by a point-to-plane model benchmark [33]. Detailed mathematical formulations and validations can be found in paper [30,32]. In this section we briefly present the equations solved, and introduce the analytical model used for estimation of thrust in this work.…”
Section: Model Descriptionmentioning
confidence: 99%