Boundary condition modifications of the Suzen-Huang plasma actuator model

The accuracy of the Suzen-Huang (S-H) model is improved by altering the boundary condition of the dielectric surface above the lower electrode. For the equation governing the electric field, we introduce a ‘dielectric shielding’ condition at the same region, which results in a spread of the electric...

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Main Authors: Ibrahim, Imran H., Skote, Martin
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2014
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Online Access:https://hdl.handle.net/10356/101731
http://hdl.handle.net/10220/19358
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1017312023-03-04T17:19:41Z Boundary condition modifications of the Suzen-Huang plasma actuator model Ibrahim, Imran H. Skote, Martin School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering The accuracy of the Suzen-Huang (S-H) model is improved by altering the boundary condition of the dielectric surface above the lower electrode. For the equation governing the electric field, we introduce a ‘dielectric shielding’ condition at the same region, which results in a spread of the electric field strength along the dielectric surface. For the equation governing the surface charge density, we introduce boundary conditions that modify the behavior of the charge density variable in the S-H model. The conditions represent a fitting procedure by adding the features of propagation and dissipation in a one-dimensional Fokker-Plank equation. The equation is initiated by a normal distribution function centered at the leading edge of the lower electrode. These modifications improved model results by about 50% when comparing the maximum induced velocity value with experimental results. Furthermore, charge density growth is propagating in a similar manner to that obtained by charge transport models. Published version 2014-05-19T01:17:47Z 2019-12-06T20:43:30Z 2014-05-19T01:17:47Z 2019-12-06T20:43:30Z 2012 2012 Journal Article Ibrahim, I. H., & Skote, M. (2011). Boundary condition modifications of the Suzen-Huang plasma actuator model. International Journal of Flow Control, 3(2/3), 111-132. 174064 1756-8250 https://hdl.handle.net/10356/101731 http://hdl.handle.net/10220/19358 10.1260/1756-8250.3.2-3.111 174064 en International journal of flow control © 2012 Multi Science Publishing. This paper was published in International journal of flow control and is made available as an electronic reprint (preprint) with permission of Multi Science Publishing. The paper can be found at the following official DOI: [http://dx.doi.org/10.1260/1756-8250.3.2-3.111].  One print or electronic copy may be made for personal use only. Systematic or multiple reproduction, distribution to multiple locations via electronic or other means, duplication of any material in this paper for a fee or for commercial purposes, or modification of the content of the paper is prohibited and is subject to penalties under law. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering
spellingShingle DRNTU::Engineering::Aeronautical engineering
Ibrahim, Imran H.
Skote, Martin
Boundary condition modifications of the Suzen-Huang plasma actuator model
description The accuracy of the Suzen-Huang (S-H) model is improved by altering the boundary condition of the dielectric surface above the lower electrode. For the equation governing the electric field, we introduce a ‘dielectric shielding’ condition at the same region, which results in a spread of the electric field strength along the dielectric surface. For the equation governing the surface charge density, we introduce boundary conditions that modify the behavior of the charge density variable in the S-H model. The conditions represent a fitting procedure by adding the features of propagation and dissipation in a one-dimensional Fokker-Plank equation. The equation is initiated by a normal distribution function centered at the leading edge of the lower electrode. These modifications improved model results by about 50% when comparing the maximum induced velocity value with experimental results. Furthermore, charge density growth is propagating in a similar manner to that obtained by charge transport models.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Ibrahim, Imran H.
Skote, Martin
format Article
author Ibrahim, Imran H.
Skote, Martin
author_sort Ibrahim, Imran H.
title Boundary condition modifications of the Suzen-Huang plasma actuator model
title_short Boundary condition modifications of the Suzen-Huang plasma actuator model
title_full Boundary condition modifications of the Suzen-Huang plasma actuator model
title_fullStr Boundary condition modifications of the Suzen-Huang plasma actuator model
title_full_unstemmed Boundary condition modifications of the Suzen-Huang plasma actuator model
title_sort boundary condition modifications of the suzen-huang plasma actuator model
publishDate 2014
url https://hdl.handle.net/10356/101731
http://hdl.handle.net/10220/19358
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