Robust control of flow separation over a pitching aerofoil using plasma actuators

We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma actuators. Despite the complexity of the dynamics of interest, we show how the problem of controlling flow separation can be formulated as a simple output regulation problem, so that a simple control st...

Full description

Bibliographic Details
Main Authors: Pasquale, Laura, Broglia, R., Choi, K.S., Durante, D., Zanchetta, Pericle
Format: Article
Published: Elsevier 2017
Subjects:
Online Access:https://eprints.nottingham.ac.uk/48247/
_version_ 1848797723963162624
author Pasquale, Laura
Broglia, R.
Choi, K.S.
Durante, D.
Zanchetta, Pericle
author_facet Pasquale, Laura
Broglia, R.
Choi, K.S.
Durante, D.
Zanchetta, Pericle
author_sort Pasquale, Laura
building Nottingham Research Data Repository
collection Online Access
description We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma actuators. Despite the complexity of the dynamics of interest, we show how the problem of controlling flow separation can be formulated as a simple output regulation problem, so that a simple control strategy may be used. A robust multivariable feedback control is designed and tested in a configuration with two actuator/sensor pairs. Accurate numerical simulations of incompressible flows on a pitching NACA 0012 at Reynolds Re = 20,000 are performed in order to illustrate the effectiveness of the proposed approach. Robust, fast flow reattachment is achieved, along with both stabilisation and increase/reduction of the lift/drag, respectively. The control system shows good dynamic performances, as the angle of attack is varied. The chosen output can be experimentally measured by appropriate sensors and the extension of the proposed approach to 3D configurations is straightforward.
first_indexed 2025-11-14T20:08:25Z
format Article
id nottingham-48247
institution University of Nottingham Malaysia Campus
institution_category Local University
last_indexed 2025-11-14T20:08:25Z
publishDate 2017
publisher Elsevier
recordtype eprints
repository_type Digital Repository
spelling nottingham-482472020-05-04T19:13:10Z https://eprints.nottingham.ac.uk/48247/ Robust control of flow separation over a pitching aerofoil using plasma actuators Pasquale, Laura Broglia, R. Choi, K.S. Durante, D. Zanchetta, Pericle We address the problem of controlling the unsteady flow separation over an aerofoil, using plasma actuators. Despite the complexity of the dynamics of interest, we show how the problem of controlling flow separation can be formulated as a simple output regulation problem, so that a simple control strategy may be used. A robust multivariable feedback control is designed and tested in a configuration with two actuator/sensor pairs. Accurate numerical simulations of incompressible flows on a pitching NACA 0012 at Reynolds Re = 20,000 are performed in order to illustrate the effectiveness of the proposed approach. Robust, fast flow reattachment is achieved, along with both stabilisation and increase/reduction of the lift/drag, respectively. The control system shows good dynamic performances, as the angle of attack is varied. The chosen output can be experimentally measured by appropriate sensors and the extension of the proposed approach to 3D configurations is straightforward. Elsevier 2017-10-18 Article PeerReviewed Pasquale, Laura, Broglia, R., Choi, K.S., Durante, D. and Zanchetta, Pericle (2017) Robust control of flow separation over a pitching aerofoil using plasma actuators. IFAC Papers Online, 50 (1). pp. 11120-11125. ISSN 1474-6670 Flow control Robust control Flow separation Plasma actuators Boundary layer control http://www.sciencedirect.com/science/article/pii/S2405896317314763 doi:10.1016/j.ifacol.2017.08.1000 doi:10.1016/j.ifacol.2017.08.1000
spellingShingle Flow control
Robust control
Flow separation
Plasma actuators
Boundary layer control
Pasquale, Laura
Broglia, R.
Choi, K.S.
Durante, D.
Zanchetta, Pericle
Robust control of flow separation over a pitching aerofoil using plasma actuators
title Robust control of flow separation over a pitching aerofoil using plasma actuators
title_full Robust control of flow separation over a pitching aerofoil using plasma actuators
title_fullStr Robust control of flow separation over a pitching aerofoil using plasma actuators
title_full_unstemmed Robust control of flow separation over a pitching aerofoil using plasma actuators
title_short Robust control of flow separation over a pitching aerofoil using plasma actuators
title_sort robust control of flow separation over a pitching aerofoil using plasma actuators
topic Flow control
Robust control
Flow separation
Plasma actuators
Boundary layer control
url https://eprints.nottingham.ac.uk/48247/
https://eprints.nottingham.ac.uk/48247/
https://eprints.nottingham.ac.uk/48247/