On amplitude scaling of active separation control
On amplitude scaling of active separation control
Various scaling options for the effects of excitation magnitude on the lift alternation due to zero-mass-flux periodic excitation for boundary layer separation control are examined. Physical scaling analysis leads to five amplitude parameters. The different scaling laws are examined using experimental data acquired at low Reynolds numbers and various angles of attack. The results indicate that both the velocity ratio and the momentum coefficient, commonly used for amplitude scaling of separation control applications, do not scale the current data-set. For 2D excitation with a Strouhal number of order unity, a Reynolds weighted momentum coefficient provides reasonable scaling. For 3D excitation with a Strouhal number greater than 10, the Reynolds scaled momentum coefficient, the Strouhal scaled velocity ratio and the newly defined vorticity-flux coefficient, all provide good scaling. The airfoil incidence variations are accounted for by using the velocity at the boundary layer edge at the actuation location, rather than the fixed free-stream velocity as a velocity scale. The main finding of this study is that the Reynolds number scaled momentum coefficient provides good amplitude scaling for the entire current data set.
63-80
Stalnov, Oksana
6ca7508b-4d32-4e46-9158-ef8f03795ece
Seifert, Avraham
5fa00ae2-672d-4d86-8d0d-48106c697169
26 May 2010
Stalnov, Oksana
6ca7508b-4d32-4e46-9158-ef8f03795ece
Seifert, Avraham
5fa00ae2-672d-4d86-8d0d-48106c697169
Stalnov, Oksana and Seifert, Avraham
(2010)
On amplitude scaling of active separation control.
King, Rudibert
(ed.)
In Active Flow Control II: Papers Contributed to the Conference ”Active Flow Control II 2010”, Berlin, Germany, May 26 to 28, 2010.
vol. 108,
Springer.
.
(doi:10.1007/978-3-642-11735-0_5).
Record type:
Conference or Workshop Item
(Paper)
Abstract
Various scaling options for the effects of excitation magnitude on the lift alternation due to zero-mass-flux periodic excitation for boundary layer separation control are examined. Physical scaling analysis leads to five amplitude parameters. The different scaling laws are examined using experimental data acquired at low Reynolds numbers and various angles of attack. The results indicate that both the velocity ratio and the momentum coefficient, commonly used for amplitude scaling of separation control applications, do not scale the current data-set. For 2D excitation with a Strouhal number of order unity, a Reynolds weighted momentum coefficient provides reasonable scaling. For 3D excitation with a Strouhal number greater than 10, the Reynolds scaled momentum coefficient, the Strouhal scaled velocity ratio and the newly defined vorticity-flux coefficient, all provide good scaling. The airfoil incidence variations are accounted for by using the velocity at the boundary layer edge at the actuation location, rather than the fixed free-stream velocity as a velocity scale. The main finding of this study is that the Reynolds number scaled momentum coefficient provides good amplitude scaling for the entire current data set.
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More information
Published date: 26 May 2010
Venue - Dates:
2nd Conference on Active Flow Control, Berlin, Germany, 2010-05-26 - 2010-05-28
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 352096
URI: http://eprints.soton.ac.uk/id/eprint/352096
PURE UUID: 4d4ba808-7ccf-4629-9ab3-a91565afe491
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Date deposited: 07 May 2013 09:36
Last modified: 16 Mar 2024 00:30
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Contributors
Author:
Oksana Stalnov
Author:
Avraham Seifert
Editor:
Rudibert King
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