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Active Separation Control on High-Lift Configurations using a URANS approach

Ciobaca, vlad and Kühn, Timo (2011) Active Separation Control on High-Lift Configurations using a URANS approach. ODAS 2011, 9-11 Februar 2011, Toulouse, Frankreich.

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This contribution discusses numerical investigations of active flow separation control for high-lift configurations under atmospheric low-speed wind tunnel conditions. A two dimensional (2D), 2-element airfoil and a three-dimensional (3D), 3-element, wing body setup are the configurations of interest. The slot-actuators are applied on the suction side of the trailing edge flap to prevent the local flow separation. The active flow control (AFC) method of choice is the pulsed blowing. This study explores the resulting effects of the flow control application on the global aerodynamic coefficients and, beyond this, by the analysis of the resulting loads variation by specific actuation parameters. The computational results highlight the ability of pulsed blowing at moderate blowing momentum coefficients to suppress the flow separation on the trailing edge flap and support the global aerodynamic enhancement.

Item URL in elib:https://elib.dlr.de/72011/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Active Separation Control on High-Lift Configurations using a URANS approach
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ciobaca, vladvlad.ciobaca (at) dlr.deUNSPECIFIED
Kühn, Timotimo.kuehn (at) dlr.deUNSPECIFIED
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:AFC, High-Lift, URANS
Event Title:ODAS 2011
Event Location:Toulouse, Frankreich
Event Type:Workshop
Event Dates:9-11 Februar 2011
HGF - Research field:other
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:no assignment
DLR - Program:no assignment
DLR - Research theme (Project):no assignment
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Ciobaca, Vlad
Deposited On:29 Nov 2011 09:19
Last Modified:29 Nov 2011 09:19

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