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Mach-, Reynolds- and Sweep Effects on Active Flow Separation Control Effectivity on a 2-Element Airfoil Wing

Wild, Jochen (2014) Mach-, Reynolds- and Sweep Effects on Active Flow Separation Control Effectivity on a 2-Element Airfoil Wing. In: Acitve Flow and Combustion Control 2014 Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 127. Springer Verlag. pp. 87-100. ISBN 978-3-319-11966-3. ISSN 1612-2909

Full text not available from this repository.

Abstract

Over the last decade numerous experimental and numerical studies have been conducted by DLR together with partners regarding the maturation of active flow seperation control technologies at low speed high-lift conditions. The DLR-F15 high-lift airfoil has been established as a common test bed for such kind of investigations within the German national framework and in the scope of European Research. The present paper highlights major results of this research regarding flow seperation suppression by means of pulsed blowing.

Item URL in elib:https://elib.dlr.de/91124/
Document Type:Contribution to a Collection
Title:Mach-, Reynolds- and Sweep Effects on Active Flow Separation Control Effectivity on a 2-Element Airfoil Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wild, Jochenjochen.wild (at) dlr.deUNSPECIFIED
Date:2014
Journal or Publication Title:Acitve Flow and Combustion Control 2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:127
Page Range:pp. 87-100
Editors:
EditorsEmail
King, RudibertTU Berlin, Deutschland
Publisher:Springer Verlag
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-319-11966-3
Status:Published
Keywords:Aerodynamik, Strömungskontrolle, Hochauftrieb
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Seyfried, Beate
Deposited On:20 Oct 2014 12:01
Last Modified:13 Apr 2015 16:57

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