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Transition control testing in the supersonic S2MA wind tunnel (SUPERTRAC project)

Archambaud, Jean-Pierre and Arnal, Daniel and Godard, Jean-Luc and Hein, Stefan and Krier, Johann Valentin and Donelli, Raffaele S. and Hanifi, Ardeshir (2010) Transition control testing in the supersonic S2MA wind tunnel (SUPERTRAC project). In: IUTAM Bookseries, Vol. 18. Springer, Dordrecht Heidelberg London New York. pp. 75-80. ISBN 978-90-481-3722-0 (Print), 978-90-481-3723-7 (Online). ISSN 1875-3507

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Official URL: http://www.springer.com

Abstract

This paper presents an attempt to control the laminar-turbulent transition on a swept wing in supersonic flow. The first part deals with the control of the transition due to crossflow (CF) instabilities present on a swept wing, by using Micron-Sized Roughness elements (MSR); the second one is focused on the prevention of the turbulent contamination along the Leading Edge (LE), using appropriate Anti-Contamination Devices (ACD). The work includes both numerical and experimental investigation.

Document Type:Contribution to a Collection
Title:Transition control testing in the supersonic S2MA wind tunnel (SUPERTRAC project)
Authors:
AuthorsInstitution or Email of Authors
Archambaud, Jean-PierreONERA, Toulouse
Arnal, DanielONERA, Toulouse
Godard, Jean-LucONERA, Toulouse
Hein, StefanUNSPECIFIED
Krier, Johann ValentinIBK, Nürnberg
Donelli, Raffaele S.CIRA, Capua
Hanifi, ArdeshirFOI, Stockholm
Date:2010
Refereed publication:Yes
In Open Access:Yes
In ISI Web of Science:No
Volume:Vol. 18
DOI:10.1007/978-90-481-3723-7_10
Page Range:pp. 75-80
Editors:
EditorsEmail
Schlatter, P.UNSPECIFIED
Henningson, D.S.UNSPECIFIED
Publisher:Springer, Dordrecht Heidelberg London New York
Series Name:IUTAM Bookseries
ISSN:1875-3507
ISBN:978-90-481-3722-0 (Print), 978-90-481-3723-7 (Online)
Status:Published
Keywords:laminar-turbulent transition, flow control, supersonic, swept wing, attachment-line contamination, crossflow, micron-sized roughness, anti-contamination device
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Deposited By: Dr.-Ing. Stefan Hein
Deposited On:10 Dec 2008
Last Modified:27 Feb 2014 14:26

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