elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Laminar flow control by suction at Mach 2

Hein, Stefan and Schülein, Erich and Hanifi, Ardeshir and Sousa, Joao and Arnal, Daniel (2010) Laminar flow control by suction at Mach 2. In: Seventh IUTAM Symposium on Laminar-Turbulent Transition IUTAM Bookseries, Vol. 18. Springer, Dordrecht Heidelberg London New York. pp. 189-194. ISBN 978-90-481-3722-0 (Print), 978-90-481-3723-7 (Online). ISSN 1875-3507

Full text not available from this repository.

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

Abstract

A wind-tunnel experiment on laminar flow control by suction at Mach 2 has been performed for an infinite swept-wing configuration. A significant delay of laminar-turbulent transition could be achieved in this experiment using a suction panel manufactured from porous sinter material. The transition locations from experiment were used to determine the corresponding transition N-factor values. The transition N-factor values obtained for the different test cases are independent of the suction rate and moreover similar to those found for the reference model without suction panel.

Item URL in elib:https://elib.dlr.de/56831/
Document Type:Contribution to a Collection
Title:Laminar flow control by suction at Mach 2
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hein, StefanUNSPECIFIEDUNSPECIFIED
Schülein, ErichUNSPECIFIEDUNSPECIFIED
Hanifi, ArdeshirFOI, StockholmUNSPECIFIED
Sousa, JoaoIST, LisboaUNSPECIFIED
Arnal, DanielONERA, ToulouseUNSPECIFIED
Date:2010
Journal or Publication Title:Seventh IUTAM Symposium on Laminar-Turbulent Transition
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 18
DOI :10.1007/978-90-481-3723-7_29
Page Range:pp. 189-194
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, supersonic swept wing, flow control, suction
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Institute of Aerodynamics and Flow Technology > High Speed Configurations
Deposited By: Hein, Dr.-Ing. Stefan
Deposited On:11 Dec 2008
Last Modified:25 May 2010 13:00

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.