Hein, Stefan and Schülein, Erich and Hanifi, Ardeshir and Sousa, Joao and Arnal, Daniel (2010) Laminar flow control by suction at Mach 2. In: IUTAM Bookseries, Vol. 18. Springer, Dordrecht Heidelberg London New York. pp. 189-194. doi: 10.1007/978-90-481-3723-7_29. 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
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/ | ||||||||||||||||||||||||
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Document Type: | Contribution to a Collection | ||||||||||||||||||||||||
Title: | Laminar flow control by suction at Mach 2 | ||||||||||||||||||||||||
Authors: |
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Date: | 2010 | ||||||||||||||||||||||||
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: |
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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 | ||||||||||||||||||||||||
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: | 24 Apr 2024 19:21 |
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