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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