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Schülein, Erich (2005) Experimental Investigation of Boundary Layer Transition on a Supersonic Swept Wing. DLR-Interner Bericht. DLR-IB 224 - 2005 A 15. 25 S.
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Abstract
The laminar-turbulent transition on a swept-wing leading-edge model at Mach 3 is investigated. The experiments are obtained in the Ludwieg Tube Facility at DLR Göttingen. The data contain surface pressure distributions, the location of the transition region, the structure of the limiting streamlines as well as some quantitative skin friction distributions at the upper side of the swept-wing model for the range of the unit Reynolds number and angles of attack at two different leading-edge shapes.
| Item URL in elib: | https://elib.dlr.de/21726/ | ||||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||||
| Title: | Experimental Investigation of Boundary Layer Transition on a Supersonic Swept Wing | ||||||||
| Authors: |
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| Date: | September 2005 | ||||||||
| Open Access: | No | ||||||||
| Number of Pages: | 25 | ||||||||
| Publisher: | DLR Göttingen | ||||||||
| Status: | Published | ||||||||
| Keywords: | Transition, Swept Wing, Experiment, Skin Friction | ||||||||
| 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 - Military Technologies (old) | ||||||||
| Location: | Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > High Speed Configurations | ||||||||
| Deposited By: | Schülein, Dr.rer.nat. Erich | ||||||||
| Deposited On: | 26 Jan 2006 | ||||||||
| Last Modified: | 27 Apr 2009 04:56 |
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