Transition Detection on High-Lift Devices in the DNW-KKK by means of Temperature-Sensitive Paint
Egami, Yasuhiro and Fey, Uwe and Klein, Christian and Sitzmann, Martin and Wild, Jochen (2006) Transition Detection on High-Lift Devices in the DNW-KKK by means of Temperature-Sensitive Paint. Other.
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Abstract
Transition detection on high-lift devices of a 3D half model using the TSP technique was performed in the DNW-Cologne Cryogenic Wind Tunnel (KKK). A new method using heating foils to enhance temperature difference between laminar- and turbulent-boundary layers on a small and thin model surface were tested in order to be able to obtain the highest quality result images. Consequently, the TSP technique used with heating foils applied to a lower surface of slats showed that laminar-to-turbulent transition line on thin slats even at low temperatures and low Mach numbers could be reliably detected.
| Document Type: | Monograph (Other) | ||||||||||||
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| Title: | Transition Detection on High-Lift Devices in the DNW-KKK by means of Temperature-Sensitive Paint | ||||||||||||
| Authors: |
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| Date: | 2006 | ||||||||||||
| Journal or Publication Title: | DNW Annual Report | ||||||||||||
| Refereed publication: | No | ||||||||||||
| In SCOPUS: | No | ||||||||||||
| In ISI Web of Science: | No | ||||||||||||
| Page Range: | pp. 10-11 | ||||||||||||
| Editors: |
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| Series Name: | DNW Annual Report 2005 | ||||||||||||
| Status: | Published | ||||||||||||
| Keywords: | Temperature-Sensitive Paint (TSP), cryogenic wind tunnel, boundary layer transition, visualization | ||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||
| HGF - Program Themes: | L AR - Aircraft Research | ||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||
| DLR - Program: | L AR - Aircraft Research | ||||||||||||
| DLR - Research theme (Project): | L - Flight Physics | ||||||||||||
| Location: | Braunschweig , Göttingen | ||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Transport Aircraft Institute of Aerodynamics and Flow Technology > Experimental Methods | ||||||||||||
| Deposited By: | Ilka Micknaus | ||||||||||||
| Deposited On: | 16 Nov 2006 | ||||||||||||
| Last Modified: | 27 Apr 2009 13:13 |
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