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Transition Detection by Temperature Sensitive Paint at Cryogenic Temperatures in the European Transonic Wind Tunnel (ETW)

Fey, Uwe and Egami, Yasuhiro and Iijima, Y. and Asai, K. and Jansen, U. and Quest, Jürgen (2003) Transition Detection by Temperature Sensitive Paint at Cryogenic Temperatures in the European Transonic Wind Tunnel (ETW). IEEE. 20th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF 2003), 2003-08-25 - 2003-08-29, Göttingen (Germany). ISBN 0-7803-8149-1

Full text not available from this repository.

Abstract

The identification of laminar-turbulent boundary layer transition on wind tunnel models provides essential data for modern wing design. However, simulating true flight Reynolds numbers with scaled models requires the use of cryogenic wind tunnels. Transition detection in ‘warm’ wind tunnels can be realized using commercially available IR cameras. In parallel, the temperature sensitive paint (TSP) technique is well established as an additional tool. In cryogenic testing, IR imaging becomes more difficult because of the reduction in radiated energy and the shift to longer wavelengths. Therefore, the TSP technique has become a promising alternative here. However, applying temperature sensitive paint in a large-scale cryogenic wind tunnel like the European Transonic Wind tunnel (ETW) needs specific modification of existing TSP formulations. Cooperative tests in the ETW therefore were performed by DLR and NAL (Japan). In these measurements, NAL’s paint and DLR’s mobile PSP/TSP system for data acquisition and evaluation were used. Some efforts were made to adapt the system to specific conditions given at the ETW wind tunnel. So for the first time it was successfully realized to perform a TSP luminescent paint test at cryogenic temperatures in a commercial wind tunnel.

Item URL in elib:https://elib.dlr.de/12614/
Document Type:Conference or Workshop Item (Speech, Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Transition Detection by Temperature Sensitive Paint at Cryogenic Temperatures in the European Transonic Wind Tunnel (ETW)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fey, UweUNSPECIFIEDUNSPECIFIED
Egami, YasuhiroUNSPECIFIEDUNSPECIFIED
Iijima, Y.UNSPECIFIEDUNSPECIFIED
Asai, K.National Aerospace Laboratory of Japan, NAL, 7-44-1 Jindaiji-Higashi, Chofu Tokyo 182-8522, JapanUNSPECIFIED
Jansen, U.UNSPECIFIEDUNSPECIFIED
Quest, JürgenEuropean Transonic Wind Tunnel, ETW, Ernst-Mach-Strasse 51147 Köln-PorzUNSPECIFIED
Date:2003
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 77-88
Editors:
EditorsEmail
IEEE, UNSPECIFIED
Publisher:IEEE
Series Name:Conference Proceedings ICIASF 2003 Record
ISBN:0-7803-8149-1
Status:Published
Keywords:temperature sensitive paint, TSP, cryogenic windtunnel, ETW, transition detection, cryo TSP, cryogenic testing, DLR mobile PSP system, European Transonic Windtunnel, thermal quenching, new measurement techniques
Event Title:20th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF 2003)
Event Location:Göttingen (Germany)
Event Type:international Conference
Event Dates:2003-08-25 - 2003-08-29
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 > Experimental Methods
Deposited By: Micknaus, Ilka
Deposited On:20 Dec 2005
Last Modified:14 Jan 2010 19:14

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