Egami, Yasuhiro und Fey, Uwe und Klein, Christian und Quest, Jürgen und Ondrus, Vladimir und Beifuss, Uwe (2012) Development of new two-component temperature-sensitive paint (TSP) for cryogenic testing. Measurement Science and Technology, 23 (11), Seiten 1-10. Institute of Physics (IOP) Publishing. doi: 10.1088/0957-0233/23/11/115301. ISSN 0957-0233.
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Offizielle URL: http://stacks.iop.org/MST/23/115301
Kurzfassung
Two-component temperature-sensitive paint (TSP) for cryogenic wind tunnels has been newly developed to extend the highest working temperature up to 320 K, whereas a conventional single-component cryoTSP operates in the temperature range from 100 to 240 K. The two-component cryoTSP includes two luminophores: a ruthenium complex (Ru(trpy)2) and a europium complex, which are very temperature sensitive in the range of 100–240 K and 220–320 K, respectively. The ruthenium complex is excited by blue light while the europium complex requires UV light. One can thence operate the two luminophores independently by illuminating the paint at different wavelengths. Both luminophores emit red light, so that it is possible to use a single camera filter to observe both luminophores. Verification tests at different cryogenic wind tunnels proved that the two-component cryoTSP could detect a boundary layer transition line even up to room temperatures with only a single coating. This means that it is neither necessary to apply a different TSP coating to a model nor use an infrared camera when the wind tunnel is operated at room temperatures. As a result, the two-component cryoTSP enables one to save time and money in cryogenic testing.
elib-URL des Eintrags: | https://elib.dlr.de/65788/ | ||||||||||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||||||||||
Zusätzliche Informationen: | Paper 115301 | ||||||||||||||||||||||||||||
Titel: | Development of new two-component temperature-sensitive paint (TSP) for cryogenic testing | ||||||||||||||||||||||||||||
Autoren: |
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Datum: | 2012 | ||||||||||||||||||||||||||||
Erschienen in: | Measurement Science and Technology | ||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||||||||||
Band: | 23 | ||||||||||||||||||||||||||||
DOI: | 10.1088/0957-0233/23/11/115301 | ||||||||||||||||||||||||||||
Seitenbereich: | Seiten 1-10 | ||||||||||||||||||||||||||||
Verlag: | Institute of Physics (IOP) Publishing | ||||||||||||||||||||||||||||
ISSN: | 0957-0233 | ||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||
Stichwörter: | temperature-sensitive paint, transition detection, laminar–turbulent flows, cryogenic wind tunnel, aerodynamics, image-based measurement technique, molecular imaging | ||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||
HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation & Validierung (alt) | ||||||||||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren | ||||||||||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||||||||||
Hinterlegt am: | 08 Okt 2012 15:44 | ||||||||||||||||||||||||||||
Letzte Änderung: | 06 Sep 2019 15:28 |
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