Yorita, Daisuke und Lemarechal, Jonathan und Klein, Christian und Fujita, Koji und Nagai, Hiroki (2020) Transition Detection Methods in a Pitch-sweep Test by means of TSP using Lifetime and Intensity Measurements. In: AIAA Scitech 2020 Forum (0296), 1 - 9. AIAA. AIAA Science and Technology Forum and Exposition 2020, 2020-01-06 - 2020-01-10, Orlando, FL, USA. doi: 10.2514/6.2020-0296. ISBN 978-162410595-1.
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Offizielle URL: https://doi.org/10.2514/6.2020-0296
Kurzfassung
A combination of carbon nanotube and Temperature Sensitive Paint (cntTSP) has a potential to visualize dynamic movement of the boundary-layer transition on a model surface. One wide area of application for the use of cntTSP is the continuous model pitch-sweep tests, which are desired in order to improve the data productivity of the wind tunnel. In this paper, the applicability of cntTSP to a continuous moving model (pitch-sweep test) is investigated in a low-speed wind tunnel with a simplified airplane model wing. Two TSP measurement methods, the intensity and single-shot lifetime method, and two data reduction methods for the transition detection, the maximum temperature slope method and the differential thermography methods, were examined. All methods performed in this work successfully detected the moving boundary-layer transition on the pitch-sweep model and results matched well. The advantages and technical difficulties of each method are also discussed.
elib-URL des Eintrags: | https://elib.dlr.de/134623/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Zusätzliche Informationen: | AIAA-2020-0296 | ||||||||||||||||||||||||
Titel: | Transition Detection Methods in a Pitch-sweep Test by means of TSP using Lifetime and Intensity Measurements | ||||||||||||||||||||||||
Autoren: |
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Datum: | 5 Januar 2020 | ||||||||||||||||||||||||
Erschienen in: | AIAA Scitech 2020 Forum | ||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
DOI: | 10.2514/6.2020-0296 | ||||||||||||||||||||||||
Seitenbereich: | 1 - 9 | ||||||||||||||||||||||||
Verlag: | AIAA | ||||||||||||||||||||||||
Name der Reihe: | Conference Proceedings online | ||||||||||||||||||||||||
ISBN: | 978-162410595-1 | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Temperature-sensitive paint, continous pitch traverse, Transition, TSP, CNT, low-speed | ||||||||||||||||||||||||
Veranstaltungstitel: | AIAA Science and Technology Forum and Exposition 2020 | ||||||||||||||||||||||||
Veranstaltungsort: | Orlando, FL, USA | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 6 Januar 2020 | ||||||||||||||||||||||||
Veranstaltungsende: | 10 Januar 2020 | ||||||||||||||||||||||||
Veranstalter : | AIAA | ||||||||||||||||||||||||
Institution: | Deutsches Zentrum für Luft- und Raumfahrt e.V. | ||||||||||||||||||||||||
Abteilung: | AS-EXV | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Flugzeuge | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Aircraft Research | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Simulation und Validierung (alt) | ||||||||||||||||||||||||
Standort: | Göttingen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren, GO | ||||||||||||||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||||||||||||||
Hinterlegt am: | 08 Jun 2020 13:08 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:37 |
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