Haxter, Stefan und Spehr, Carsten (2013) Examination of the Influence of Flight Altitude and Speed on the Efimtsov Model Parameters. In: 19th AIAA/CEAS Aeroacoustics Conference (AIAA 2), Seiten 1-27. American Institute of Aeronautics and Astronautics Inc.. 19th AIAA/CEAS Aeroacoustics Conference (34th AIAA Aeroacoustics Conference), 2013-05-27 - 2013-05-29, Berlin, Germany. doi: 10.2514/6.2013-2028. ISBN 978-162410213-4.
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Offizielle URL: https://doi.org/10.2514/6.2013-2028
Kurzfassung
A flight test was conducted and the data was evaluated in order to investigate the influence of flight altitude and flight speed on the coherence length model by Efimtsov. An underestimation of the measured values by the model was found below a frequency of 1kHz. Above this frequency, the predicted values matched the measured values very well. The Efimtsov ansatz was found to be suitable for the description of coherence length, when the parameters are adapted. Three further analyses were performed: the flight speed was varied with constant altitude, the altitude was varied with constant flight speed, and both speed & altitude were varied together. No considerable variation was measured when the flight speed was varied separately. A small variation was determined at low frequency when the flight altitude was altered separately. When varying the parameters together, a distinct variation was found for the cases of highest speed and altitude. The applicability of the exponential coherence decay was analyzed. The absolute deviation was found to increase with lower frequency. The characteristic of the deviation was found to collapse in different regions with different scaling of the strouhal number.
elib-URL des Eintrags: | https://elib.dlr.de/77817/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||
Zusätzliche Informationen: | DOI: 10.2514/6.2013-2028 | ||||||||||||
Titel: | Examination of the Influence of Flight Altitude and Speed on the Efimtsov Model Parameters | ||||||||||||
Autoren: |
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Datum: | 24 Mai 2013 | ||||||||||||
Erschienen in: | 19th AIAA/CEAS Aeroacoustics Conference | ||||||||||||
Referierte Publikation: | Nein | ||||||||||||
Open Access: | Ja | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Ja | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
DOI: | 10.2514/6.2013-2028 | ||||||||||||
Seitenbereich: | Seiten 1-27 | ||||||||||||
Herausgeber: |
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Verlag: | American Institute of Aeronautics and Astronautics Inc. | ||||||||||||
Name der Reihe: | Conference Proceedings online | ||||||||||||
ISBN: | 978-162410213-4 | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | turbulent boundary layer, coherence length model, | ||||||||||||
Veranstaltungstitel: | 19th AIAA/CEAS Aeroacoustics Conference (34th AIAA Aeroacoustics Conference) | ||||||||||||
Veranstaltungsort: | Berlin, Germany | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsbeginn: | 27 Mai 2013 | ||||||||||||
Veranstaltungsende: | 29 Mai 2013 | ||||||||||||
Veranstalter : | American Institute of Aeronautics and Astronautics | ||||||||||||
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, GO | ||||||||||||
Hinterlegt von: | Micknaus, Ilka | ||||||||||||
Hinterlegt am: | 22 Aug 2013 13:32 | ||||||||||||
Letzte Änderung: | 24 Apr 2024 19:44 |
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