Jones, Michael G. und Watson, W. R. und Howerton, B. M. und Busse-Gerstengarbe, St. (2015) Effects of Mean Flow Assumption and Harmonic Distortion on Impedance Eduction Methods. AIAA Journal, Seiten 1-12. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J053399. ISSN 0001-1452.
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Kurzfassung
This investigation uses methods based on the Pridmore-Brown and convected Helmholtz equations to study the acoustic behavior of a single-layer, conventional liner fabricated by DLR, German Aerospace Center and tested in the NASA Langley Grazing Flow Impedance Tube. Two key assumptions are explored in this investigation. First, a comparison of results achieved with uniform-flow and shear-flow impedance eduction methods is considered. Second, an approach based on the Prony method is used to extend these methods from single-mode to multimode implementations. In addition, a detailed study into the effects of harmonic distortion on the educed impedance is performed, and the results are used to develop guidelines regarding acceptable levels of harmonic distortion.
elib-URL des Eintrags: | https://elib.dlr.de/94358/ | ||||||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
Titel: | Effects of Mean Flow Assumption and Harmonic Distortion on Impedance Eduction Methods | ||||||||||||||||||||
Autoren: |
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Datum: | 2015 | ||||||||||||||||||||
Erschienen in: | AIAA Journal | ||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||
In ISI Web of Science: | Ja | ||||||||||||||||||||
DOI: | 10.2514/1.J053399 | ||||||||||||||||||||
Seitenbereich: | Seiten 1-12 | ||||||||||||||||||||
Verlag: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||||||
ISSN: | 0001-1452 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | Impedance eduction, harmonic distortion, liner, acoustic damping | ||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||
HGF - Programmthema: | Antriebssysteme | ||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
DLR - Forschungsgebiet: | L ER - Engine Research | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Turbinentechnologien (alt) | ||||||||||||||||||||
Standort: | Berlin-Charlottenburg | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Antriebstechnik > Triebwerksakustik | ||||||||||||||||||||
Hinterlegt von: | Bake, Dr.-Ing. Friedrich | ||||||||||||||||||||
Hinterlegt am: | 15 Jan 2015 14:08 | ||||||||||||||||||||
Letzte Änderung: | 22 Jun 2023 10:29 |
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