Broszat, D. und Tapken, U. und Enghardt, L. und Lengani, D. und Marn, A. (2011) Validation of an integrated acoustic absorber in a turbine exit guide vane. In: Proceedings 17th AIAA / CEAS Aeroacoustics Conference (32nd Aeroacoustics Conference). AIAA. 17th AIAA / CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), 2011-06-05 - 2011-06-08, Portland, USA.
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Kurzfassung
Within the scope of previous papers, the general setup of an acoustic turbine test facility at the Graz University of Technology has been presented. In addition, its significance for the validation of acoustic prediction tools and the verification of noise reduction features related to the LPT (Low Pressure Turbine) has been highlighted. In contrast to the passive noise reduction feature presented last year, the purpose of the present paper is the verification of an innovative integrated acoustic absorber. It considerably extends the available area for acoustic lining in the tailpipe downstream of the LPT by integrating it into the Turbine Exit Case (TEC). The innovative absorber has been acoustically designed for a maximum area utilization and tested at the above mentioned cold flow LPT rig. In parallel, numerical predictions based on the MTU in-house Linearized Euler (LEE) tool have been performed and compared to the results of the experimental investigations. The results show a very promising noise reduction potential of the integrated TEC absorber with a relatively broadband attenuation characteristic that allowed for a noticeable effect at all three acoustic operating conditions as well as the first and second Blade Passage Frequency (BPF). In addition, they, again, demonstrate the adequate correlation of the LEE predictions with the experimental data and its qualification as a design tool.
elib-URL des Eintrags: | https://elib.dlr.de/74140/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||||||||||
Titel: | Validation of an integrated acoustic absorber in a turbine exit guide vane | ||||||||||||||||||||||||
Autoren: |
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Datum: | 2011 | ||||||||||||||||||||||||
Erschienen in: | Proceedings 17th AIAA / CEAS Aeroacoustics Conference (32nd Aeroacoustics Conference) | ||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Verlag: | AIAA | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | turbo machinery, turbine noise, aeroacoustics, noise source identification, noise prediction, duct acoustics, acoustic absorber | ||||||||||||||||||||||||
Veranstaltungstitel: | 17th AIAA / CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference) | ||||||||||||||||||||||||
Veranstaltungsort: | Portland, USA | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 5 Juni 2011 | ||||||||||||||||||||||||
Veranstaltungsende: | 8 Juni 2011 | ||||||||||||||||||||||||
Veranstalter : | AIAA | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Antriebe (alt) | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | L ER - Antriebsforschung | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Verdichtertechnologien (alt) | ||||||||||||||||||||||||
Standort: | Berlin-Adlershof | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Antriebstechnik > Triebwerksakustik | ||||||||||||||||||||||||
Hinterlegt von: | Kaur, Balbir | ||||||||||||||||||||||||
Hinterlegt am: | 20 Jan 2012 12:34 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:40 |
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