Hirschberg, Lionel und Bake, Friedrich und Knobloch, Karsten und Hulshoff, Steven J. (2021) Swirl-Nozzle Interaction Experiments: Influence of Injection-Reservoir Pressure and Injection Time. In: AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021. 27th AIAA/CEAS Aeroacoustics Conference / AIAA AVIATION 2021 FORUM, 2021-08-02 - 2021-08-06, Virtual Event. doi: 10.2514/6.2021-2286. ISBN 978-162410610-1.
PDF
1MB |
Offizielle URL: https://doi.org/10.2514/6.2021-2286
Kurzfassung
Quantitative measurements of sound due to swirl-nozzle interaction are presented for the first time. In the experiment a swirl structure was generated by means of tangential injection into a steady swirl-free flow upstream from a choked convergent-divergent nozzle. Ingestion of swirl by the choked nozzle caused a mass-flow rate change, which resulted in a downstream measured acoustic response. The amplitude of this acoustic response was found to be proportional to the square of the tangential mass-flow rate used to generate swirl. This was, assuming that the upstream generated swirl intensity is proportional to the tangential injection mass-flow rate, predicted by a previously published quasi-steady model for the swirl-nozzle interaction sound source (Hirschberg, L., Hulshoff, S. J., and Bake, F., “Sound Production due to SwirlNozzle Interaction: Model-Based Analysis of Experiments,” AIAA Journal, Published online on Nov. 11th 2020, doi: 10.2514/1.J059669.). The tangential-injection time was varied, and found to not influence the amplitude of the acoustic response. This indicates that quasi-steady modelling remains applicable, even for smallest achievable upstream swirl structure with an axial length of ca. three upstream diameters.
elib-URL des Eintrags: | https://elib.dlr.de/143475/ | ||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
Titel: | Swirl-Nozzle Interaction Experiments: Influence of Injection-Reservoir Pressure and Injection Time | ||||||||||||||||||||
Autoren: |
| ||||||||||||||||||||
Datum: | August 2021 | ||||||||||||||||||||
Erschienen in: | AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021 | ||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
DOI: | 10.2514/6.2021-2286 | ||||||||||||||||||||
ISBN: | 978-162410610-1 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | Core Noise, Combustion Noise, Vortex Noise, Swirl-Nozzle-Interaction, Indirect Combustion Noise | ||||||||||||||||||||
Veranstaltungstitel: | 27th AIAA/CEAS Aeroacoustics Conference / AIAA AVIATION 2021 FORUM | ||||||||||||||||||||
Veranstaltungsort: | Virtual Event | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsbeginn: | 2 August 2021 | ||||||||||||||||||||
Veranstaltungsende: | 6 August 2021 | ||||||||||||||||||||
Veranstalter : | AIAA / CEAS | ||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||
HGF - Programmthema: | Umweltschonender Antrieb | ||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
DLR - Forschungsgebiet: | L CP - Umweltschonender Antrieb | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Komponenten und Emissionen | ||||||||||||||||||||
Standort: | Berlin-Charlottenburg | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Antriebstechnik > Triebwerksakustik | ||||||||||||||||||||
Hinterlegt von: | Bake, Dr.-Ing. Friedrich | ||||||||||||||||||||
Hinterlegt am: | 19 Aug 2021 07:51 | ||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:43 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags