Geyer, Thomas und Abromeit, Paul und Prügel, Maximilian und Enghardt, Lars (2025) Experimental Investigation of the Tonal Noise Generation From Tandem Cylinders with Different Diameter. In: AIAA Aviation Forum and ASCEND, 2025. AIAA AVIATION FORUM AND ASCEND 2025, 2025-07-21 - 2025-07-25, Las Vegas, Nevada. doi: 10.2514/6.2025-3212. ISBN 978-162410738-2.
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Offizielle URL: https://dx.doi.org/10.2514/6.2025-3212
Kurzfassung
Aerodynamic noise generated by various technical applications, such as parts of the landing gear of aircraft or protective grilles for axial fans, can be investigated in a simplified manner by using two circular cylinders in a tandem configuration. Although a variety of experimental and numerical studies exists on such configurations, the effects of unequal cylinder diameters on the resulting far-field noise generation are not fully understood, especially for varying distances between the cylinders. With the aim of providing a substantial experimental data set and to allow for preliminary investigations of possible scaling approaches, a detailed wind tunnel study was performed on a set of two-dimensional circular cylinders with diameters from 6~mm to 40~mm in a tandem arrangement. Different normalized distances were investigated, using a nominal diameter of 30~mm as a reference. Acoustic measurements were performed using a set of free-field microphones located in the acoustic far field. The results indicate that for configurations with a thicker upstream cylinder, the vortex shedding and the subsequent generation of tonal noise are governed by the flow around the upstream cylinder. For configurations with a thicker downstream cylinder and small normalized spacing, the vortex shedding scales with the diameter of the downstream cylinder.
| elib-URL des Eintrags: | https://elib.dlr.de/216446/ | ||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
| Titel: | Experimental Investigation of the Tonal Noise Generation From Tandem Cylinders with Different Diameter | ||||||||||||||||||||
| Autoren: |
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| Datum: | 2025 | ||||||||||||||||||||
| Erschienen in: | AIAA Aviation Forum and ASCEND, 2025 | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| DOI: | 10.2514/6.2025-3212 | ||||||||||||||||||||
| ISBN: | 978-162410738-2 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Airframe/High-Lift Noise and Computational Aeroacoustics | ||||||||||||||||||||
| Veranstaltungstitel: | AIAA AVIATION FORUM AND ASCEND 2025 | ||||||||||||||||||||
| Veranstaltungsort: | Las Vegas, Nevada | ||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
| Veranstaltungsbeginn: | 21 Juli 2025 | ||||||||||||||||||||
| Veranstaltungsende: | 25 Juli 2025 | ||||||||||||||||||||
| 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: | Cottbus | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Elektrifizierte Luftfahrtantriebe > Umweltwirkungen und Sensorik | ||||||||||||||||||||
| Hinterlegt von: | Mewes, Carolin | ||||||||||||||||||||
| Hinterlegt am: | 15 Sep 2025 09:56 | ||||||||||||||||||||
| Letzte Änderung: | 29 Okt 2025 13:07 |
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