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A Testbed for large scale and high Reynolds number Airframe Noise Research

Pott-Pollenske, Michael und Delfs, Jan und Reichenberger, Johann (2013) A Testbed for large scale and high Reynolds number Airframe Noise Research. AIAA/CEAS Aeroacoustics Conference, 2013-05-27 - 2013-05-29, Berlin.

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Kurzfassung

Airframe noise testing in open jet wind tunnels is and will be an indispensable means to (i) identify airframe noise sources and develop noise reduction technologies and (ii) to provide validation data in order to support the development of numerical acoustic methods like e.g. CAA codes. Usually such wind tunnel experiments were conducted in small research facilities like DLR's AWB (nozzle size 1.2 m x 0.8 m) using 2-dimensional wind tunnel models featuring a retracted chord length of about 300 to 400 mm. In very rare cases full aircraft models of 1:7.5 to 1:11 scale were tested in the Large Low-Speed Facility of DNW (DNW-LLF), which provides a nozzle size of 8 x 6 m2 and a maximum flow speed of 78 m/s. Even though these full aircraft models provide almost realistic 3-dimensional flow conditions the mean retracted chord length is pretty similar to the 2D test cases. Therefore most airframe noise tests are restricted to a Reynolds number regime between Re=1.0*106 and Re=2.0*106. This finally means that the aerodynamic conditions during most airframe noise wind tunnel experiments do not comply with realistic operating conditions. In order to overcome these deficiencies DLR, Airbus and EADS-IW decided to design a new large scale test bed for airframe noise testing. This plan could be realized in the mainframe of the German national founded research project FTEG (Flight Physics Technologies for Green Aircraft).The finally designed high lift system features a retracted chord length of 1200 mm and a wing span of 7200 mm. It was tested for representative approach conditions and Reynolds numbers up to 5.0*106. By means of this wind tunnel model high Reynolds number slat noise data were acquired that later serve for the validation of the DLR CAA code PIANO. It reveals the slat noise spectra did not contain any relevant tonal slat noise components that are well known from small scale experiments. Dedicated Reynolds number variations gave evidence that (i) low Reynolds number tests on high lift airfoils do not completely represent the broadband sound radiation typical for respective full scale components and that (ii) the tonal components are related to more than one generation mechanism. The new large scale F15LS high lift system successfully proved its ability to enable the assessment of noise reduction technology and the acquisition of validation data for numerical methods under almost realistic flow conditions.

elib-URL des Eintrags:https://elib.dlr.de/84365/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:A Testbed for large scale and high Reynolds number Airframe Noise Research
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Pott-Pollenske, Michaelmichael.pott-pollenske (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Delfs, JanJan.Delfs (at) dlr.dehttps://orcid.org/0000-0001-8893-1747NICHT SPEZIFIZIERT
Reichenberger, Johannjohann.reichenberger (at) eads.netNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:Mai 2013
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Umströmungsgeräusch, Hochauftriebssystem, Windkanal
Veranstaltungstitel:AIAA/CEAS Aeroacoustics Conference
Veranstaltungsort:Berlin
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:27 Mai 2013
Veranstaltungsende:29 Mai 2013
Veranstalter :AIAA / CEAS
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 - Flugphysik (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Technische Akustik
Hinterlegt von: Pott-Pollenske, Stephan-Michael
Hinterlegt am:16 Okt 2013 09:15
Letzte Änderung:24 Apr 2024 19:50

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  • A Testbed for large scale and high Reynolds number Airframe Noise Research. (deposited 16 Okt 2013 09:15) [Gegenwärtig angezeigt]

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