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Evaluation of free stream acoustic noise in a shock tunnel using focused laser differential interferometry

Ponchio Camillo, Giannino und Wagner, Alexander und Surujhlal, Divek (2024) Evaluation of free stream acoustic noise in a shock tunnel using focused laser differential interferometry. In: International Workshop on Shock Tube Technology 2024. International Workshop on Shock Tube Technology 2024, 2024-09-13, Oxford, United Kingdom.

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Offizielle URL: https://eng.ox.ac.uk/iwstt

Kurzfassung

Free stream disturbances of acoustic nature are known to be amplified in the boundary layer on the test model and cause transition to occur much earlier than in flight, even though the exact governing mechanisms are still not fully understood. In order to enable the best use of experimental observations conducted in conventional shock tubes or shock tunnels and support the interpretation of data obtained in different facilities, it is therefore important to quantify the free stream environment, in terms of inherent acoustic disturbances. In the present work, free stream disturbance measurements in a shock tunnel are presented using the technique of Focused Laser Differential Interferometry (FLDI). The experiments are conducted in the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) under free stream unit Reynolds numbers of approximately 1.5e6, 2.2e6, and 2.4e6 1/m, and total enthalpies of 11.9, 9.8, and 3.5 MJ/kg, respectively. Free stream fluctuations in terms of FLDI phase shift spectra are shown. In this data, the lower and upper frequency bounds of the FLDI instrument are identified. Convection velocities are calculated by cross-correlating the time signals from the streamwise FLDI probes, which are separated by a known distance. Using the obtained convection velocities, the frequency bounds are converted into the smaller and larger detected disturbance wavelengths. RMS values of density and pressure fluctuations are calculated from the post-processed FLDI data within the identified frequency bounds. The RMS of pressure fluctuation are compared with measurements performed in a previous work using pressure transducers in a wedge probe in HEG, for the free stream unit Reynolds number 2.4e6 1/m case. The spectra of the pressure fluctuations for all cases are shown, and the effect of Reynolds number and total enthalpy are analyzed. The ease of implementation of FLDI and its clean view of the disturbance spectrum make it a promising candidate technique for the standardization of free stream disturbance measurements, aiming at improving the interpretation and comparison of boundary layer data across different facilities.

elib-URL des Eintrags:https://elib.dlr.de/204859/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Evaluation of free stream acoustic noise in a shock tunnel using focused laser differential interferometry
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Ponchio Camillo, GianninoGiannino.PonchioCamillo (at) dlr.dehttps://orcid.org/0000-0002-2178-0777NICHT SPEZIFIZIERT
Wagner, AlexanderAlexander.Wagner (at) dlr.dehttps://orcid.org/0000-0002-9700-1522NICHT SPEZIFIZIERT
Surujhlal, DivekDivek.Surujhlal (at) dlr.dehttps://orcid.org/0000-0002-0349-3328NICHT SPEZIFIZIERT
Datum:13 September 2024
Erschienen in:International Workshop on Shock Tube Technology 2024
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Shock tunnel, acoustic disturbances, FLDI, HEG
Veranstaltungstitel:International Workshop on Shock Tube Technology 2024
Veranstaltungsort:Oxford, United Kingdom
Veranstaltungsart:Workshop
Veranstaltungsdatum:13 September 2024
Veranstalter :University of Oxford
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Standort: Göttingen
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge, GO
Hinterlegt von: Ponchio Camillo, Giannino
Hinterlegt am:12 Nov 2024 13:56
Letzte Änderung:09 Jan 2025 15:48

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