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Brief Communication: measurement of boundary layer turbulent transition using an acoustic microphone unit

dc.contributor.authorLawson, Nicholas J.
dc.contributor.authorZachos, Pavlos K.
dc.date.accessioned2025-08-22T16:04:20Z
dc.date.available2025-08-22T16:04:20Z
dc.date.freetoread2025-08-22
dc.date.issued2025-07-16
dc.date.pubOnline2025-07-16
dc.description.abstractIn this article the transition of a laminar boundary layer (BL) over a flat plate is characterized using an acoustic technique with a pitot probe linked to a microphone unit. The probe was traversed along a BL plate at a fixed wind tunnel flow velocity of 5.5 m/s. A spectral analysis of the acoustic fluctuations showed that this setup can estimate the streamwise location and length of the BL transition region, as well as the BL thickness, by using the intermittency similitude approach. Further work is required to quantify the uncertainty caused by signal attenuation within the data acquisition system.
dc.description.journalNameSAE International Journal of Aerospace
dc.format.extentpp. 167-173
dc.identifier.citationLawson NJ, Zachos PK. (2025) Brief Communication: measurement of boundary layer turbulent transition using an acoustic microphone unit. SAE International Journal of Aerospace, Volume 18, Issue 2, pp. 167-173. SAE 01-18-02-0011en_UK
dc.identifier.eissn1946-3901
dc.identifier.elementsID736618
dc.identifier.issn1946-3855
dc.identifier.issueNo2
dc.identifier.paperNoSAE 01-18-02-0011
dc.identifier.urihttps://doi.org/10.4271/01-18-02-0011
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/24316
dc.identifier.volumeNo18
dc.languageEnglish
dc.language.isoen
dc.publisherSociety of Automotive Engineers (SAE)en_UK
dc.publisher.urihttps://saemobilus.sae.org/articles/brief-communication-measurement-boundary-layer-turbulent-transition-using-acoustic-microphone-unit-01-18-02-0011
dc.rightsAttribution 4.0 Internationalen
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectBoundary layeren_UK
dc.subjectFlowen_UK
dc.subjectmeasurementen_UK
dc.subjectAerodynamicsen_UK
dc.subject4012 Fluid Mechanics and Thermal Engineeringen_UK
dc.subject40 Engineeringen_UK
dc.subject4001 Aerospace engineeringen_UK
dc.titleBrief Communication: measurement of boundary layer turbulent transition using an acoustic microphone uniten_UK
dc.typeArticle
dc.type.subtypeJournal Article
dcterms.dateAccepted2025-06-14

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