Brief Communication: measurement of boundary layer turbulent transition using an acoustic microphone unit
| dc.contributor.author | Lawson, Nicholas J. | |
| dc.contributor.author | Zachos, Pavlos K. | |
| dc.date.accessioned | 2025-08-22T16:04:20Z | |
| dc.date.available | 2025-08-22T16:04:20Z | |
| dc.date.freetoread | 2025-08-22 | |
| dc.date.issued | 2025-07-16 | |
| dc.date.pubOnline | 2025-07-16 | |
| dc.description.abstract | In 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.journalName | SAE International Journal of Aerospace | |
| dc.format.extent | pp. 167-173 | |
| dc.identifier.citation | Lawson 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 01-18-02-0011 | en_UK |
| dc.identifier.eissn | 1946-3901 | |
| dc.identifier.elementsID | 736618 | |
| dc.identifier.issn | 1946-3855 | |
| dc.identifier.issueNo | 2 | |
| dc.identifier.paperNo | SAE 01-18-02-0011 | |
| dc.identifier.uri | https://doi.org/10.4271/01-18-02-0011 | |
| dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/24316 | |
| dc.identifier.volumeNo | 18 | |
| dc.language | English | |
| dc.language.iso | en | |
| dc.publisher | Society of Automotive Engineers (SAE) | en_UK |
| dc.publisher.uri | https://saemobilus.sae.org/articles/brief-communication-measurement-boundary-layer-turbulent-transition-using-acoustic-microphone-unit-01-18-02-0011 | |
| dc.rights | Attribution 4.0 International | en |
| dc.rights.uri | http://creativecommons.org/licenses/by/4.0/ | |
| dc.subject | Boundary layer | en_UK |
| dc.subject | Flow | en_UK |
| dc.subject | measurement | en_UK |
| dc.subject | Aerodynamics | en_UK |
| dc.subject | 4012 Fluid Mechanics and Thermal Engineering | en_UK |
| dc.subject | 40 Engineering | en_UK |
| dc.subject | 4001 Aerospace engineering | en_UK |
| dc.title | Brief Communication: measurement of boundary layer turbulent transition using an acoustic microphone unit | en_UK |
| dc.type | Article | |
| dc.type.subtype | Journal Article | |
| dcterms.dateAccepted | 2025-06-14 |
