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The Aeroacoustic Effect of Different Inter-Spaced Self-oscillating Passive Trailing Edge Flaplets

Talboys, E. ORCID: 0000-0001-8993-0180, Geyer, T. F., Prüfer, F. and Brücker, C. ORCID: 0000-0001-5834-3020 (2021). The Aeroacoustic Effect of Different Inter-Spaced Self-oscillating Passive Trailing Edge Flaplets. In: Braza, M., Hoarau, Y., Zhou, Y., Lucey, A. D., Huang, L. and Stavroulakis, G. E. (Eds.), Fluid-Structure-Sound Interactions and Control. FSSIC 2019. Lecture Notes in Mechanical Engineering. (pp. 161-166). Singapore: Springer. ISBN 9789813349599


An aeroacoustic investigating looking into the effect of changing the inter-spacing of passive self-oscillating trailing edge flaplets has been carried out using a NACA 0012 aerofoil. Clear differences can be observed between each of the different cases. Where a reduction in low frequency noise, an increase in high frequency noise and a reduction in turbulence intensity in the wake can be seen for each case. As the inter-spacing is reduced, the differences become more prominent, when compared to the reference aerofoil.

Publication Type: Book Section
Publisher Keywords: Passive oscillators, aeroacoustics, trailing edge flaplets, fluid structure interaction
Subjects: T Technology > TJ Mechanical engineering and machinery
T Technology > TL Motor vehicles. Aeronautics. Astronautics
Departments: School of Mathematics, Computer Science & Engineering > Engineering > Mechanical Engineering & Aeronautics
Date available in CRO: 18 Jun 2021 07:44
Date deposited: 18 June 2021
Date of first online publication: 6 May 2021
[img] Text - Accepted Version
This document is not freely accessible until 6 May 2022 due to copyright restrictions.

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