Print Email Facebook Twitter Boundary layer characterization and acoustic measurements of flow-aligned trailing edge serrations Title Boundary layer characterization and acoustic measurements of flow-aligned trailing edge serrations Author Arce Leon, C.A. (TU Delft Aerodynamics; Aerodynamics and Acoustics Group) Merino Martinez, R. (TU Delft Aircraft Noise and Climate Effects) Ragni, D. (TU Delft Wind Energy) Avallone, F. (TU Delft Wind Energy) Snellen, M. (TU Delft Aircraft Noise and Climate Effects) Date 2016 Abstract Trailing edge serrations designed to reduce airfoil self-noise are retrofitted on a NACA 0018 airfoil. An investigation of the boundary layer flow statistical properties is performed using time-resolved stereoscopic PIV. Three streamwise locations over the edge of the serrations are compared. An analysis of the results indicates that, while there is no upstream effect, the flow experiences significant changes as it convects over the serrations and toward its edges. Among the most important, a reduced shear stress and modifications of the turbulence spectra suggest beneficial changes in the unsteady surface pressure that would result in a reduction of trailing edge noise. Microphone array measurements are additionally performed to confirm that noise reduction is indeed observed by the application of the chosen serration design over the unmodified airfoil. To reference this document use: http://resolver.tudelft.nl/uuid:f7d252ac-1044-49ca-a904-91e8d0c799e8 DOI https://doi.org/10.1007/s00348-016-2272-z ISSN 0723-4864 Source Experiments in Fluids: experimental methods and their applications to fluid flow, 57 (182) Part of collection Institutional Repository Document type journal article Rights © 2016 C.A. Arce Leon, R. Merino Martinez, D. Ragni, F. Avallone, M. Snellen Files PDF 10.1007_s00348_016_2272_z.pdf 5.25 MB Close viewer /islandora/object/uuid:f7d252ac-1044-49ca-a904-91e8d0c799e8/datastream/OBJ/view