Related Experiment Video
Updated: Jun 17, 2025

Visually Based Characterization of the Incipient Particle Motion in Regular Substrates: From Laminar to Turbulent Conditions
Published on: February 22, 2018
Acoustic response of structured and randomized porous blunt trailing edges subject to turbulent boundary layers
Elias J G Arcondoulis1, Daniele Ragni2, Daniele Fiscaletti3
1School of Civil Aerospace and Design Engineering, University Walk, Bristol BS8 1TR, United Kingdom.
Abstract:
The attachment of porous media to a blunt trailing edge (TE) can significantly suppress vortex shedding processes and the related tonal noise, yet the near-wall and internal flow fields of porous media are difficult to analyze experimentally and rely on numerical simulations to elucidate the internal flow features. A structured porous trailing edge (SPTE) has been recently designed that follows a methodology of a structured porous coated cylinder. The SPTE acoustic response was compared against randomized porous media with 10 and 30 pores/in. in an anechoic wind tunnel over a range of flow velocities. Acoustic beamforming revealed that the dominant acoustic sources were at the end of the solid plate, even when a porous TE was attached. A region of integration was used to extract acoustic spectra without additional noise sources, revealing that the SPTE possesses superior noise reduction capability. Dipolar directivity patterns were observed at the vortex shedding frequency for each TE, and the coherence between microphones revealed the complex acoustic propagation of the high-frequency content. A wavelet analysis revealed how the SPTE breaks periodic vortex shedding cycles into smaller cycles over a wider frequency range, leading to an overall noise reduction relative to the other TEs.
Related Concept Videos
Boundary Layer Characteristics
Turbulent Flow
Steady, Laminar Flow Between Parallel Plates
Laminar and Turbulent Flow
General Characteristics of Pipe Flow II
The distance to reach a fully developed flow is called the entrance length and depends on the...
Free Jet

