Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates

Author:

Kershner John R.1ORCID,Jaworski Justin W.2ORCID,Geyer Thomas F.3ORCID

Affiliation:

1. Lehigh University, Bethlehem, PA 18015

2. Virginia Polytechnic Institute and State University, Blacksburg, VA 24061

3. Institute of Electrified Aero Engines, German Aerospace Center (DLR), 03046 Cottbus, Germany

Abstract

The acoustic and aerodynamic fields of blunt porous plates are examined experimentally in an effort to mitigate trailing-edge bluntness noise. The plates are characterized by a single dimensionless porosity parameter identified in previous works that controls the influence of porosity on the sound field. Hot-wire anemometry interrogates the velocity field to connect turbulence details of specific regions to flow noise directivity and beamforming source maps. Porous plates are demonstrated to reduce the bluntness-induced noise by up to 17 dB and progressively suppress broadband low-frequency noise as the value of the porosity parameter increases. However, an increase in this parameter also increases the high-frequency noise created by the pores themselves. The same highly perforated plate characterized by a large value of the porosity parameter reduces the bluntness-induced vortex shedding that is present in the wake of the impermeable plate. Lastly, pore shape and positional alignment are shown to have a complex effect on the acoustic field. Among the porosity designs considered, plates with circular pores are most effective for low-frequency noise reductions but generate high-frequency noise. No meaningful difference is found between the acoustic spectra from plates of the same open-area fraction with pores aligned along or staggered about the flow direction.

Funder

National Science Foundation

German-American Fulbright Commission

The Germanistic Society of America

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

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