Tip vortex formation noise produced by wall-mounted finite airfoils with flat and rounded tip geometries

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Copyright: Copyright 2019, University of New South Wales
Abstract
The data collection consists of measurements of tip vortex formation noise produced by a finite length airfoil with flat and rounded tip shape. These data were obtained using the specialist aeroacoustic test facilities at the Brandenburg University of Technology in Cottbus, Germany. Over 1200 unique test cases with variations in airfoil profile shape, tip geometry, angle of attack and Reynolds number were measured during the experimental campaign. The dataset contains raw microphone array data and data processed using Acoular, a Python module that produces acoustic maps of sound source distributions and one-third octave band tip noise spectra.
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Electronic Location
Contact Information
Please contact Danielle Moreau (d.moreau@unsw.edu.au) for access to the dataset.
Research Data Creator(s)
Lead Chief Investigator
Other Contributor(s)
Corporate/Industry Contributor(s)
Publication Year
2019
Resource Type
Dataset
Keyword(s)
Aeroacoustics
Noise
Beamforming
Airfoil noise
UNSW Faculty
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Related publication(s)
Related grant(s)
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