Tip vortex formation noise produced by wall-mounted finite airfoils with porous and sinusoidal tip geometries

Access & Terms of Use
open access
Copyright: Copyright 2019, University of New South Wales
The data collection consists of measurements of tip vortex formation noise produced by a finite length airfoil with porous and sinusoidal tip geometries. These data were obtained using the specialist aeroacoustic test facilities at the Brandenburg University of Technology in Cottbus, Germany. Over 2600 unique test cases with variations in airfoil 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.
Link to External Data Repository
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
Resource Type
Airfoil noise
UNSW Faculty
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Related grant(s)
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