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Acoustic and Psychoacoustic Characterisation of Small-Scale Contra-Rotating Propellers

Casagrande Hirono, Fabio; Robertson, James; Torija Martinez, Antonio J

Acoustic and Psychoacoustic Characterisation of Small-Scale Contra-Rotating Propellers Thumbnail


Authors

Fabio Casagrande Hirono

James Robertson



Abstract

This paper reports an experimental investigation of noise radiation and psychoacoustic evaluation of contra-rotating propellers with different blade counts over multiple emission angles and thrust settings. A series of aeroacoustic and psychoacoustic tests were performed with a contra-rotating propeller rig at the University of Salford, UK, where both propellers' blade count and their axial separation z were varied at static conditions and constant thrust. The sounds were analysed using conventional acoustic metrics, such as Sound Pressure Level (SPL) and Sound Power Level for tonal, broadband, and overall noise, and using the psychoacoustic Sound Quality Metrics (SQMs) Loudness, Fluctuation Strength, Roughness, Tonality, and Impulsiveness. Configurations with axial separation-to-diameter ratio z/D between 0.2-0.4 exhibited a balance between tonal and broadband noise generation mechanisms, resulting in reduced noise levels and reduced annoyance for on-axis observers. The number of blades played a secondary role on determining noise levels: higher blade counts resulted in lower overall noise levels at larger axial separations, although at shorter distances (z/D < 0.2) increasing the blade count led to higher noise levels. The SQMs Loudness, Fluctuation Strength, and Tonality were found to also reach a minimum at z/D = 0.3, although increasing the number of propeller blades led to a decrease in Loudness but not in Fluctuation Strength and Tonality. The dominant noise generation mechanisms observed here present a directivity null perpendicular to the propellers' axis, and no clear trends were observed for acoustic and psychoacoustic metrics at this emission angle. A listening experiment was set up to validate the results of the acoustic and psychoacoustic analysis, and its results suggest that the reported noise annoyance is driven by Loudness, Fluctuation Strength and Tonality metrics (p < 0.01) at on-axis radiation, while at 90 • emission angle, Loudness (p < 0.01) and Tonality (p < 0.05) are the main contributors to noise annoyance.

Citation

Casagrande Hirono, F., Robertson, J., & Torija Martinez, A. J. (2023). Acoustic and Psychoacoustic Characterisation of Small-Scale Contra-Rotating Propellers. Journal of Sound and Vibration, 569, https://doi.org/10.1016/j.jsv.2023.117971

Journal Article Type Article
Acceptance Date Jul 30, 2023
Online Publication Date Aug 11, 2023
Publication Date Aug 11, 2023
Deposit Date Jul 31, 2023
Publicly Available Date Aug 12, 2025
Journal Journal of Sound and Vibration
Print ISSN 0022-460X
Publisher Elsevier
Peer Reviewed Peer Reviewed
Volume 569
DOI https://doi.org/10.1016/j.jsv.2023.117971
Keywords Psychoacoustics; Contra-rotating propellers; Noise Annoyance; Experimental Aeroacoustics * Corresponding author

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