Temporal integration of partial loudness of helicopter-like sounds
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Authors
Schlittenlacher, J
Moore, BCJ
Publication Date
2021-08-01Journal Title
Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering
Conference Name
Inter-Noise 2021
ISSN
0736-2935
ISBN
9781732598652
Publisher
Institute of Noise Control Engineering (INCE)
Type
Conference Object
This Version
AM
Metadata
Show full item recordCitation
Schlittenlacher, J., & Moore, B. (2021). Temporal integration of partial loudness of helicopter-like sounds. Proceedings of INTER-NOISE 2021 - 2021 International Congress and Exposition of Noise Control Engineering https://doi.org/10.3397/IN-2021-2830
Abstract
<jats:p>When developing new vehicles that are to be operated in existing background noise, such as electric vertical take-off and landing aircraft (eVTOLs) in cities, a sound design goal should be to minimize the loudness in the given background noise. Rotorcraft sounds are characterised by their pulses, and the choice of rotor size and number allows to vary the temporal characteristics. We asked participants to compare the loudness of pulse trains with pulse durations of 1, 2, 5, 10 and 20 ms and a pulse rate of 20 Hz in a two-interval, two-alternatives forced choice task and a 1-up/1-down procedure. Street noise was presented simultaneously with the pulse trains, and had the same root-mean-square (RMS) level as the fixed reference pulse train of about 65 dB SPL. First results indicate that the sounds with a short pulse duration need considerably less RMS level to result in the same loudness as a long pulse duration, i.e. the partial loudness of shorter pulses is higher at the same equivalent sound pressure level.</jats:p>
Relationships
Is supplemented by: https://doi.org/10.3397/IN-2021-2830
Sponsorship
EPSRC
Funder references
Engineering and Physical Sciences Research Council (EP/M026957/1)
Identifiers
External DOI: https://doi.org/10.3397/IN-2021-2830
This record's URL: https://www.repository.cam.ac.uk/handle/1810/330479
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