Correction: Psychoacoustic Characterization of Multirotor Drones in Realistic Flyover Maneuvers

Conference Paper (2024)
Author(s)

R.M. Yupa Villanueva (TU Delft - Aircraft Noise and Climate Effects)

R. Merino Martinez (TU Delft - Aircraft Noise and Climate Effects)

A. Altena (TU Delft - Aircraft Noise and Climate Effects)

M. Snellen (TU Delft - Control & Operations)

Research Group
Aircraft Noise and Climate Effects
DOI related publication
https://doi.org/10.2514/6.2024-3015.c1 Final published version
More Info
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Publication Year
2024
Language
English
Related content
Research Group
Aircraft Noise and Climate Effects
Article number
AIAA 2024-3015.c1
ISBN (electronic)
978-1-62410-720-7
Event
30th AIAA/CEAS Aeroacoustics Conference (2024) (2024-06-04 - 2024-06-07), Rome, Italy
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Abstract

Correction Notice • Place s5 in front of the symbols ‘greater than or equal to (≥)’ and ‘less than (<)’ in Equation 2, as shown below. (Formula Presented). • Replace the correlation coefficient ‘0.886’ showed in Table 6 to ‘-0.886’. This correction also apply to the paragraph below Section 3 (Correlation between Annoyance and Drone Characteristics) and in the last paragraph of the Conclusions. This negative value indicates an inverse relationship between the installation ratio (d/D) and the annoyance computed using the More PA model. • Replace ‘0.337 (Zwicker PA model)’ by ‘0.362 (Willemsen PA model)’ in the paragraph below Section 3 (Correlation between Annoyance and Drone Characteristics). This value (0.362) is also reported in Table 6.

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