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Auralization of Amplitude Modulated Helicopter Flyover NoiseRotorcraft noise is an active field of study as the sound produced by these vehicles is often found to be annoying. A means to auralize rotorcraft flyover noise is sought to help understand the factors leading to annoyance. Previous work by the authors auralized a complete flyover event in which the source noise synthesis traversed a range of emission angles. The source noise definition process for the synthesis used helicopter flyover recordings. Although this process yielded both periodic and aperiodic (modulation) components at a set of discrete emission angles, only the periodic components were used in the previous work to synthesize the sound of the flyover event. In the current work, aperiodic amplitude modulation is incorporated into the source noise synthesis to improve its fidelity toward assessing rotorcraft noise annoyance. The method is demonstrated using ground recordings from a flight test of the AS350 helicopter for the source noise definition.



Document ID
20200002058
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Krishnamurthy, Siddhartha
(NASA Langley Research Center Hampton, VA, United States)
Rizzi, Stephen A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
March 30, 2020
Publication Date
January 7, 2019
Subject Category
Air Transportation And Safety
Acoustics
Report/Patent Number
NF1676L-30378
Report Number: NF1676L-30378
Meeting Information
Meeting: 2019 AIAA SciTech Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 664817.02.07.03.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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