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A Recording-Based Method for Auralization of Rotorcraft 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 focused on auralization of rotorcraft fly-in noise, in which a simplification was made that enabled the source noise synthesis to be based on a single emission angle. Here, the goal is to auralize a complete flyover event, so the source noise synthesis must be capable of traversing a range of emission angles. The synthesis uses a source noise definition process that yields periodic and aperiodic (modulation) components at a set of discrete emission angles. In this work, only the periodic components are used for the source noise synthesis for the flyover; the inclusion of modulation components is the subject of ongoing research. Propagation of the synthesized source noise to a ground observer is performed using the NASA Auralization Framework. The method is demonstrated using ground recordings from a flight test of the AS350 helicopter for the source noise definition.
Document ID
20180002090
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Pera, Nicholas M.
(Virginia Tech Blacksburg, VA, United States)
Rizzi, Stephen A.
(NASA Langley Research Center Hampton, VA, United States)
Krishnamurthy, Siddhartha
(NASA Langley Research Center Hampton, VA, United States)
Fuller, Christopher R.
(Virginia Tech Blacksburg, VA, United States)
Christian, Andrew
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
March 23, 2018
Publication Date
January 8, 2018
Subject Category
Acoustics
Report/Patent Number
NF1676L-25385
Report Number: NF1676L-25385
Meeting Information
Meeting: AIAA SciTech 2018
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 664817.02.07.03.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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