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Receiver-Based Auralization of Broadband Aircraft Flyover Noise Using the NASA Auralization FrameworkThe NASA Auralization Framework (NAF) consists of a set of dynamic link libraries (DLLs) to facilitate auralization of aircraft noise. Advanced capabilities for synthesis, propagation, and external interfaces are provided by the NAF Advanced Plugin Libraries (APL); a separate set of DLLs that are made accessible through the NAF’s plugin architecture. In the typical time domain use case, the sound is first synthesized at the source location based on a source noise definition, and is then propagated in the time domain to a receiver on or near the ground. Alternatively, it may be desirable to synthesize the sound at the receiver, after it has been propagated in the frequency domain, e.g., when the source definition is inaccessible or when alternative propagation methods are needed. Receiver-based auralization requires three new developments in the NAF APL: a component plugin to interpolate the propagated noise spectra as a function of time for input to sound synthesis, and a path finder and path traversal plugin to calculate the effects of the differential propagation path length between the direct and ground reflected rays. This paper describes those developments and demonstrates their use in the auralization of broadband flyover noise.
Document ID
20200002559
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Aumann, Aric R.
(Science Applications International Corp. Hampton, VA, United States)
Rizzi, Stephen A.
(NASA Langley Research Center Hampton, VA, United States)
Heath, Stephanie L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 17, 2020
Publication Date
August 26, 2018
Subject Category
Acoustics
Report/Patent Number
NF1676L-29493
Meeting Information
Meeting: International Congress and Exposition on Noise Control Engineering
Location: Chicago, IL
Country: United States
Start Date: August 26, 2018
End Date: August 29, 2018
Sponsors: Institute of Noise Control Engineering
Funding Number(s)
WBS: 109492.02.07.01.10
Distribution Limits
Public
Copyright
Public Use Permitted.
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