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An Overview of Virtual Acoustic Simulation of Aircraft Flyover NoiseMethods for testing human subject response to aircraft flyover noise have greatly advanced in recent years as a result of advances in simulation technology. Capabilities have been developed which now allow subjects to be immersed both visually and aurally in a three-dimensional, virtual environment. While suitable for displaying recorded aircraft noise, the true potential is found when synthesizing aircraft flyover noise because it allows the flexibility and freedom to study sounds from aircraft not yet flown. A virtual acoustic simulation method is described which is built upon prediction-based source noise synthesis, engineering-based propagation modeling, and empirically-based receiver modeling. This source-path-receiver paradigm allows complete control over all aspects of flyover auralization. With this capability, it is now possible to assess human response to flyover noise by systematically evaluating source noise reductions within the context of a system level simulation. Examples of auralized flyover noise and movie clips representative of an immersive aircraft flyover environment are made in the presentation.
Document ID
20140000602
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Rizzi, Stephen A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 7, 2014
Publication Date
July 1, 2013
Subject Category
Acoustics
Report/Patent Number
NF1676L-16815
Report Number: NF1676L-16815
Meeting Information
Meeting: International Conference on Recent Advances in Structural Dynamics
Location: Pisa
Country: Italy
Start Date: July 1, 2013
End Date: July 3, 2013
Sponsors: Institute of Sound and Vibration Research
Funding Number(s)
WBS: WBS 794072.02.07.04.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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