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Aircraft noise synthesis system: Version 4 user instructionsA modified version of the Aircraft Noise Synthesis System with improved directivity and tonal content modeling has been developed. The synthesis system is used to provide test stimuli for studies of community annoyance to aircraft flyover noise. The computer-based system generates realistic, time-varying audio simulations of aircraft flyover noise at a specified observer location on the ground. The synthesis takes into account the time-varying aircraft position relative to the observer; specified reference spectra consisting of broadband, narrowband, and pure tone components; directivity patterns; Doppler shift; atmospheric effects; and ground effects. These parameters can be specified and controlled in such a way as to generate stimuli in which certain noise characteristics such as duration or tonal content are independently varied while the remaining characteristics such as broadband content are held constant. The modified version of the system provides improved modeling of noise directivity patterns and an increased number of pure tone components. User instructions for the modified version of the synthesis system are provided.
Document ID
19870011364
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mccurdy, David A.
(NASA Langley Research Center Hampton, VA, United States)
Sullivan, Brenda M.
(Bionetics Corp. Hampton, Va., United States)
Grandle, Robert E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Subject Category
Acoustics
Report/Patent Number
NASA-TM-89089
NAS 1.15:89089
Report Number: NASA-TM-89089
Report Number: NAS 1.15:89089
Accession Number
87N20797
Funding Number(s)
PROJECT: RTOP 535-03-11-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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