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Helicopter main-rotor speed effects: A comparison of predicted ranges of detection from the aural detection program ICHIN and the electronic detection program ARCASNASA LaRC personnel have conducted a strudy of the predicted acoustic detection ranges associated with reduced helicopter main rotor speeds. This was accomplished by providing identical input information to both the aural detection program ICHIN 6, (I Can Hear It Now, version 6) and the electronic acoustic detection program ARCAS (Assessment of Rotorcraft Detection by Acoustics Sensing). In this study, it was concluded that reducing the main rotor speed of the helicopter by 27 percent reduced both the predicted aural and electronic detection ranges by approximately 50 percent. Additionally, ARCAS was observed to function better with narrowband spectral input than with one-third octave band spectral inputs and the predicted electronic range of acoustic detection is greater than the predicted aural detection range.
Document ID
19920003380
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mueller, Arnold W.
(NASA Langley Research Center Hampton, VA, United States)
Smith, Charles D.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Acoustics
Report/Patent Number
NASA-TM-104134
NAS 1.15:104134
Report Number: NASA-TM-104134
Report Number: NAS 1.15:104134
Accession Number
92N12598
Funding Number(s)
PROJECT: RTOP 532-06-36-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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