Helicopter Main Rotor Speed Effects A Comparison Of Predicted Ranges Of Detection From The Aural Detection Program Ichin And The Electronic Detection Program Arcas PDF Download

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Helicopter Main-Rotor Speed Effects

Helicopter Main-Rotor Speed Effects
Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
Total Pages: 32
Release: 2018-12-31
Genre:
ISBN: 9781792751509

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NASA 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. Mueller, Arnold W. and Smith, Charles D. Langley Research Center NASA-TM-104134, NAS 1.15:104134 RTOP 532-06-36-02...


Government Reports Annual Index

Government Reports Annual Index
Author:
Publisher:
Total Pages: 1228
Release: 1992
Genre: Government reports announcements & index
ISBN:

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Aeronautical Engineering

Aeronautical Engineering
Author:
Publisher:
Total Pages: 712
Release: 1993
Genre: Aeronautics
ISBN:

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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)