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In-flight acoustic testing techniques using the YO-3A Acoustic Research AircraftThis report discusses the flight testing techniques and equipment employed during air-to-air acoustic testing of helicopters at Ames Research Center. The in flight measurement technique used enables acoustic data to be obtained without the limitations of anechoic chambers or the multitude of variables encountered in ground based flyover testing. The air-to-air testing is made possible by the NASA YO-3A Acoustic Research Aircraft. This "Quiet Aircraft' is an acoustically instrumented version of a quiet observation aircraft manufactured for the military. To date, tests with the following aircraft have been conducted: YO-3A background noise; Hughes 500D; Hughes AH-64; Bell AH-1S; Bell AH-1G. Several system upgrades are being designed and implemented to improve the quality of data. This report will discuss not only the equipment involved and aircraft tested, but also the techniques used in these tests. In particular, formation flying position locations, and the test matrices will be discussed. Examples of data taken will also be presented.
Document ID
19840011266
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cross, J. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Watts, M. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-85895
NAS 1.15:85895
A-9660
Report Number: NASA-TM-85895
Report Number: NAS 1.15:85895
Report Number: A-9660
Accession Number
84N19334
Funding Number(s)
PROJECT: RTOP 532-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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