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Measured Noise from Small Unmanned Aerial VehiclesProposed uses of small unmanned aerial vehicles (UAVs), including home package delivery, have the potential to expose large portions of communities to a new noise source. This paper discusses results of flyover noise measurements of four small UAVs, including an internal combustion-powered model airplane and three battery-powered multicopters. Basic noise characteristics of these vehicles are discussed, including spectral properties and sound level metrics such as sound pressure level, effective perceived noise level, and sound exposure level. The size and aerodynamic characteristics of the multicopters in particular make their flight path susceptible to atmospheric disturbances such as wind gusts. These gusts, coupled with a flight control system that varies rotor speed to maintain vehicle stability, create an unsteady acoustic signature. The spectral variations resulting from this unsteadiness are explored, in both hover and flyover conditions for the multicopters. The time varying noise, which differs from the relatively steady noise generated by large transport aircraft, may complicate the prediction of human annoyance using conventional sound level metrics.
Document ID
20160010139
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Cabell, Randolph
(NASA Langley Research Center Hampton, VA, United States)
McSwain, Robert
(NASA Langley Research Center Hampton, VA, United States)
Grosveld, Ferdinand
(Northrop Grumman Corp. Hampton, VA, United States)
Date Acquired
August 9, 2016
Publication Date
June 13, 2016
Subject Category
Acoustics
Report/Patent Number
nc16-102
NF1676L-23558
Meeting Information
Meeting: NOISE-CON 2016
Location: Providence, RI
Country: United States
Start Date: June 13, 2016
End Date: June 15, 2016
Sponsors: Institute of Noise Control Engineering
Funding Number(s)
WBS: WBS 533127.02.15.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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