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Investigation of Speed and Altitude Effects on Sound Exposure Level Calculations for Multiple HelicoptersInternational and United States Federal regulations evaluate helicopter acoustic emissions for certification purposes as well as community noise impact assessments. The Sound Exposure Level (SEL) is a commonly used metric that represents the loudness of a single event, with a penalty for duration. For example, a flyover lasting ten seconds can have the same SEL as a five-second duration flyover that is 3 dB higher in peak level. Ten helicopters spanning the light and medium weight classes were modeled using flight test data. They were then virtually flown using the Advanced Acoustic Model at multiple speeds and altitudes. SEL and A-weighted SEL (SELA) were calculated at ground-based observer locations for each condition. Scaling laws with altitude are determined, and cruising airspeeds which result in the minimum SEL are found. Implications for future land-use planning will be discussed, and the relationships are reduced to general or vehicle-specific operational guidance for pilots.
Document ID
20240005628
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Mary Houston
(Langley Research Center Hampton, United States)
Kyle Pascioni
(Langley Research Center Hampton, United States)
James Stephenson
(United States Department of the Army Arlington, United States)
Date Acquired
May 3, 2024
Subject Category
Acoustics
Meeting Information
Meeting: 186th Meeting of the Acoustical Society of America
Location: Ottawa, ON
Country: CA
Start Date: May 13, 2024
End Date: May 17, 2024
Sponsors: Acoustical Society of America
Funding Number(s)
WBS: 664817.02.07.03.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
community noise
rotorcraft noise
helicopter noise
rotorcraft acoustics
flight testing
helicopter acoustics
flight test
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