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Simulated X-59 on- and off-Design Sonic Boom Levels in Realistic Atmospheres for Noise Dose Range EstimationNASA is planning several community noise surveys across the USA using the X-59 low-boom aircraft. These surveys require a range of noise levels to resolve a dose-response relationship. The X-59 was designed to produce a shaped sonic boom with a Stevens’ Perceived Level (PL) of 75 dB or less across the boom carpet in a standard atmosphere. However, the X-59’s flight condition can be adjusted to produce levels other than 75 PLdB to obtain a range of doses during community testing. Simulated nearfield pressure waveforms of the X-59 C612A in its on-design condition (Mach 1.4 at 53,200 ft) and an off-design condition at a lower altitude (Mach 1.4 at 46,000 ft) were propagated using PCBoom through realistic atmospheres over the span of one year at several locations across the country. The predicted on-design and off-design boom levels and carpet widths are presented, resulting in a preliminary estimate of the dose range that the X-59 may produce. Future work is planned with additional off-design conditions to assess the true capable dose range of the X-59.
Document ID
20210013118
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
William Doebler
(Langley Research Center Hampton, Virginia, United States)
Alexandra Loubeau
(Langley Research Center Hampton, Virginia, United States)
Joel Lonzaga
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
April 2, 2021
Subject Category
Acoustics
Meeting Information
Meeting: Acoustics in Focus - 180th Meeting of the Acoustical Society of America
Location: Online
Country: US
Start Date: June 7, 2021
End Date: June 11, 2021
Sponsors: Acoustical Society of America
Funding Number(s)
WBS: 110076.02.07.06.13
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
Keywords
X-59
low-boom
PCBoom
noise exposure
dose-response
sound propagation
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