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Sonic Boom Analyses in Support of Improved X-59 Community Noise Testinginforming measurement planning and analysis of quiet supersonic aircraft community testing. The report is divided into three main sections: (1) investigations on the impacts of contaminating noise on sonic boom community noise metrics; (2) investigations into sonic boom variability, including turbulence effects on metrics of interest and development of a data-driven boom variability analysis framework; (3) other studies that support developing improved methodologies for community testing and analysis.
Document ID
20240008985
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Kent L Gee
(Brigham Young University Provo, United States)
Mark C Anderson
(Brigham Young University Provo, United States)
Kaylee Nyborg
(Brigham Young University Provo, United States)
J Taggart Durrant
(Brigham Young University Provo, United States)
Jesse D Blaine
(Brigham Young University Provo, United States)
Avery K Sorrell
(Brigham Young University Provo, United States)
Date Acquired
July 16, 2024
Publication Date
November 1, 2024
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Acoustics
Report/Patent Number
NASA/CR-20240008985
Funding Number(s)
CONTRACT_GRANT: 80LARC17C004
WBS: 110076.02.07.06.13
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
community noise
BYU
X-59
sonic boom
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