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Updates to PCBoom Sonic Boom Propagation Code: Modeling QSF18 Sonic ThumpsNASA PCBoom sonic boom propagation code has recently been updated to improve the code's numerical accuracy and efficiency. This paper specifically discusses algorithms for calculating the ray tube area, accounting for turbulence effects, and determining the entire sonic boom carpet. Unlike most existing sonic boom propagation codes that require three or four neighboring acoustic rays for the ray tube area calculation, the updated PCBoom requires only one ray to perform the same calculation. In addition, the turbulence algorithm employed here is based on a multiple-scattering theory rather than based on a oneway parabolic equation used by existing algorithms. Numerical models obtained using the updated PCBoom are compared with a measured dataset from the Quiet Supersonic Flights 2018 research campaign (QSF18) that NASA conducted in Texas in 2018. The dataset was obtained using dive maneuvers performed by supersonic conventional aircraft that generated small-amplitude sonic booms, called sonic thumps, mostly with small elevation angles of arrival. In such sonic booms, the effects due to turbulence and spreading from refraction are significantly large, making the dataset suitable for assessing the code's performance to
accurately predict such effects.
Document ID
20200003630
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Joel Barce Lonzaga
(Langley Research Center Hampton, United States)
Date Acquired
May 8, 2020
Subject Category
Aeronautics (General)
Report/Patent Number
NF1676L-33629
Meeting Information
Meeting: 178th Meeting of the Acoustical Society of America
Location: San Diego, CA
Country: US
Start Date: December 2, 2019
End Date: December 6, 2019
Sponsors: Langley Research Center
Funding Number(s)
WBS: D321 110076.02.07.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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