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Perceived Level of Sonic Boom Noise: Recommended Computation Methods, Rationale, and a Minor ModificationAnalysts face algorithmic choices when writing software to compute the Perceived Level (PL) noise metric. This document contains algorithmic recommendations for computing the PL of a sonic boom waveform. For the four main computational steps, the recommended algorithm and a less accurate alternative are introduced. Rationale for each recommendation is provided by comparing levels returned by the recommended algorithms versus the alternate algorithms while discussing the expected accuracies of each. Algorithm evaluations are performed using as input predicted shaped sonic boom waveforms for the X-59 aircraft and background noise waveforms measured in a community. A minor addition to a data table used to weight the loudness spectrum while summing to total loudness is also described here; that weighting is a precursor to the Perceived Level value. This table addition, which fills a gap at low sound levels, should increase the accuracy of PL values for quiet background noise and evanescent waves in the Mach cutoff shadow region.
Document ID
20250003346
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Jacob Klos
(Langley Research Center Hampton, United States)
Date Acquired
April 3, 2025
Publication Date
April 1, 2025
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Acoustics
Report/Patent Number
NASA/TM-20250003346
Funding Number(s)
WBS: 110076.02.07.06.13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Perceived Level
Sonic Boom
X-59
Recommended Practices
Recommended Methods
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