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May 14, 2026The Journal of the Acoustical Society of America0 citations

A hybrid analysis of Mach cutoff noise using nonlinear acoustics and finite-difference time-domain method—Comparison with NASA's flight test FaInt–

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TTTakao TsuchiyaMKMasashi Kanamori

Key Points

  • This research aims to develop a hybrid method for analyzing Mach cutoff noise by treating boom signatures and atmospheric turbulence separately.
  • Utilized a 2-D hybrid analysis combining the augmented Burgers equation and nonlinear Tricomi equation for boom signature analysis.
  • Applied a compact-explicit finite-difference time-domain method for the propagation analysis of atmospheric disturbances.
  • Conducted numerical experiments replicating conditions of NASA's flight test FaInt.
  • Observed that the Perceived Level on the ground matched flight test results when corrections from 2-D to 3-D were accurately applied.

Abstract

This paper proposes a 2-D, hybrid analysis method of so-called Mach cutoff noise, which treats boom signature and its disturbance due to collision of the signature with atmospheric turbulence separately. A combination of the augmented Burgers equation analysis and the nonlinear Tricomi equation analysis are applied to the former, while the conventional compact-explicit finite-difference time-domain method is applied to the propagation analysis to the latter. Several numerical experiments using this hybrid method under the same conditions as NASA's flight test FaInt showed that the Perceived Level on the ground is equivalent to the flight test results when the correction from 2-D results to 3-D results is properly made.

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Cite This Study

Tsuchiya et al. (2025) studied this question.

synapsesocial.com/papers/6a0567bca550a87e60a1ff58https://doi.org/10.1121/10.0040534
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