Numerical Method Comparison on Shaped Sonic Boom Propagation Through Atmospheric Boundary Layer Turbulence

Joshua L. Kapcsos, Victor W. Sparrow

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Nonlinear propagation code KZKFourier is used to simulate the propagation of sonic booms through atmospheric boundary layers with turbulence. Use of the recommended “natural” spline numerical method results in the emergence of spiking artifacts at the ends of various ground waveforms after propagating shaped sonic booms through turbulent atmospheric boundary layers. The four other available numerical methods of KZKFourier were investigated under identical atmospheric conditions: linear interpolation, Hermite spline, finite differences, and frequency domain solution. Effects of the post-processing application of a 25% taper to the results of each numerical method were also explored. The Hermite spline method did not produce spiking, is accurate, and has a faster runtime than other options, so this method is recommended for future KZKFourier simulations with similar atmospheric conditions and turbulence levels.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum and Exposition, 2023
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106996
DOIs
StatePublished - 2023
EventAIAA SciTech Forum and Exposition, 2023 - Orlando, United States
Duration: Jan 23 2023Jan 27 2023

Publication series

NameAIAA SciTech Forum and Exposition, 2023

Conference

ConferenceAIAA SciTech Forum and Exposition, 2023
Country/TerritoryUnited States
CityOrlando
Period1/23/231/27/23

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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