TY - GEN
T1 - Numerical Method Comparison on Shaped Sonic Boom Propagation Through Atmospheric Boundary Layer Turbulence
AU - Kapcsos, Joshua L.
AU - Sparrow, Victor W.
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - 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.
AB - 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.
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U2 - 10.2514/6.2023-1352
DO - 10.2514/6.2023-1352
M3 - Conference contribution
AN - SCOPUS:85199108515
SN - 9781624106996
T3 - AIAA SciTech Forum and Exposition, 2023
BT - AIAA SciTech Forum and Exposition, 2023
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2023
Y2 - 23 January 2023 through 27 January 2023
ER -