TY - GEN
T1 - Asymptotic analysis of wave packets in high-speed boundary layers
AU - Bailey, Michelle
AU - Tumin, Anatoli
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2022
Y1 - 2022
N2 - Asymptotic methods are utilized to analyze the propagation of linear, three-dimensional and two-dimensional wave packets in a weakly non-parallel, compressible, zero pressure gradient, boundary layer over a flat plate. Wave packets generated due to a low amplitude coherent perturbation are analyzed in the framework of Linear Stability Theory while omitting the effect of receptivity. Application of two asymptotic techniques, namely the steepest descent method and a Gaussian model are demonstrated. The steepest descent method is used to identify the frequency and spanwise wavenumber of the disturbance wave with the maximum amplitude in the wavepacket at a given location and a Gaussian approximation around these disturbance parameters is used to construct the fine structures of the wavepacket. Details of the wavepacket evolution in boundary layers with edge Mach numbers, Me = 2 and Me = 7 are presented and validity of the asymptotic techniques for these flow conditions are discussed.
AB - Asymptotic methods are utilized to analyze the propagation of linear, three-dimensional and two-dimensional wave packets in a weakly non-parallel, compressible, zero pressure gradient, boundary layer over a flat plate. Wave packets generated due to a low amplitude coherent perturbation are analyzed in the framework of Linear Stability Theory while omitting the effect of receptivity. Application of two asymptotic techniques, namely the steepest descent method and a Gaussian model are demonstrated. The steepest descent method is used to identify the frequency and spanwise wavenumber of the disturbance wave with the maximum amplitude in the wavepacket at a given location and a Gaussian approximation around these disturbance parameters is used to construct the fine structures of the wavepacket. Details of the wavepacket evolution in boundary layers with edge Mach numbers, Me = 2 and Me = 7 are presented and validity of the asymptotic techniques for these flow conditions are discussed.
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U2 - 10.2514/6.2022-1707
DO - 10.2514/6.2022-1707
M3 - Conference contribution
AN - SCOPUS:85123633363
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -