TY - GEN
T1 - The calculation of sound propagation in nonuniform flows
T2 - 41st Aerospace Sciences Meeting and Exhibit 2003
AU - Agarwal, Anurag
AU - Morrisy, Philip J.
AU - Mani, Ramani
PY - 2003
Y1 - 2003
N2 - Acoustic waves propagating through nonuniform flows are subject to convection and refraction. Most noise prediction schemes use a linear wave operator to capture these effects. However, the wave operator can also support instability waves that, for a jet, are the well-known Kelvin-Helmholtz instabilities. These are convective instabilities that can completely overwhelm the acoustic solution downstream of the source location. In this paper, a general technique to filter out the instability waves is presented. A mathematical analysis is presented that demonstrates that the instabilities are suppressed if the governing equations are solved by a direct solver in the frequency domain, if a time-harmonic response is assumed. Also, a buffer-zone treatment for a non-reflecting boundary condition implementation in the frequency domain is developed. The outgoing waves are damped in the buffer zone simply by adding positive imaginary values to the required real frequency of the response. An analytical solution to a one-dimensional model problem, as well as numerical and analytical solutions to a two-dimensional jet instability problem, are provided. They demonstrate the effectiveness, robustness, and simplicity of the present technique.
AB - Acoustic waves propagating through nonuniform flows are subject to convection and refraction. Most noise prediction schemes use a linear wave operator to capture these effects. However, the wave operator can also support instability waves that, for a jet, are the well-known Kelvin-Helmholtz instabilities. These are convective instabilities that can completely overwhelm the acoustic solution downstream of the source location. In this paper, a general technique to filter out the instability waves is presented. A mathematical analysis is presented that demonstrates that the instabilities are suppressed if the governing equations are solved by a direct solver in the frequency domain, if a time-harmonic response is assumed. Also, a buffer-zone treatment for a non-reflecting boundary condition implementation in the frequency domain is developed. The outgoing waves are damped in the buffer zone simply by adding positive imaginary values to the required real frequency of the response. An analytical solution to a one-dimensional model problem, as well as numerical and analytical solutions to a two-dimensional jet instability problem, are provided. They demonstrate the effectiveness, robustness, and simplicity of the present technique.
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M3 - Conference contribution
AN - SCOPUS:84894742100
SN - 9781624100994
T3 - 41st Aerospace Sciences Meeting and Exhibit
BT - 41st Aerospace Sciences Meeting and Exhibit
Y2 - 6 January 2003 through 9 January 2003
ER -