TY - JOUR
T1 - Aerodynamic sound generation in thermoviscous fluids
T2 - A canonical problem revisited
AU - Morfey, Christopher L.
AU - Sorokin, Sergey V.
AU - Wright, Matthew C.M.
N1 - Funding Information:
This research did not receive any specific grant from funding agencies in the public, commercial, or not-for-profit sectors. The authors are grateful for the anonymous reviewers’ helpful comments.
Publisher Copyright:
© 2022
PY - 2022/10/24
Y1 - 2022/10/24
N2 - Although the Lighthill–Curle acoustic analogy theory is formally exact, the presence of linear source terms related to viscous stresses and non-isentropic density changes makes it unsuitable for studying aerodynamic sound generation in low Reynolds number thermoviscous flows. Here we use an extension of the Ffowcs Williams and Hawkings formulation, with thermoviscous effects explicitly included, to find an analytical solution to the canonical problem of sound radiation from a circular cylinder immersed in a viscous heat-conducting fluid and rotating sinusoidally about its axis. Existing published solutions are compared and an earlier null result is explained. The new analysis reveals the dominant source of sound at low Mach numbers to be unsteady viscous dissipation rather than Reynolds-stress quadrupoles, unless the fluid parameter B=αc2/cp is zero.
AB - Although the Lighthill–Curle acoustic analogy theory is formally exact, the presence of linear source terms related to viscous stresses and non-isentropic density changes makes it unsuitable for studying aerodynamic sound generation in low Reynolds number thermoviscous flows. Here we use an extension of the Ffowcs Williams and Hawkings formulation, with thermoviscous effects explicitly included, to find an analytical solution to the canonical problem of sound radiation from a circular cylinder immersed in a viscous heat-conducting fluid and rotating sinusoidally about its axis. Existing published solutions are compared and an earlier null result is explained. The new analysis reveals the dominant source of sound at low Mach numbers to be unsteady viscous dissipation rather than Reynolds-stress quadrupoles, unless the fluid parameter B=αc2/cp is zero.
KW - Aeroacoustics theory
KW - Green's functions
KW - Low Reynolds number flows
KW - Unsteady dissipation
UR - http://www.scopus.com/inward/record.url?scp=85137584246&partnerID=8YFLogxK
U2 - 10.1016/j.jsv.2022.117253
DO - 10.1016/j.jsv.2022.117253
M3 - Journal article
AN - SCOPUS:85137584246
SN - 0022-460X
VL - 539
JO - Journal of Sound and Vibration
JF - Journal of Sound and Vibration
M1 - 117253
ER -