Abstract
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.
Original language | English |
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Article number | 117253 |
Journal | Journal of Sound and Vibration |
Volume | 539 |
ISSN | 0022-460X |
DOIs | |
Publication status | Published - 24 Oct 2022 |
Bibliographical note
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
Keywords
- Aeroacoustics theory
- Green's functions
- Low Reynolds number flows
- Unsteady dissipation