Abstract
A method is presented for the computation of the acoustic field around a tonal circular source, such as a rotor or propeller, based on an exact formulation which is valid in the near and far fields. The only input data required are the pressure field sampled on a cylindrical surface surrounding the source, with no requirement for acoustic velocity or pressure gradient information. The formulation is approximated with exponentially small errors and appears to require input data at a theoretically minimal number of points. The approach is tested numerically, with and without added noise, and demonstrates excellent performance, especially when compared to extrapolation using a far-field
assumption.
assumption.
Original language | English |
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Pages (from-to) | 1623-1629 |
Number of pages | 7 |
Journal | Journal of the Acoustical Society of America |
Volume | 143 |
Issue number | 3 |
DOIs | |
Publication status | Published - 26 Mar 2018 |
ASJC Scopus subject areas
- Arts and Humanities (miscellaneous)
- Acoustics and Ultrasonics