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 |
|---|---|
| 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