Abstract
A unique concept for suppression of trailing edge noise scattering from a splitter plate in a low Reynolds number flow is proposed. The key idea of the concept is the adoption of a structural compliance system embedded with a finite number of elastic panels. Specific compliance system designs are devised for promotion of panel structural resonance that effectively absorbs broadband flow/acoustic fluctuation energy responsible for noise scattering. The concept is examined using high-fidelity direct aeroacoustic simulation together with spatiotemporal aeroacoustic-structural interaction analysis. The concept is confirmed feasible and outperforms many similar trailing edge noise reduction approaches reported in the literature.
| Original language | English |
|---|---|
| Article number | 023602 |
| Number of pages | 8 |
| Journal | JASA Express Letters |
| Volume | 3 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 21 Feb 2023 |
Bibliographical note
Publisher Copyright:© 2023 Author(s).