Abstract
A method of singularity is developed to predict the effect of sound absorbing wall liners on the unsteady aerodynamic forces for a linear cascade vibrating in subsonic uniform flow between parallel walls. A side wall of the model is partially composed of a sound absorbing liner with uniform acoustic admittance. The lined section of the wall is confined to the portion swept by blades.
| Original language | English |
|---|---|
| Pages (from-to) | 251-278 |
| Number of pages | 28 |
| Journal | Memoirs of the Faculty of Engineering, Kyushu University |
| Volume | 42 |
| Issue number | 4 |
| Publication status | Published - Dec 1982 |
| Externally published | Yes |
All Science Journal Classification (ASJC) codes
- Engineering(all)