Abstract
Feedback control is used to suppress oscillations in the subsonic flow past a rectangular cavity. A heuristic feedback law is introduced into 2D direct numerical simulations, using zero-net-mass forcing at the leading edge of the cavity and a pressure sensor at the wall, and the oscillations are reduced by -13 dB. Reduced-order models are obtained from full-order direct numerical simulations, and used to design observers to reconstruct the full flow information from a single pressure measurement at the wall, and these observers are shown to be more effective than Linear Stochastic Estimation (LSE), which is commonly used for this purpose. Initial results of a new experiment are also given, and a model for designing zero-net-mass actuators with a desired bandwidth is presented, along with experimental data which supports the model predictions.
| Original language | English (US) |
|---|---|
| Pages | 1577-1587 |
| Number of pages | 11 |
| DOIs | |
| State | Published - 2005 |
| Event | 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: Jan 10 2005 → Jan 13 2005 |
Other
| Other | 43rd AIAA Aerospace Sciences Meeting and Exhibit |
|---|---|
| Country/Territory | United States |
| City | Reno, NV |
| Period | 1/10/05 → 1/13/05 |
All Science Journal Classification (ASJC) codes
- General Engineering