Abstract
This paper describes the results of initial experiments using polynomial neural network based feedback control to reduce flow-induced vibration in aircraft panels due to turbulent boundary layer/structural interaction. The experiments consist of computer simulations used to develop and analyze feedback control strategies to reduce vibration in a beam subjected to turbulent and transitional boundary layers. The experiments suggest that significant suppression of flow-induced vibration can be accomplished through this technique.
Original language | English (US) |
---|---|
Title of host publication | Active Control of Noise and Vibration - 1992 |
Publisher | Publ by ASME |
Pages | 33-46 |
Number of pages | 14 |
Volume | 38 |
ISBN (Print) | 0791810933 |
State | Published - Dec 1 1992 |
Externally published | Yes |
Event | Winter Annual Meeting of the American Society of Mechanical Engineers - Anaheim, CA, USA Duration: Nov 8 1992 → Nov 13 1992 |
Other
Other | Winter Annual Meeting of the American Society of Mechanical Engineers |
---|---|
City | Anaheim, CA, USA |
Period | 11/8/92 → 11/13/92 |
All Science Journal Classification (ASJC) codes
- Software
- Mechanical Engineering