Active Flutter Suppression of a Wing Section in the Subsonic, Sonic and Supersonic Regimes by the H ∞ Control Method.
- Resource Type
- Article
- Source
- Aerospace (MDPI Publishing); Mar2024, Vol. 11 Issue 3, p198, 23p
- Subject
FLUTTER (Aerodynamics) UNSTEADY flow (Aerodynamics) POLE assignment SUPERSONIC flow COMPRESSIBLE flow AERODYNAMIC load - Language
- ISSN
- 22264310