Open/closed-loop nonlinear aeroelasticlty for airfoils via volterra series approach

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2002, Pages 2256-2266

  Marzocca, Piergiovanni ^a   Silva, Walter A ^a   Librescu, Liviu ^a  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CLOSED LOOP CONTROL SYSTEMS; EIGENVALUES AND EIGENFUNCTIONS; FEEDBACK CONTROL; NONLINEAR CONTROL SYSTEMS;

NONLINEAR AEROELASTICITY;

FLUTTER (AERODYNAMICS);

EID: 0036079150     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (20)

1. "Aeroelastic stability of orthotropic heterogeneous thin panels in the vicinity of the flutter critical boundary," Part I
2. Nonlinear stability and response of lifting surfaces via volterra series
3. Aeroelastic response of nonlinear wing section by functional series technique
4. Reduced-order models based on linear and nonlinear aerodynamic impulse response
5. Application of nonlinear systems theory to transonic unsteady aerodynamic responses
6. Aeroelastic response of swept aircraft wings in a compressible flow field
7. Unified approach of aeroelastic response and flutter of swept aircraft wings in an incompressible flow
8. Response of laminated composite flat panels to sonic boom and explosive blast loading
9. Bending vibration control of cantilevers via boundary moment and combined feedback control laws
10. Identification and control of limit cycle oscillations in aeroelastic systems
11. Nonlinear response of airfoil section with control surface freeplay to gust loads
12. Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment