Active and passive suppressions of nonlinear panel flutter using finite element method

AIAA Journal

Volumn 39, Issue 11, 2001, Pages 2042-2050

  Moon, Seong Hwan ^a,b   Kim, Seung Jo ^a,b  

^a Seoul National University   (South Korea)

^b Department of Aerospace Engineering ^*  (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ATTENUATION; CONTROL THEORY; DAMPING; ELECTRIC POWER SYSTEMS; FINITE ELEMENT METHOD; GENETIC ALGORITHMS; LEAD COMPOUNDS; MODAL ANALYSIS; NUMERICAL METHODS; OPTIMAL CONTROL SYSTEMS; PIEZOELECTRIC DEVICES; ROBUSTNESS (CONTROL SYSTEMS); TIME DOMAIN ANALYSIS;

NONLINEAR PANEL FLUTTER; PASSIVE SUPPRESSIONS; QUASI-STEADY PISTON THEORY;

FLUTTER (AERODYNAMICS);

EID: 0035506651     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1217     Document Type: Article

References (11)

1. Controlling panel flutter using adaptive materials
2. Suppression of nonlinear panel flutter with piezoelectric actuators using finite element
3. Damping of structural vibrations with piezoelectric materials and passive electrical networks
4. Multimodal passive vibration suppression with piezoelectric materials and resonant shunts
5. Sliding mode control of structural vibrations via active-passive hybrid piezoelectric network
6. An experimental comparison of piezoelectric and constrained layer damping
7. Improvement of aeroelastic stability of hingeless helicopter rotor blade by passive piezoelectric damping
8. Nonlinear oscillations of a fluttering plate
9. Finite time domain-modal formulation for nonlinear flutter of composite panels