Double flutter in an aeroelastic system

AIAA Journal

Volumn 39, Issue 6, 2001, Pages 1206-1208

  Chamara, P A ^a   Coller, B D ^a  

^a University of Illinois at Chicago   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; AIRFOILS; BIFURCATION (MATHEMATICS); COMPUTER SIMULATION; EIGENVALUES AND EIGENFUNCTIONS; EQUATIONS OF MOTION; MATHEMATICAL MODELS; VELOCITY;

HOPF-HOPF BIFURCATION; VORTEX LATTICE SIMULATION;

FLUTTER (AERODYNAMICS);

EID: 0035369441     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1436     Document Type: Article

References (8)

1. Limit cycle behavior of an airfoil with a control surface
2. Surge/stall interactions in compressors part I: Theoretical development
3. Application of continuous vorticity panels to general unsteady incompressible two-dimensional lifting flows
4. Eigenanalysis of unsteady flows, about airfoils, cascades, and wings
5. Semi-empirical model for the dynamic stall of airfoils in view of the application to the calculation of responses of a helicopter blade in forward flight
6. Structural nonlinearities and the nature of the classic flutter instability