Aeroelastic response of an airfoil-aileron combination with freeplay in aileron hinge

Journal of Aircraft

Volumn 39, Issue 4, 2002, Pages 711-713

  Alighanbari, H ^a  

^a RYERSON UNIVERSITY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; DESCRIBING FUNCTIONS; DYNAMIC RESPONSE; FINITE DIFFERENCE METHOD; FLUTTER (AERODYNAMICS); HINGES; INTEGRATION; LAPLACE TRANSFORMS; OSCILLATIONS; STATE SPACE METHODS; STIFFNESS; STRUCTURAL ANALYSIS;

STATE-SPACE APPROXIMATION;

AIRFOILS;

EID: 0036650261     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2986     Document Type: Article

References (7)

1. An investigation of effects of certain types of structural nonlinearities on wing and control surface flutter
2. Effects of structural nonlinearities on aircraft vibration and flutter
3. Experimental and theoretical study of nonlinear flutter
4. Flutter and stall response of a helicopter blade with structural nonlinearity
5. The aeroelastic response of a two dimensional airfoil with bilinear and cubic structural non-linearities
6. Behavior of airfoil with control surface freeplay for nonzero angle of attack
7. Aeroelastic response of an airfoil-aileron combination with structural nonlinearities