Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings

AIAA Journal

Volumn 39, Issue 8, 2001, Pages 1430-1441

  Tang, D ^a   Dowell, E H ^a  

^a DUKE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; COMPUTER SIMULATION; DEFORMATION; PERTURBATION TECHNIQUES; SUBSONIC FLOW; SUPERSONIC FLOW; WIND TUNNELS; WINGS;

LIMIT-CYCLE OSCILLATIONS (LCO);

FLUTTER (AERODYNAMICS);

EID: 0035421036     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1484     Document Type: Article

References (9)

1. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades
2. Limit cycle oscillations in high-aspect-ratio wings
3. Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect ratio wings
4. Semi-empirical model for the dynamic stall of airfoils in view to the application to the calculation of responses of a helicopter blade in forward flight
5. An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam
6. Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft
7. On the importance of aerodynamic and structural geometrical nonlinearities on aeroelastic behavior of high-aspect-ratio wings
8. Experiments and analysis for composite blades under large deflections, part II: Dynamic behavior