Experimental and theoretical study of gust response for high-aspect-ratio wing

AIAA Journal

Volumn 40, Issue 3, 2002, Pages 419-429

  Tang, Deman ^a   Dowell, Earl H ^a  

^a DUKE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; BOUNDARY CONDITIONS; EQUATIONS OF MOTION; FLUTTER (AERODYNAMICS); OSCILLATIONS; PERTURBATION TECHNIQUES; WIND EFFECTS;

HIGH-ASPECT-RATIO WINGS;

WINGS;

EID: 0036493461     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1691     Document Type: Article

References (11)

1. Nonlinear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades
2. Nonlinear aeroelastic analysis of complete aircraft in subsonic flow
3. Limit cycle oscillations in high-aspect-ratio wings
4. Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect ratio wings
5. Importance of aerodynamic and structural geometrical nonlinearities on aeroelastic behavior of high-aspect-ratio wings
6. Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings
7. Experiments and analysis for a gust generator in a wind tunnel
8. 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
9. Experiments and analysis for composite blades under large deflections, Part II: Dynamic behavior
10. Nonlinear response of a non-rotating rotor blade to a periodic gust