Limit-cycle oscillations in high-aspect-ratio wings

Journal of Fluids and Structures

Volumn 15, Issue 1, 2001, Pages 107-132

  Patil, M J ^a   Hodges, D H ^a   Cesnik, C E S ^b  

^a Georgia Institute of Technology   (United States)

^b Massachusetts Institute of Technology Cambridge   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; FLUTTER; OSCILLATION; STRUCTURAL ANALYSIS;

EID: 0035527295     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1006/jfls.2000.0329     Document Type: Article

References (17)

1. Space-time mixed finite elements for rods
2. An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam
3. Nonlinear stall flutter and divergence analysis of cantilevered graphite/epoxy wings
4. On the presence of internal resonances in aeroelastic systems
5. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams
6. Investigating transient and limit cycle behaviors of a nonlinear structure by wavelet transforms
7. Experiments and analysis for composite blades under large deflections. Part ii - Dynamic behavior
8. Nonlinear aeroelastic response - Analyses and experiments
9. Nonlinear aeroelasticity and flight dynamics of aircraft in subsonic flow
10. Nonlinear aeroelastic analysis of aircraft with high-aspect-ratio wings
11. Nonlinear aeroelasticity and flight dynamics of high-altitude long-endurance aircraft
12. Finite-state airloads for deformable airfoils on fixed and rotating wings
13. Finite state induced flow models; Part I: Two-dimensional thin airfoil
14. Reduced-order aerodynamic model and its application to a nonlinear aeroelastic system
15. Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade