Limit cycle oscillations of aircraft due to flutter-induced drag

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2002, Pages 1614-1624

  Patil, Mayuresh J ^a  

^a WIDENER UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; AIRCRAFT PROPULSION; DRAG; OSCILLATIONS; STRUCTURAL ANALYSIS; VIBRATIONS (MECHANICAL); WINGS;

LIMIT CYCLE OSCILLATIONS (LCO); STRUCTURAL INSTABILITY;

FLUTTER (AERODYNAMICS);

EID: 0036078672     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-1409     Document Type: Conference Paper

References (10)

1. Nonlinear stall flutter and divergence analysis of cantilevered graphite/epoxy wings
2. Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade
3. Nonlinear aeroelastic response - Analyses and experiments
4. Limit cycle oscillations in high-aspect-ratio wings
5. From fluttering wings to flapping flight: The energy connection
6. Eigenanalysis of unsteady flows about airfoils, cascades, and wings
7. Present state of development in non-steady motion of a lifting surface
8. General aerodynamic theory - Perfect fluids
9. General theory of aerodynamic instability and the mechanism of flutter
10. Propulsion of flapping and oscillating airfoil