Nonlinear aeroelastic behavior of an oscillating airfoil during stall-induced vibration

Journal of Fluids and Structures

Volumn 24, Issue 6, 2008, Pages 757-777

  Sarkar, S ^a   Bijl, H ^b  

^a INDIAN INSTITUTE OF TECHNOLOGY MADRAS   (India)

^b DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

Dynamic stall; Flap edgewise oscillation; Pitching oscillation; Stall flutter

Indexed keywords

AERODYNAMICS; AIRFOILS; BIFURCATION (MATHEMATICS); ELECTRIC GENERATORS; GAS DYNAMICS; HELICOPTER ROTORS; HYDRAULIC MACHINERY; HYDRAULIC MOTORS; MILITARY HELICOPTERS; NONLINEAR CONTROL SYSTEMS; SCHRODINGER EQUATION; SYSTEM STABILITY; TURBINES; TWO DIMENSIONAL; WIND POWER; WINGS;

AEROELASTIC INSTABILITIES; AEROELASTIC STABILITY; DYNAMIC STALL; DYNAMICAL BEHAVIORS; FLAP-EDGEWISE OSCILLATION; FORCED RESPONSES; INDUCED VIBRATIONS; INITIAL CONDITIONS; NONLINEAR AEROELASTIC BEHAVIOR; OSCILLATING AIRFOILS; OSCILLATION MODELS; PARAMETRIC STUDIES; PITCHING OSCILLATION; PITCHING OSCILLATIONS; QUASI-HARMONIC RESPONSE; ROTOR BLADES; STALL FLUTTER; STRUCTURAL DAMAGES; STRUCTURAL NONLINEARITY; SYSTEM PARAMETERS; SYSTEM RESPONSES;

DYNAMICAL SYSTEMS;

EID: 49049120518     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2007.11.004     Document Type: Article

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