Evaluation of Reynolds number effects on flutter derivatives of a flat plate by means of a computational approach

Journal of Fluids and Structures

Volumn 24, Issue 7, 2008, Pages 1058-1076

  Bruno, L ^a   Fransos, D ^a  

^a POLITECNICO DI TORINO   (Italy)

Author keywords

Computational wind engineering; Flutter derivatives; Grid based methods; Indicial approach; Reynolds number effects

Indexed keywords

AERODYNAMICS; AIRFOILS; COMPUTATIONAL METHODS; FLOW OF FLUIDS; FLUID DYNAMICS; FLUID MECHANICS; FLUTTER (AERODYNAMICS); GAS DYNAMICS; KETONES; MIXED CONVECTION; REYNOLDS NUMBER; RHENIUM; TRANSFER FUNCTIONS; TWO DIMENSIONAL;

AEROELASTIC BEHAVIOUR; ARBITRARY LAGRANGIAN EULERIAN FORMULATIONS; COMPUTATIONAL APPROACH; COMPUTATIONAL COSTS; COMPUTATIONAL EVALUATION; COMPUTATIONAL WIND ENGINEERING; EFFICIENT METHODS; FINITE THICKNESS; FLAT PLATES; FLOW FIELDS; FLUID FLOWING; FLUTTER DERIVATIVES; FREQUENCY DOMAINS; GRID-BASED METHODS; INDICIAL APPROACH; MOVING PLATE; NAVIER-STOKES SOLVERS; NUMBER EFFECTS; PITCH MOTIONS; REYNOLDS; REYNOLDS NUMBER EFFECTS; STRUCTURAL MOTIONS; THIN AIRFOIL THEORY; TRANSIENT FORCES;

PLATES (STRUCTURAL COMPONENTS);

EID: 52749098984     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2008.03.001     Document Type: Article

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