Incremental harmonic balance method for nonlinear flutter of an airfoil with uncertain-but-bounded parameters

Applied Mathematical Modelling

Volumn 36, Issue 2, 2012, Pages 657-667

  Chen, Y M ^a   Liu, J K ^a   Meng, G ^b  

^a SUN YAT SEN UNIVERSITY   (China)

^b SHANGHAI JIAO TONG UNIVERSITY   (China)

Author keywords

Incremental harmonic balance method; Limit cycle oscillation; Nonlinear flutter; Statistic; Uncertainty

Indexed keywords

ACTIVE PARAMETERS; BOUNDED PARAMETERS; BOUNDED UNCERTAINTY; INCREMENTAL HARMONIC BALANCE METHOD; LIMIT CYCLE OSCILLATIONS; MONTE CARLO SIMULATION; NONLINEAR FLUTTER; NONLINEAR FLUTTERS; NUMERICAL EXAMPLE; PARAMETER VARIABILITY; PITCH STIFFNESS; SOLUTION PROCESS; STATISTICAL PROPERTIES; STOCHASTIC PARAMETERS; STRONGLY NONLINEAR; TWO-DIMENSIONAL AIRFOILS; UNCERTAIN-BUT-BOUNDED PARAMETERS; UNCERTAINTY; VARIABLE PARAMETERS; WIND SPEED;

AIRFOILS; COMPUTER SIMULATION; FIGHTER AIRCRAFT; FLUTTER (AERODYNAMICS); HARMONIC ANALYSIS; INCOMPRESSIBLE FLOW; MONTE CARLO METHODS; OSCILLATING FLOW; PLATES (STRUCTURAL COMPONENTS); STATISTICS; TIME VARYING SYSTEMS; VIBRATION ANALYSIS;

UNCERTAINTY ANALYSIS;

EID: 80053572814     PISSN: 0307904X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.apm.2011.07.016     Document Type: Article

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