Bifurcation analysis of aeroelastic systems with hysteresis by incremental harmonic balance method

Applied Mathematics and Computation

Volumn 219, Issue 5, 2012, Pages 2398-2411

  Liu, J K ^a   Chen, F X ^a   Chen, Y M ^a  

^a SUN YAT SEN UNIVERSITY   (China)

Author keywords

Aeroelastic system; Airfoil; Hysteresis; Incremental harmonic balance method

Indexed keywords

AEROELASTIC SYSTEM; BIFURCATION ANALYSIS; FLOQUET THEORY; FLOW SPEED; FREEPLAY; HYSTERESIS NONLINEARITY; INCREMENTAL HARMONIC BALANCE METHOD; ITERATIVE SCHEMES; LIMIT CYCLE OSCILLATIONS; METHOD OF UNDETERMINED COEFFICIENTS; NUMERICAL EXAMPLE; NUMERICAL RESULTS; PRE LOADS; SADDLE NODE BIFURCATION; SYMMETRY-BREAKING;

AEROELASTICITY; AIRFOILS; BIFURCATION (MATHEMATICS); ITERATIVE METHODS;

HYSTERESIS;

EID: 84868208351     PISSN: 00963003     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.amc.2012.08.034     Document Type: Article

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