Bifurcation analysis of a two-degree-of-freedom aeroelastic system with freeplay structural nonlinearity by a perturbation-incremental method

Journal of Sound and Vibration

Volumn 299, Issue 3, 2007, Pages 520-539

  Chung, K W ^a   Chan, C L ^a   Lee, B H K ^b  

^a CITY UNIVERSITY OF HONG KONG   (Hong Kong)

^b NATIONAL RESEARCH COUNCIL CANADA   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

BIFURCATION (MATHEMATICS); CONTROL NONLINEARITIES; DEGREES OF FREEDOM (MECHANICS); HARMONIC ANALYSIS; OSCILLATIONS; PERTURBATION TECHNIQUES; STRUCTURAL ANALYSIS;

AEROELASTIC SYSTEMS; BIFURCATION ANALYSIS; FLOQUET THEORY; LIMIT CYCLE OSCILLATIONS (LCO);

AERODYNAMICS;

EID: 33750313407     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2006.06.059     Document Type: Article

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