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

Journal of Sound and Vibration

Volumn 320, Issue 1-2, 2009, Pages 163-183

  Chung, K W ^a   He, Y B ^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

DELTA SIGMA MODULATION; DYNAMIC RESPONSE; ELASTICITY; HYSTERESIS; PERTURBATION TECHNIQUES;

AEROELASTIC RESPONSES; AEROELASTIC SYSTEMS; BIFURCATION ANALYSES; DEGREE OF ACCURACIES; FREEPLAY; INCREMENTAL METHODS; LIMIT CYCLE OSCILLATIONS; LIMIT CYCLES; PERIODIC MOTIONS; POINCARE; PRESENT METHODS; STRUCTURAL NONLINEARITIES;

BIFURCATION (MATHEMATICS);

EID: 57349128447     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2008.07.019     Document Type: Article

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