Limit cycle oscillation and orbital stability in aeroelastic systems with torsional nonlinearity

Nonlinear Dynamics

Volumn 31, Issue 4, 2003, Pages 435-450

  Singh, Sahjendra N ^a   Brenner, Martin ^b  

^a UNIVERSITY OF NEVADA   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

Aeroelastic system; Describing function; Flutter; Limit cycle oscillation; Orbital stability

Indexed keywords

DAMPING; DEGREES OF FREEDOM (MECHANICS); TRANSFER FUNCTIONS;

LIMIT CYCLE OSCILLATIONS;

AERODYNAMICS;

EID: 0037666085     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1023264319167     Document Type: Article

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