A direct method for quantifying limit-cycle oscillation response characteristics in the presence of uncertainties

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2004, Pages 2032-2043

  Beran, Philip S ^a,b   Pettit, Chris L ^a,b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Multidisc Technologies Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CHAOS THEORY; COMPUTER SIMULATION; INCOMPRESSIBLE FLOW; ITERATIVE METHODS; MONTE CARLO METHODS; NONLINEAR SYSTEMS; OSCILLATORS (MECHANICAL); RANDOM PROCESSES; STIFFNESS; TIME DOMAIN ANALYSIS;

AEROELASTIC SYSTEM; HOPF POINT; LIMIT CYCLE OSCILLATIONS (LCO); TORSIONAL STRUCTURAL COUPLING;

FLUTTER (AERODYNAMICS);

EID: 16244397731     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-1695     Document Type: Conference Paper

References (19)

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