Limit cycle oscillation of missile control fin with structural non-linearity

Journal of Sound and Vibration

Volumn 269, Issue 3-5, 2004, Pages 669-687

  Bae, J S ^a   Lee, I ^a  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; FLUTTER (AERODYNAMICS); FRICTION; HINGES; HYSTERESIS; LAPLACE TRANSFORMS; PROJECTILES; STIFFNESS MATRIX; WINGS;

FLIGHT VEHICLES; LIMIT CYCLE OSCILLATIONS (LCO); MISSILE CONTROL FINS;

OSCILLATIONS;

EID: 0346500813     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0022-460X(03)00125-1     Document Type: Article

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