A linearized parametric continuum model of a long-span suspension bridge is coupled with a nonlinear quasi-steady aero-dynamic model giving the aeroelastic partial differential equations of motion reduced to the state-space ordinary differential form by adopting the Galerkin method. Numerical time-domain simulations are performed to investigate the limit cycle oscillations occurring in the range of post-flutter wind speeds. Continuation tools are thus employed to path follow the limit cycles past the flutter speed where the Hopf bifurcation occurs. The stable post-flutter behavior, which can significantly affect the bridge by fatigue, terminate at a fold bifurcation. This result represents an important assessment of the conducted aeroelastic investigations. The stability range of the limit cycle oscillations is evaluated by carrying out sensitivity analyses with respect to the main design parameters, such as the structural damping and the initial wind angle of attack. Copyright © 2013 by ASME.
Post-flutter bifurcation behavior in long-span suspension bridges / Arena, Andrea; Lacarbonara, Walter; Piergiovanni, Marzocca. - ELETTRONICO. - 7 A:(2013), p. V07AT10A062. (Intervento presentato al convegno ASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE 2013 tenutosi a Portland, OR nel 4 August 2013 through 7 August 2013) [10.1115/detc2013-12429].
Post-flutter bifurcation behavior in long-span suspension bridges
ARENA, ANDREA;LACARBONARA, Walter;
2013
Abstract
A linearized parametric continuum model of a long-span suspension bridge is coupled with a nonlinear quasi-steady aero-dynamic model giving the aeroelastic partial differential equations of motion reduced to the state-space ordinary differential form by adopting the Galerkin method. Numerical time-domain simulations are performed to investigate the limit cycle oscillations occurring in the range of post-flutter wind speeds. Continuation tools are thus employed to path follow the limit cycles past the flutter speed where the Hopf bifurcation occurs. The stable post-flutter behavior, which can significantly affect the bridge by fatigue, terminate at a fold bifurcation. This result represents an important assessment of the conducted aeroelastic investigations. The stability range of the limit cycle oscillations is evaluated by carrying out sensitivity analyses with respect to the main design parameters, such as the structural damping and the initial wind angle of attack. Copyright © 2013 by ASME.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
