The paper outlines a framework for the analysis of bridges under wind excitation, based on structural finite element modeling and on cross-sectional aerodynamic load models. After a brief review, a time-domain load model for self-excited actions accounting for unsteadiness, mean angle of attack, along wind forces and displacements, asymptotically converging to the steady model is proposed. Afterwards, by means of a numerical example based on the quasi-steady load model, two facts are investigated: (1) the effects of the mean steady configuration on aerodynamic stability; and (2) the effects of load nonlinearities on the response. The results point out that: (1) the modifications in structural stiffness and aerodynamic properties due to steady deformation both affects the aerodynamic stability threshold, especially in case of bluff aerodynamics; (2) nonlinear loads produces larger structural response than linearized loads.
Three-dimensional simulations of suspension bridges under wind load: Numerical approach in the time domain / L.Salvatori;P.Spinelli. - ELETTRONICO. - (2005), pp. 1-13. (Intervento presentato al convegno The Fourth European & African Conference on Wind Engineering tenutosi a Prague, Czech Republic nel 11-15 luglio 2005).
Three-dimensional simulations of suspension bridges under wind load: Numerical approach in the time domain
SALVATORI, LUCA;SPINELLI, PAOLO
2005
Abstract
The paper outlines a framework for the analysis of bridges under wind excitation, based on structural finite element modeling and on cross-sectional aerodynamic load models. After a brief review, a time-domain load model for self-excited actions accounting for unsteadiness, mean angle of attack, along wind forces and displacements, asymptotically converging to the steady model is proposed. Afterwards, by means of a numerical example based on the quasi-steady load model, two facts are investigated: (1) the effects of the mean steady configuration on aerodynamic stability; and (2) the effects of load nonlinearities on the response. The results point out that: (1) the modifications in structural stiffness and aerodynamic properties due to steady deformation both affects the aerodynamic stability threshold, especially in case of bluff aerodynamics; (2) nonlinear loads produces larger structural response than linearized loads.File | Dimensione | Formato | |
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