The paper deals with the simulation of the dynamic nonlinear behaviour of seabed anchored submerged floating tunnels (SFTs) under environmental excitation, by addressing the problem of vortex induced excitation. A model based on the ‘fluid oscillator’ approach is proposed, tailored to be coupled to a geometrically non linear FE developed, for the anchor bars, in a previous work. The approach allows for representing the entire anchoring bar, thus reducing the computational effort required for global modelling of the SFT. In this light, mainly based on a lumped fluid oscillator model, a computationally more efficient approach is here sought in the form of a continuous model (Distributed Vortex Layer - DVL). This consists of a distributed ‘aerodynamic’ mass which is connected to the structural element and to a fixed reference system by distributed non linear spring-dashpot elements. Governing equations of motion are obtained substituting Galerkin-type decomposition of both the structure and the aerodynamic mass displacements; global equations of motion are integrated by a step-by-step procedure based on the Newmark method. Validations of the numerical model are finally given, regarding experimental results obtained for two basic structures: an elastically suspended rigid cylinder and a long slender cylinder.
Vortex Induced Vibration in Submerged Floating Tunnels: DVL a Distributed Vortex Layer Model
PEROTTI, FEDERICO;DI PILATO, MARIA GRAZIA
2009-01-01
Abstract
The paper deals with the simulation of the dynamic nonlinear behaviour of seabed anchored submerged floating tunnels (SFTs) under environmental excitation, by addressing the problem of vortex induced excitation. A model based on the ‘fluid oscillator’ approach is proposed, tailored to be coupled to a geometrically non linear FE developed, for the anchor bars, in a previous work. The approach allows for representing the entire anchoring bar, thus reducing the computational effort required for global modelling of the SFT. In this light, mainly based on a lumped fluid oscillator model, a computationally more efficient approach is here sought in the form of a continuous model (Distributed Vortex Layer - DVL). This consists of a distributed ‘aerodynamic’ mass which is connected to the structural element and to a fixed reference system by distributed non linear spring-dashpot elements. Governing equations of motion are obtained substituting Galerkin-type decomposition of both the structure and the aerodynamic mass displacements; global equations of motion are integrated by a step-by-step procedure based on the Newmark method. Validations of the numerical model are finally given, regarding experimental results obtained for two basic structures: an elastically suspended rigid cylinder and a long slender cylinder.File | Dimensione | Formato | |
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