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http://dx.doi.org/10.12989/was.2013.16.4.341

Maximum Vortex-Induced Vibrations of a square prism  

Barrero-Gil, A. (Aerospace Thermal and Fluids Mechanics Department, School of Aeronautics, Universidad Politecnica de Madrid)
Fernandez-Arroyo, P. (Aerospace Thermal and Fluids Mechanics Department, School of Aeronautics, Universidad Politecnica de Madrid)
Publication Information
Wind and Structures / v.16, no.4, 2013 , pp. 341-354 More about this Journal
Abstract
This paper presents an experimental investigation concerning the peak amplitudes of oscillation of a square prism due to Vortex-Induced-Vibrations (VIV) as a function of the mass damping parameter $m^*{\zeta}$ (the so called Griffin--plot); $m^*$ and ${\zeta}$ being, respectively, the non-dimensional mass and the mechanical (structural) damping ratio. With this purpose in mind, an electromagnetic actuator has been employed to provide controlled damping. During the experiments the mass--damping parameter was in the range 0.15 < $m^*{\zeta}$ < 2.4. Experiments show that there is a value of $m^*{\zeta}$ below which VIV appears combined with galloping and the prism oscillation increases monotonically with the incoming flow velocity. For $m^*{\zeta}$ >0.3 the present experiments show a well-defined VIV phenomenon and, consequently, a Griffin-plot can be defined.
Keywords
Vortex-Induced Vibrations; Griffin plot; square prism;
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