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<dc:title>3D LES simulations of a static and vertically free-to-oscillate 4:1 rectangular cylinder: effects of the grid resolution</dc:title>
<dc:creator>Álvarez Naveira, Antonio José</dc:creator>
<dc:creator>Nieto Mouronte, Félix</dc:creator>
<dc:creator>Nguyen, D.T.</dc:creator>
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<dc:subject>3D LES</dc:subject>
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<dc:subject>Vortex shedding</dc:subject>
<dc:subject>Vortex induced vibrations</dc:subject>
<dc:subject>Spatial discretisation</dc:subject>
<dc:subject>Correlations</dc:subject>
<dc:subject>Coherence</dc:subject>
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<dcterms:abstract>[Abstract:] In the present study, the aerodynamics of the flow fields around a static and vertically free-to-oscillate 4:1 rectangular cylinder are analysed by means of 3D LES simulations, adopting the OneEqEddy viscosity model. Integral parameters, pressure distributions, amplitudes of oscillation, coherences and correlations are obtained and compared with the available experimental data. Aiming to ascertain the impact of the boundary conditions and the grid resolution on the accuracy of results, five cases adopting 3 different meshes including two different spanwise discretisations have been considered. When studying the aerodynamics of the cylinder in static conditions, the influence of the spatial discretisation is very limited, and the agreement with experimental data is fairly good. On the other hand, for the free-to-oscillate cylinder, the structural response is dramatically dependent on the spanwise discretisation. The maximum amplitude of the structural response decreases as the mesh resolution increases, providing a closer fit with the experimental data. Also, the spanwise correlation of pressures is studied, finding remarkable differences depending on the level of spatial discretisation.</dcterms:abstract>
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<dc:identifier>Álvarez, A. J., Nieto, F., Nguyen, D. T., Owen, J. S., Hernández, S. (2019). 3D LES simulations of a static and vertically free-to-oscillate 4:1 rectangular cylinder: Effects of the grid resolution. Journal of Wind Engineering and Industrial Aerodynamics, 192, p. 31-44.</dc:identifier>
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<dc:title>3D LES simulations of a static and vertically free-to-oscillate 4:1 rectangular cylinder: effects of the grid resolution</dc:title>
<dc:creator>Álvarez Naveira, Antonio José</dc:creator>
<dc:creator>Nieto Mouronte, Félix</dc:creator>
<dc:creator>Nguyen, D.T.</dc:creator>
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<dc:creator>Hernández, Santiago</dc:creator>
<dc:subject>3D LES</dc:subject>
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<dc:subject>Vortex shedding</dc:subject>
<dc:subject>Vortex induced vibrations</dc:subject>
<dc:subject>Spatial discretisation</dc:subject>
<dc:subject>Correlations</dc:subject>
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<dc:description>[Abstract:] In the present study, the aerodynamics of the flow fields around a static and vertically free-to-oscillate 4:1 rectangular cylinder are analysed by means of 3D LES simulations, adopting the OneEqEddy viscosity model. Integral parameters, pressure distributions, amplitudes of oscillation, coherences and correlations are obtained and compared with the available experimental data. Aiming to ascertain the impact of the boundary conditions and the grid resolution on the accuracy of results, five cases adopting 3 different meshes including two different spanwise discretisations have been considered. When studying the aerodynamics of the cylinder in static conditions, the influence of the spatial discretisation is very limited, and the agreement with experimental data is fairly good. On the other hand, for the free-to-oscillate cylinder, the structural response is dramatically dependent on the spanwise discretisation. The maximum amplitude of the structural response decreases as the mesh resolution increases, providing a closer fit with the experimental data. Also, the spanwise correlation of pressures is studied, finding remarkable differences depending on the level of spatial discretisation.</dc:description>
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