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2019 | OriginalPaper | Chapter

Benchmark on the Aerodynamics of a 5:1 Rectangular Cylinder: Further Experimental and LES Results

Authors : C. Mannini, A. Mariotti, L. Siconolfi, M. V. Salvetti

Published in: Direct and Large-Eddy Simulation XI

Publisher: Springer International Publishing

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Abstract

The flow around a rectangular cylinder, having chord-to-depth ratio equal to 5, has been the object of a benchmark (BARC) launched in 2008 (http://​www.​aniv-iawe.​org/​barc/​). The BARC configuration is of practical interest, e.g. in civil engineering, and, in spite of the simple geometry, the related flow dynamics and topology is complex. Indeed, the high-Reynolds-number flow around such a stationary rectangular cylinder is turbulent with flow separation from the upstream corners and unsteady reattachment on the cylinder side. Furthermore, a vortex shedding also occurs from the rear corners and interferes with the leading-edge vortices, according to the mechanism of impinging shear-layer instability (Nakamura et al, J Fluid Mech, 222:437–447, 1991, [1]).

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Literature
1.
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2.
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Metadata
Title
Benchmark on the Aerodynamics of a 5:1 Rectangular Cylinder: Further Experimental and LES Results
Authors
C. Mannini
A. Mariotti
L. Siconolfi
M. V. Salvetti
Copyright Year
2019
DOI
https://doi.org/10.1007/978-3-030-04915-7_56

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