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Aspect-ratio effect on the wake of a wall-mounted square cylinder immersed in a turbulent boundary layer
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. (FLOW)ORCID iD: 0000-0002-5730-4430
Dipartimento di Scienze e Tecnologie Aerospaziali, Politecnico di Milano, Milan, Italy.ORCID iD: 0000-0003-0790-8460
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0001-5723-9571
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0001-9902-6216
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2025 (English)In: International Journal of Heat and Fluid Flow, ISSN 0142-727X, E-ISSN 1879-2278, Vol. 112, article id 109672Article in journal (Refereed) Published
Abstract [en]

The wake topology behind a wall-mounted square cylinder immersed in a turbulent boundary layer is investigated using high-resolution large-eddy simulations (LES). The boundary-layer thickness at the obstacle location is fixed, with a Reynolds number based on cylinder height ℎ and free-stream velocity 𝑢∞ of 10,000 while the aspect ratio (AR), defined as obstacle height divided by its width, ranges from 1 to 4. The mesh resolution is comparable to DNS standards used for similar wall-mounted obstacles, though with relatively lower Reynolds numbers. The effects of AR on wake structures, turbulence production, and transport are analyzed via Reynolds stresses, anisotropy-invariant maps (AIM), and the turbulent kinetic energy (TKE)budget. In particular, the transition from ‘‘dipole’’ to a ‘‘quadrupole’’ wake is extensively examined as AR increases. With increasing AR, the wake shrinks in both the streamwise and spanwise directions, attributed to the occurrence of the base vortices (AR = 3 and 4). This change in the flow structure also affects the size of the positive-production region that extends from the roof and the flank of the obstacle to the wake core. The AIMs confirm three-dimensional wake features, showing TKE redistribution in all directions (Simonsen and Krogstad, 2005). Stronger turbulence production in AR = 3 and 4 cases highlights the role of tip and base vortices behind the cylinder. The overall aim is to refine the dipole-to-quadrupole transition as a function of AR and accounting for the incoming TBL properties. The novelty relies on proposing the momentum-thickness-based Reynolds number Re𝜃 as a discriminant for assessing TBL effects on turbulent wake structures.

Place, publisher, year, edition, pages
Elsevier BV , 2025. Vol. 112, article id 109672
Keywords [en]
Wall-mounted square cylinder, Turbulent boundary layer, Critical aspect ratio
National Category
Fluid Mechanics Environmental Engineering Aerospace Engineering
Research subject
Engineering Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-357714DOI: 10.1016/j.ijheatfluidflow.2024.109672ISI: 001383291500001Scopus ID: 2-s2.0-85211096803OAI: oai:DiVA.org:kth-357714DiVA, id: diva2:1920830
Funder
EU, Horizon Europe, 101096698
Note

QC 20250122

Available from: 2024-12-12 Created: 2024-12-12 Last updated: 2025-02-05Bibliographically approved

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Zampino, GerardoAtzori, MarcoZea, EliasOtero, EvelynVinuesa, Ricardo

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