Spectral proper orthogonal decomposition analysis of coherent vortical structures in the wake of a rectangular cylinder

This study investigates the unsteady flow around a wall-mounted square cylinder (WMSC) with an aspect ratio of 7 at a Reynolds number of 12 000 using large eddy simulation with the wall-adapting local eddy-viscosity subgrid-scale model in OpenFOAM. To analyze dominant flow structures, spectral proper orthogonal decomposition (SPOD) is applied to 26 planes oriented in the x-, y-, and z-normal directions. The results reveal key shedding phenomena, including a primary vortex-shedding mode at a Strouhal number of ∼0.105 and a second-cell vortex shedding at St≈0.127. The second-cell vortex shedding is concentrated near the base and junction of the cylinder, with minimal influence from mid to tip regions. Additionally, a secondary tip vortex at St≈1.8 is identified in three dimensions, originating at the rooftop of leading edge and localized near the tip. To examine this high-frequency feature, both two-dimensional and three-dimensional SPOD analyses are performed. While two-dimensional SPOD captures localized high-frequency structures, full-domain three-dimensional SPOD shows these structures are often masked by more energetic low-frequency modes. However, restricting the three-dimensional SPOD domain to the tip region clearly distinguishes the secondary tip vortex from dominant wake shedding. These findings demonstrate multi-cell shedding patterns and distinct high-frequency vortical structures, challenging the assumption of a single dominant shedding mechanism behind WMSC. Identifying multiple coherent structures at different frequencies highlights the importance of spectral techniques in resolving turbulence interactions in finite cylinder wakes.

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Publication Details

Journal
Physics of Fluids
Published
2025-04-01
DOI
https://doi.org/10.1063/5.0263818
Citations
4
Primary Topic
Fluid Dynamics and Vibration Analysis
Type
article
Field-Weighted Citation Impact
5.34

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article

Spectral proper orthogonal decomposition analysis of coherent vortical structures in the wake of a rectangular cylinder

Reda R. Mankbadi, Vladimir V. Golubev, Alireza Maleki
4 citations
Physics of Fluids
Fluid Dynamics and Vibration Analysis
5.34
article

Spectral proper orthogonal decomposition analysis of coherent vortical structures in the wake of a rectangular cylinder

Reda R. Mankbadi, Vladimir V. Golubev, Alireza Maleki
article en
4 citations

Abstract

This study investigates the unsteady flow around a wall-mounted square cylinder (WMSC) with an aspect ratio of 7 at a Reynolds number of 12 000 using large eddy simulation with the wall-adapting local eddy-viscosity subgrid-scale model in OpenFOAM. To analyze dominant flow structures, spectral proper orthogonal decomposition (SPOD) is applied to 26 planes oriented in the x-, y-, and z-normal directions. The results reveal key shedding phenomena, including a primary vortex-shedding mode at a Strouhal number of ∼0.105 and a second-cell vortex shedding at St≈0.127. The second-cell vortex shedding is concentrated near the base and junction of the cylinder, with minimal influence from mid to tip regions. Additionally, a secondary tip vortex at St≈1.8 is identified in three dimensions, originating at the rooftop of leading edge and localized near the tip. To examine this high-frequency feature, both two-dimensional and three-dimensional SPOD analyses are performed. While two-dimensional SPOD captures localized high-frequency structures, full-domain three-dimensional SPOD shows these structures are often masked by more energetic low-frequency modes. However, restricting the three-dimensional SPOD domain to the tip region clearly distinguishes the secondary tip vortex from dominant wake shedding. These findings demonstrate multi-cell shedding patterns and distinct high-frequency vortical structures, challenging the assumption of a single dominant shedding mechanism behind WMSC. Identifying multiple coherent structures at different frequencies highlights the importance of spectral techniques in resolving turbulence interactions in finite cylinder wakes.

Physics of FluidsVol. 37(4)
Embry–Riddle Aeronautical University (US)
Aeronautics Research Mission Directorate
Openalex Percentile: Top 5%
Fluid Dynamics and Vibration Analysis
5.34
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