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Article

Effect of Surface Roughness on Aerodynamic Loads of Bluff Body in Vicinity of Smoothed Moving Wall

by
Marcos André de Oliveira
1 and
Luiz Antonio Alcântara Pereira
2,*
1
Civil Engineering Institute, Federal University of Tocantins (UFT), Palmas 77001-090, TO, Brazil
2
Mechanical Engineering Institute, Federal University of Itajubá (UNIFEI), Itajubá 37500-903, MG, Brazil
*
Author to whom correspondence should be addressed.
Appl. Sci. 2024, 14(7), 2919; https://doi.org/10.3390/app14072919
Submission received: 29 February 2024 / Revised: 25 March 2024 / Accepted: 27 March 2024 / Published: 29 March 2024
(This article belongs to the Special Issue Advances and Applications of CFD (Computational Fluid Dynamics))

Abstract

This paper contributes to a new Lagrangian vortex method for the statistical control of turbulence in two-dimensional flow configurations around a rough circular cylinder in ground effect when considering higher subcritical Reynolds numbers, namely 3 × 104 ≤ Re ≤ 2 × 105. A smoothed moving wall (active control technique) is used to include the blockage effect in association with the variation in cylinder surface roughness (passive control technique), characterizing a hybrid approach. In contrast with the previous approaches of our research group, the rough cylinder surface is here geometrically constructed, and a new momentum source term is introduced and calculated for the investigated problem. The methodology is structured by coupling the random Discrete Vortex Method, the Lagrangian Dynamic Roughness Model, and the Large Eddy Simulation with turbulence closure using the truncated Second-Order Velocity Structure Function model. This methodological option has the advantage of dispensing with the use of both a refined near-wall mesh and wall functions. The disadvantage of costly processing is readily solved with Open Multi-Processing. The results reveal that intermediate and high roughness values are most efficient for Reynolds numbers on the orders of 105 and 104, respectively. In employing a moving wall, the transition from the large-gap to the intermediate-gap regime is satisfactorily characterized. For the conditions studied with the hybrid technique, it was concluded that the effect of roughness is preponderant and acts to anticipate the characteristics of a lower gap-to-diameter ratio regime, especially with regard to intermittency.
Keywords: drag reduction; Venturi effect; LES theory; Lagrangian Dynamic Roughness Model; panel method; Discrete Vortex Method drag reduction; Venturi effect; LES theory; Lagrangian Dynamic Roughness Model; panel method; Discrete Vortex Method

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MDPI and ACS Style

Oliveira, M.A.d.; Alcântara Pereira, L.A. Effect of Surface Roughness on Aerodynamic Loads of Bluff Body in Vicinity of Smoothed Moving Wall. Appl. Sci. 2024, 14, 2919. https://doi.org/10.3390/app14072919

AMA Style

Oliveira MAd, Alcântara Pereira LA. Effect of Surface Roughness on Aerodynamic Loads of Bluff Body in Vicinity of Smoothed Moving Wall. Applied Sciences. 2024; 14(7):2919. https://doi.org/10.3390/app14072919

Chicago/Turabian Style

Oliveira, Marcos André de, and Luiz Antonio Alcântara Pereira. 2024. "Effect of Surface Roughness on Aerodynamic Loads of Bluff Body in Vicinity of Smoothed Moving Wall" Applied Sciences 14, no. 7: 2919. https://doi.org/10.3390/app14072919

APA Style

Oliveira, M. A. d., & Alcântara Pereira, L. A. (2024). Effect of Surface Roughness on Aerodynamic Loads of Bluff Body in Vicinity of Smoothed Moving Wall. Applied Sciences, 14(7), 2919. https://doi.org/10.3390/app14072919

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