INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD

Characteristics of the flow around two rotated square cylinders in tandem arrangements at low Reynolds numbers (Re) and normalized gap spacings (S) were numerically investigated using a newly proposed least square moving particle semi-implicit based on vortex particle method. The proposed method...

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Main Author: Firdaus, Al-Faisal
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/70077
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:70077
spelling id-itb.:700772022-12-23T16:03:39ZINVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD Firdaus, Al-Faisal Indonesia Theses Viscous flow; Flow pattern; Vortex shedding; Flow around tandem cylinders; Least square moving particle semi-implicit; Vortex particle method; Immersed boundary method INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/70077 Characteristics of the flow around two rotated square cylinders in tandem arrangements at low Reynolds numbers (Re) and normalized gap spacings (S) were numerically investigated using a newly proposed least square moving particle semi-implicit based on vortex particle method. The proposed method removes the background grid dependencies from the late vortex particle method and improves the computational cost using multiresolution particles. It is found that the proposed method captures the flow characteristics well. In this study, five vortex wake patterns are revealed at different Re (3 ? Re ? 150) and spacing (1.5 ? S ? 6.0). The time history and variations of aerodynamics coefficients, such as drag and lift coefficients, root mean square value of lift coefficient, and Strouhal number, alongside vorticity contours, are discussed to clarify each flow pattern’s characteristics. A significant increase in aerodynamics coefficients is observed for both cylinders at the critical spacing, which may range from 1.5 ? S < 3 depending on the Re. The Strouhal number has an increasing trend past the critical spacing at all selected Re. Meanwhile, the mean drag coefficient of both cylinders remains mostly the same. Conversely, the root mean square value of the lift coefficient of the downstream cylinder has a decreasing trend and, in specific cases, becomes lower than the upstream cylinder. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description Characteristics of the flow around two rotated square cylinders in tandem arrangements at low Reynolds numbers (Re) and normalized gap spacings (S) were numerically investigated using a newly proposed least square moving particle semi-implicit based on vortex particle method. The proposed method removes the background grid dependencies from the late vortex particle method and improves the computational cost using multiresolution particles. It is found that the proposed method captures the flow characteristics well. In this study, five vortex wake patterns are revealed at different Re (3 ? Re ? 150) and spacing (1.5 ? S ? 6.0). The time history and variations of aerodynamics coefficients, such as drag and lift coefficients, root mean square value of lift coefficient, and Strouhal number, alongside vorticity contours, are discussed to clarify each flow pattern’s characteristics. A significant increase in aerodynamics coefficients is observed for both cylinders at the critical spacing, which may range from 1.5 ? S < 3 depending on the Re. The Strouhal number has an increasing trend past the critical spacing at all selected Re. Meanwhile, the mean drag coefficient of both cylinders remains mostly the same. Conversely, the root mean square value of the lift coefficient of the downstream cylinder has a decreasing trend and, in specific cases, becomes lower than the upstream cylinder.
format Theses
author Firdaus, Al-Faisal
spellingShingle Firdaus, Al-Faisal
INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD
author_facet Firdaus, Al-Faisal
author_sort Firdaus, Al-Faisal
title INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD
title_short INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD
title_full INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD
title_fullStr INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD
title_full_unstemmed INVESTIGATION OF THE FLOW AROUND TWO TANDEM ROTATED SQUARE CYLINDERS USING THE LEAST SQUARE MOVING PARTICLE SEMI-IMPLICIT BASED ON VORTEX PARTICLE METHOD
title_sort investigation of the flow around two tandem rotated square cylinders using the least square moving particle semi-implicit based on vortex particle method
url https://digilib.itb.ac.id/gdl/view/70077
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