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Development of cell centred upwind scheme for 2D CFD solver

This thesis compares the cell-vertex and cell-centred schemes in the simulation of high speed compressible flow. The calculation is carried out using the Computational Fluid Dynamic (CFD) where mass, momentum and energy equations are solved simultaneously over the flow domain. The geometry used to i...

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Main Author: Mohd Hilmi Bin Hasna Merican
Format: text::Thesis
Language:English
Published: 2023
Subjects:
Fluid dynamics
Compressibility
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id my.uniten.dspace-20953
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spelling my.uniten.dspace-209532023-05-04T15:49:39Z Development of cell centred upwind scheme for 2D CFD solver Mohd Hilmi Bin Hasna Merican Fluid dynamics Compressibility This thesis compares the cell-vertex and cell-centred schemes in the simulation of high speed compressible flow. The calculation is carried out using the Computational Fluid Dynamic (CFD) where mass, momentum and energy equations are solved simultaneously over the flow domain. The geometry used to investigate the flow consist a single shock tube channel and structure H-mesh scheme is implemented throughout the flow domain. The finite volume CFD solver employs first order and second order accurate upwind differencing scheme for the spatial discretization. In addition, a few comparisons between the new solver and existing solver are made. 2023-05-03T15:38:35Z 2023-05-03T15:38:35Z 2011 Resource Types::text::Thesis https://irepository.uniten.edu.my/handle/123456789/20953 en application/pdf
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
language English
topic Fluid dynamics
Compressibility
spellingShingle Fluid dynamics
Compressibility
Mohd Hilmi Bin Hasna Merican
Development of cell centred upwind scheme for 2D CFD solver
description This thesis compares the cell-vertex and cell-centred schemes in the simulation of high speed compressible flow. The calculation is carried out using the Computational Fluid Dynamic (CFD) where mass, momentum and energy equations are solved simultaneously over the flow domain. The geometry used to investigate the flow consist a single shock tube channel and structure H-mesh scheme is implemented throughout the flow domain. The finite volume CFD solver employs first order and second order accurate upwind differencing scheme for the spatial discretization. In addition, a few comparisons between the new solver and existing solver are made.
format Resource Types::text::Thesis
author Mohd Hilmi Bin Hasna Merican
author_facet Mohd Hilmi Bin Hasna Merican
author_sort Mohd Hilmi Bin Hasna Merican
title Development of cell centred upwind scheme for 2D CFD solver
title_short Development of cell centred upwind scheme for 2D CFD solver
title_full Development of cell centred upwind scheme for 2D CFD solver
title_fullStr Development of cell centred upwind scheme for 2D CFD solver
title_full_unstemmed Development of cell centred upwind scheme for 2D CFD solver
title_sort development of cell centred upwind scheme for 2d cfd solver
publishDate 2023
_version_ 1806424518027116544
score 13.214268

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