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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| Format: | text::Thesis |
| Language: | en |
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2023
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| _version_ | 1848452268488130560 |
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| author | Mohd Hilmi Bin Hasna Merican |
| author_facet | Mohd Hilmi Bin Hasna Merican |
| author_sort | Mohd Hilmi Bin Hasna Merican |
| building | UNITEN Library |
| collection | Institutional Repository |
| content_provider | Universiti Tenaga Nasional |
| content_source | UNITEN Institutional Repository |
| continent | Asia |
| country | Malaysia |
| 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 |
| id | my.uniten.dspace-20953 |
| institution | Universiti Tenaga Nasional |
| language | en |
| publishDate | 2023 |
| record_format | dspace |
| spelling | my.uniten.dspace-209532025-11-07T15:12:15Z 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 |
| spellingShingle | Fluid dynamics Compressibility Mohd Hilmi Bin Hasna Merican Development of cell centred upwind scheme for 2D CFD solver |
| title | 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_short | Development of cell centred upwind scheme for 2D CFD solver |
| title_sort | development of cell centred upwind scheme for 2d cfd solver |
| topic | Fluid dynamics Compressibility |
| url_provider | http://dspace.uniten.edu.my/ |