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dc.contributor.author | Huda Choudry, 01-248182-002 | |
dc.date.accessioned | 2021-12-09T07:56:15Z | |
dc.date.available | 2021-12-09T07:56:15Z | |
dc.date.issued | 2020 | |
dc.identifier.uri | http://hdl.handle.net/123456789/11348 | |
dc.description | Supervised by Dr. Jafar Hasnain | en_US |
dc.description.abstract | This thesis examines the flow analysis of Al2O3 NF near a stagnation point over a stretching/shrinking sheet. In the momentum equation, the velocity-ratio effect is also employed. The influence of non-linear thermal radiation R is integrated in the heat equation. Velocity slip is also incorporated at the solid-liquid interface. Further, the effect of mass transfer in addition to chemical-reaction rate R is also considered. Moreover, 2 6 2 C H O is considered as base-fluid. In this work, firstly, the governing boundary equations are converted into ODEs by utilizing similarity variables. In order to tackle the non-dimensionless ODEs numerically, the Runge-Kutta algorithm scheme (4th - order) is employed along with shooting-technique. To acquire numerical procedure, a computer software based MATLAB is implemented as a tool. Six parameters are examined i.e. velocity-ratio reaction-rate , velocity slip ,thermal radiation R, Schmidt number Sc, and power-law index n for the problem. The impact of the above mentioned parameters on the velocity f ,temperature , and concentration fields is portrayed graphically respectively. The research indicates that when the velocity-ratio parameter is greater, the momentum boundary layers thickness increases but concentration boundary-layers thickness decreases. Moreover, for increasing Sc and , x Sh is greater but x Sh decreases in case of increasing Sc and n. | en_US |
dc.language.iso | en | en_US |
dc.publisher | Computer Sciences BUIC | en_US |
dc.relation.ispartofseries | MS (Math);T-049 | |
dc.subject | Nanofluid | en_US |
dc.title | Flow Analysis of y-Al2O3 Nanofluid Near a Stagnation Point | en_US |
dc.type | MS Thesis | en_US |