Flow Analysis of y-Al2O3 Nanofluid Near a Stagnation Point

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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


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