Thermal study on non-Newtonian fluids through a porous channel for turbine blades
The current paper aims to utilize non-Newtonian fluid and improve the cooling performance of turbine blades. To implement impinging fluid flow through a porous channel on a hot lower wall, in the first step, the rheology of non-Newtonian behavior is introduced. Then differential quadrature procedure...
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my.uniten.dspace-340642024-10-14T11:17:50Z Thermal study on non-Newtonian fluids through a porous channel for turbine blades Zhu C.-Z. Nematipour M. Bina R. Fayaz H. 57205421992 58367458600 58366758700 58494763000 Non-Newtonian fluid Numerical modeling Nusselt number Porous channel Thermal investigation Equations of motion Flow measurement Non Newtonian flow Non Newtonian liquids Nonlinear equations Nusselt number Reynolds number Rheology Turbine components Viscosity Viscous flow Cooling performance Non-Newtonian fluids Porous channel Power law index Reynold number Thermal Thermal investigation Thermal study Turbine blade Viscosity parameters Turbomachine blades The current paper aims to utilize non-Newtonian fluid and improve the cooling performance of turbine blades. To implement impinging fluid flow through a porous channel on a hot lower wall, in the first step, the rheology of non-Newtonian behavior is introduced. Then differential quadrature procedure is used to convert these highly nonlinear equations of motion to some simple algebraic expressions. There is a reasonable agreement between the present findings with previous research work. Finally, some vital parameters such as the cross-viscosity parameter and power law index are changed to evaluate how these factors improve the cooling performance of turbine blades. The findings show that a rising Prandtle number results in a 19% decrement in temperature pattern. For a constant cross-viscosity parameter, Reynolds number enhancement leads to wall friction augmentation of around 15%. Moreover, a 32% Nusselt number increment is observed by increasing the power law index for the same Reynolds number. � 2023 The Authors Final 2024-10-14T03:17:50Z 2024-10-14T03:17:50Z 2023 Article 10.1016/j.csite.2023.103185 2-s2.0-85163215377 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85163215377&doi=10.1016%2fj.csite.2023.103185&partnerID=40&md5=2b7cea3e728a10bb82c53d71d2da5966 https://irepository.uniten.edu.my/handle/123456789/34064 49 103185 All Open Access Gold Open Access Elsevier Ltd Scopus |
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Non-Newtonian fluid Numerical modeling Nusselt number Porous channel Thermal investigation Equations of motion Flow measurement Non Newtonian flow Non Newtonian liquids Nonlinear equations Nusselt number Reynolds number Rheology Turbine components Viscosity Viscous flow Cooling performance Non-Newtonian fluids Porous channel Power law index Reynold number Thermal Thermal investigation Thermal study Turbine blade Viscosity parameters Turbomachine blades |
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Non-Newtonian fluid Numerical modeling Nusselt number Porous channel Thermal investigation Equations of motion Flow measurement Non Newtonian flow Non Newtonian liquids Nonlinear equations Nusselt number Reynolds number Rheology Turbine components Viscosity Viscous flow Cooling performance Non-Newtonian fluids Porous channel Power law index Reynold number Thermal Thermal investigation Thermal study Turbine blade Viscosity parameters Turbomachine blades Zhu C.-Z. Nematipour M. Bina R. Fayaz H. Thermal study on non-Newtonian fluids through a porous channel for turbine blades |
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The current paper aims to utilize non-Newtonian fluid and improve the cooling performance of turbine blades. To implement impinging fluid flow through a porous channel on a hot lower wall, in the first step, the rheology of non-Newtonian behavior is introduced. Then differential quadrature procedure is used to convert these highly nonlinear equations of motion to some simple algebraic expressions. There is a reasonable agreement between the present findings with previous research work. Finally, some vital parameters such as the cross-viscosity parameter and power law index are changed to evaluate how these factors improve the cooling performance of turbine blades. The findings show that a rising Prandtle number results in a 19% decrement in temperature pattern. For a constant cross-viscosity parameter, Reynolds number enhancement leads to wall friction augmentation of around 15%. Moreover, a 32% Nusselt number increment is observed by increasing the power law index for the same Reynolds number. � 2023 The Authors |
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57205421992 |
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57205421992 Zhu C.-Z. Nematipour M. Bina R. Fayaz H. |
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Article |
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Zhu C.-Z. Nematipour M. Bina R. Fayaz H. |
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Zhu C.-Z. |
title |
Thermal study on non-Newtonian fluids through a porous channel for turbine blades |
title_short |
Thermal study on non-Newtonian fluids through a porous channel for turbine blades |
title_full |
Thermal study on non-Newtonian fluids through a porous channel for turbine blades |
title_fullStr |
Thermal study on non-Newtonian fluids through a porous channel for turbine blades |
title_full_unstemmed |
Thermal study on non-Newtonian fluids through a porous channel for turbine blades |
title_sort |
thermal study on non-newtonian fluids through a porous channel for turbine blades |
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Elsevier Ltd |
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2024 |
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1814061102546288640 |
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