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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Main Authors: Zhu C.-Z., Nematipour M., Bina R., Fayaz H.
Other Authors: 57205421992
Format: Article
Published: Elsevier Ltd 2024
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Institution: Universiti Tenaga Nasional
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spelling 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
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/
topic 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
spellingShingle 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
description 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
author2 57205421992
author_facet 57205421992
Zhu C.-Z.
Nematipour M.
Bina R.
Fayaz H.
format Article
author Zhu C.-Z.
Nematipour M.
Bina R.
Fayaz H.
author_sort 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
publisher Elsevier Ltd
publishDate 2024
_version_ 1814061102546288640