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Author:

Khan, Mumtaz (Khan, Mumtaz.) | Lu, Dianchen (Lu, Dianchen.) | Rasool, Ghulam (Rasool, Ghulam.) | Deebani, Wejdan (Deebani, Wejdan.) | Shaaban, Shaaban M. (Shaaban, Shaaban M..)

Indexed by:

EI Scopus SCIE

Abstract:

Nanoparticles have gained recognition for significantly improving convective heat transfer efficiency near boundary layer flows. The characteristics of both momentum and thermal boundary layers are significantly influenced by the Prandtl number, which holds a crucial role. In this vein, the current study conducted a detailed computational analysis of the mixed convection flow of gamma-Al2O3 and gamma-Al2O3-C2H6O2 nanofluids over a stretching surface. This research integrates an effective Prandtl number, utilizing viscosity and thermal conductivity models based on empirical findings. Additionally, a unique double-fractional constitutive model is debuted to accurately evaluate the effective Prandtl number's function in the boundary layer. The equations were solved using a numerical technique that combined the finite-difference method with the L-1 algorithm. This investigation presents numerical findings related to the velocity, temperature distributions, wall shear stress coefficient, and heat transfer coefficient, contrasting scenarios with and without the effective Prandtl number. The research shows that integrating nanoparticles into the base fluids reduces the temperature of the nanofluid with an effective Prandtl number while enhancing the heat transfer rate irrespective of its presence. Nonetheless, the introduction of a fractional parameter reduced the heat transfer efficiency within the system. Notably, the gamma-Al2O3-C2H6O2 nanofluid demonstrates superior heat transfer enhancement capabilities compared to its gamma-Al2O3 counterpart but also exacerbates the drag coefficient more significantly. Many practical applications of this study include electronics cooling, industrial process heat exchangers, and rotating and stationary gas turbines in power plants, and efficient heat exchangers in aircraft.

Keyword:

nanofluids double-fractional constitutive model finite difference method effective Prandtl number mixed convection flow

Author Community:

  • [ 1 ] [Khan, Mumtaz]Jiangsu Univ, Fac Sci, Zhenjiang 212013, Jiangsu, Peoples R China
  • [ 2 ] [Lu, Dianchen]Jiangsu Univ, Fac Sci, Zhenjiang 212013, Jiangsu, Peoples R China
  • [ 3 ] [Rasool, Ghulam]Beijing Univ Technol, Coll Mech & Energy Engn, Beijing 100124, Peoples R China
  • [ 4 ] [Deebani, Wejdan]King Abdulaziz Univ, Coll Sci & Arts, Dept Math, Rabigh 21911, Saudi Arabia
  • [ 5 ] [Shaaban, Shaaban M.]Northern Border Univ, Coll Engn, Dept Elect Engn, Ar Ar 91431, Saudi Arabia

Reprint Author's Address:

  • [Rasool, Ghulam]Beijing Univ Technol, Coll Mech & Energy Engn, Beijing 100124, Peoples R China;;

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Source :

JOURNAL OF COMPUTATIONAL DESIGN AND ENGINEERING

Year: 2024

Issue: 4

Volume: 11

Page: 319-331

Cited Count:

WoS CC Cited Count: 5

SCOPUS Cited Count: 5

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 8

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