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Title: Thermal charactristics for the flow of Williamson hybrid nanofluid (MoS₂ + ZnO) based with engine oil over a streched sheet
Authors: Yahya, Asmat Ullah
Salamat, Nadeem
Huang, Wen-Hua
Siddique, Imran
Abdal, Sohaib
Hussain, Sajjad
Keywords: Engineering::Mechanical engineering
Issue Date: 2021
Source: Yahya, A. U., Salamat, N., Huang, W., Siddique, I., Abdal, S. & Hussain, S. (2021). Thermal charactristics for the flow of Williamson hybrid nanofluid (MoS₂ + ZnO) based with engine oil over a streched sheet. Case Studies in Thermal Engineering, 26, 101196-.
Journal: Case Studies in Thermal Engineering
Abstract: The result for enhanced heat transfer to manage increasing heat density of miniature and several other technical processes have urged to analyze thermal transports of hybrid nanofluids. Molybdenum disulfide (MoS2) and Zinc oxide (ZnO) are hybridized as a very dilute homogenous mixture in the bulk engine oil. The flow of this colloidal fluid with heat transfer occurs through pours medium over a stretching sheet. Moreover, an invariant magnetic field, thermal dissipation, and the heat source are incorporated. Theoretical formulation resulted as, set non-linear partial differential equations. To obtain a numerical solution, similarity transform is hired to yield corresponding ordinary differential equations. Computational software Matlab is availed to run the code for the Runge-Kutta method with shooting technique. A deep insight into the problem is inspected by varying the inputs of the dependent functions influential parameters. It is perceived that the flow speed is hindered by the growing inputs of parameters of magnetic field and porosity. It also comes to know that the velocity f′(η) becomes slower with augmentation of φ2 but the temperature rises. A suitable range of the emerging parameters is tried to observe the variation of physical quantities such as skin fraction facts, velocity, local Nusselt number, and temperature of the fluid.
ISSN: 2214-157X
DOI: 10.1016/j.csite.2021.101196
Schools: School of Mechanical and Aerospace Engineering 
Rights: © 2021 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY license (
Fulltext Permission: open
Fulltext Availability: With Fulltext
Appears in Collections:MAE Journal Articles

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