Nonviscous Oblique Stagnation Point Flow towards Riga Plate

Purpose. The flow of nonviscous Casson fluid is examined in this study over an oscillating surface. The model of the fluid flow has been inspected in the presence of oblique stagnation point flow. The scrutiny is subsumed for the Riga plate by considering the effects of magnetohydrodynamics. The Rig...

Descripción completa

Guardado en:

Detalles Bibliográficos
Autores principales:	Sobia Akbar, Azad Hussain
Formato:	article
Lenguaje:	EN
Publicado:	Hindawi Limited 2021
Materias:	Engineering (General). Civil engineering (General) TA1-2040 Mathematics QA1-939
Acceso en línea:	https://doaj.org/article/9005a69fe5824bf3bc9b9f99b1c59e6d
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

id	oai:doaj.org-article:9005a69fe5824bf3bc9b9f99b1c59e6d
record_format	dspace
spelling	oai:doaj.org-article:9005a69fe5824bf3bc9b9f99b1c59e6d2021-11-29T00:56:58ZNonviscous Oblique Stagnation Point Flow towards Riga Plate1563-514710.1155/2021/2227269https://doaj.org/article/9005a69fe5824bf3bc9b9f99b1c59e6d2021-01-01T00:00:00Zhttp://dx.doi.org/10.1155/2021/2227269https://doaj.org/toc/1563-5147Purpose. The flow of nonviscous Casson fluid is examined in this study over an oscillating surface. The model of the fluid flow has been inspected in the presence of oblique stagnation point flow. The scrutiny is subsumed for the Riga plate by considering the effects of magnetohydrodynamics. The Riga plate is considered as an electromagnetic lever which carries eternal magnets and a stretching line up of alternating electrodes coupled on a plane surface. We have considered nonboundary layer two-dimensional incompressible flow of the fluid. The fluid flow model is analyzed in the fixed frame of reference. Motivation. The motivation of achieving more suitable results has always been a quest of life for scientists; the capability of determining the boundary layer of flow on aircraft which either stays laminar or turns turbulent has encouraged the researcher to study compressible flow in depth. The compressible fluid with boundary layer flow has been utilized by numerous researchers to reduce skin friction and enhance thermal and convectional heat exchange. Design/Approach/Methodology. The attained partial differential equations will be critically inspected by using suitable similarity transformation to transform these flows thrived equations into higher nonlinear ordinary differential equations (ODE). Then, these equations of motion are intercepted by mathematical techniques such as the bvp4c method in Maple and Matlab. The graphical and tabular representation of different parameters is also given. Findings. The behavior of β and modified Hartmann number M increases by positively increasing the values of both parameters for Fη, while ω decreases with increasing the values of ω for Fη. The graph of β shows upward behavior for distinct values for both Gη and G′η for velocity portray. Prandtl number and β for the temperature profile of θη and θ1η goes downward with increasing parameters.Sobia AkbarAzad HussainHindawi LimitedarticleEngineering (General). Civil engineering (General)TA1-2040MathematicsQA1-939ENMathematical Problems in Engineering, Vol 2021 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	Engineering (General). Civil engineering (General) TA1-2040 Mathematics QA1-939
spellingShingle	Engineering (General). Civil engineering (General) TA1-2040 Mathematics QA1-939 Sobia Akbar Azad Hussain Nonviscous Oblique Stagnation Point Flow towards Riga Plate
description	Purpose. The flow of nonviscous Casson fluid is examined in this study over an oscillating surface. The model of the fluid flow has been inspected in the presence of oblique stagnation point flow. The scrutiny is subsumed for the Riga plate by considering the effects of magnetohydrodynamics. The Riga plate is considered as an electromagnetic lever which carries eternal magnets and a stretching line up of alternating electrodes coupled on a plane surface. We have considered nonboundary layer two-dimensional incompressible flow of the fluid. The fluid flow model is analyzed in the fixed frame of reference. Motivation. The motivation of achieving more suitable results has always been a quest of life for scientists; the capability of determining the boundary layer of flow on aircraft which either stays laminar or turns turbulent has encouraged the researcher to study compressible flow in depth. The compressible fluid with boundary layer flow has been utilized by numerous researchers to reduce skin friction and enhance thermal and convectional heat exchange. Design/Approach/Methodology. The attained partial differential equations will be critically inspected by using suitable similarity transformation to transform these flows thrived equations into higher nonlinear ordinary differential equations (ODE). Then, these equations of motion are intercepted by mathematical techniques such as the bvp4c method in Maple and Matlab. The graphical and tabular representation of different parameters is also given. Findings. The behavior of β and modified Hartmann number M increases by positively increasing the values of both parameters for Fη, while ω decreases with increasing the values of ω for Fη. The graph of β shows upward behavior for distinct values for both Gη and G′η for velocity portray. Prandtl number and β for the temperature profile of θη and θ1η goes downward with increasing parameters.
format	article
author	Sobia Akbar Azad Hussain
author_facet	Sobia Akbar Azad Hussain
author_sort	Sobia Akbar
title	Nonviscous Oblique Stagnation Point Flow towards Riga Plate
title_short	Nonviscous Oblique Stagnation Point Flow towards Riga Plate
title_full	Nonviscous Oblique Stagnation Point Flow towards Riga Plate
title_fullStr	Nonviscous Oblique Stagnation Point Flow towards Riga Plate
title_full_unstemmed	Nonviscous Oblique Stagnation Point Flow towards Riga Plate
title_sort	nonviscous oblique stagnation point flow towards riga plate
publisher	Hindawi Limited
publishDate	2021
url	https://doaj.org/article/9005a69fe5824bf3bc9b9f99b1c59e6d
work_keys_str_mv	AT sobiaakbar nonviscousobliquestagnationpointflowtowardsrigaplate AT azadhussain nonviscousobliquestagnationpointflowtowardsrigaplate
_version_	1718407659202281472

Nonviscous Oblique Stagnation Point Flow towards Riga Plate

Ejemplares similares