Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation
This work deals with the numerical solutions of combustible boundary layer flow over an axisymmetric body. A mathematical structure is taken out by explaining the governing equations of continuity, velocity, energy and concentration. These are solved employing the finite difference technique. The na...
Main Authors: | , , , , |
---|---|
Format: | Article |
Language: | English |
Published: |
Elsevier
2021-10-01
|
Series: | Cleaner Engineering and Technology |
Subjects: | |
Online Access: | http://www.sciencedirect.com/science/article/pii/S2666790821001890 |
id |
doaj-18c113a049ea448e921ef53d8ca99bc2 |
---|---|
record_format |
Article |
spelling |
doaj-18c113a049ea448e921ef53d8ca99bc22021-09-11T04:31:17ZengElsevierCleaner Engineering and Technology2666-79082021-10-014100229Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiationNepal Chandra Roy0Sadia Masud1Salaika Parvin2Sudharonjon Roy3Ram Prakash Sharma4Department of Mathematics, University of Dhaka, Dhaka, 1000, Bangladesh; Corresponding author.Department of Mathematics, University of Dhaka, Dhaka, 1000, BangladeshDepartment of Mathematics, University of Dhaka, Dhaka, 1000, BangladeshDepartment of Mathematics, University of Dhaka, Dhaka, 1000, BangladeshDepartment of Mechanical Engineering, National Institute of Technology, Arunachal Pradesh, 791112, IndiaThis work deals with the numerical solutions of combustible boundary layer flow over an axisymmetric body. A mathematical structure is taken out by explaining the governing equations of continuity, velocity, energy and concentration. These are solved employing the finite difference technique. The nature of the flow is analyzed using velocity, temperature and mass concentration for different physical parameters such as, surface location, Prandtl number, Schmidt number, viscosity variation parameter, thermal conductivity parameter and the radiation parameter. It is found that the viscosity variation and thermal conductivity parameter augment the thicknesses of thermal and concentration layers and reduces the momentum thickness. Moreover, the momentum, thermal and concentration boundary layers become thick for larger values of radiation parameter whereas the reverse characteristic is observed for higher value of the Prandtl number.http://www.sciencedirect.com/science/article/pii/S2666790821001890Boundary layerAxisymmetric bodyThermal radiationVariable thermo-physical propertiesMixed convection |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Nepal Chandra Roy Sadia Masud Salaika Parvin Sudharonjon Roy Ram Prakash Sharma |
spellingShingle |
Nepal Chandra Roy Sadia Masud Salaika Parvin Sudharonjon Roy Ram Prakash Sharma Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation Cleaner Engineering and Technology Boundary layer Axisymmetric body Thermal radiation Variable thermo-physical properties Mixed convection |
author_facet |
Nepal Chandra Roy Sadia Masud Salaika Parvin Sudharonjon Roy Ram Prakash Sharma |
author_sort |
Nepal Chandra Roy |
title |
Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation |
title_short |
Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation |
title_full |
Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation |
title_fullStr |
Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation |
title_full_unstemmed |
Impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation |
title_sort |
impact of variable thermo-physical properties on the combustion of a gas mixture past an axisymmetric body with thermal radiation |
publisher |
Elsevier |
series |
Cleaner Engineering and Technology |
issn |
2666-7908 |
publishDate |
2021-10-01 |
description |
This work deals with the numerical solutions of combustible boundary layer flow over an axisymmetric body. A mathematical structure is taken out by explaining the governing equations of continuity, velocity, energy and concentration. These are solved employing the finite difference technique. The nature of the flow is analyzed using velocity, temperature and mass concentration for different physical parameters such as, surface location, Prandtl number, Schmidt number, viscosity variation parameter, thermal conductivity parameter and the radiation parameter. It is found that the viscosity variation and thermal conductivity parameter augment the thicknesses of thermal and concentration layers and reduces the momentum thickness. Moreover, the momentum, thermal and concentration boundary layers become thick for larger values of radiation parameter whereas the reverse characteristic is observed for higher value of the Prandtl number. |
topic |
Boundary layer Axisymmetric body Thermal radiation Variable thermo-physical properties Mixed convection |
url |
http://www.sciencedirect.com/science/article/pii/S2666790821001890 |
work_keys_str_mv |
AT nepalchandraroy impactofvariablethermophysicalpropertiesonthecombustionofagasmixturepastanaxisymmetricbodywiththermalradiation AT sadiamasud impactofvariablethermophysicalpropertiesonthecombustionofagasmixturepastanaxisymmetricbodywiththermalradiation AT salaikaparvin impactofvariablethermophysicalpropertiesonthecombustionofagasmixturepastanaxisymmetricbodywiththermalradiation AT sudharonjonroy impactofvariablethermophysicalpropertiesonthecombustionofagasmixturepastanaxisymmetricbodywiththermalradiation AT ramprakashsharma impactofvariablethermophysicalpropertiesonthecombustionofagasmixturepastanaxisymmetricbodywiththermalradiation |
_version_ |
1717757133353648128 |