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CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle

This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and flow parameters on thrust force created by the flow from convergent divergent nozzles to a suddenly expanded circular duct of larger cross-sectional area. The study is focusing on resultant thrust f...

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Main Authors: Pathan, Khizer Ahmed, Khan, Sher Afghan, Dabeer, P. S.
Format: Conference or Workshop Item
Language:English
Published: IEEE 2017
Subjects:
T Technology (General)
T175 Industrial research. Research and development
TL Motor vehicles. Aeronautics. Astronautics
Online Access:http://irep.iium.edu.my/60790/1/08226302.pdf
http://irep.iium.edu.my/60790/
http://ieeexplore.ieee.org/document/8226302/
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spelling my.iium.irep.607902017-12-26T10:59:50Z http://irep.iium.edu.my/60790/ CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle Pathan, Khizer Ahmed Khan, Sher Afghan Dabeer, P. S. T Technology (General) T175 Industrial research. Research and development TL Motor vehicles. Aeronautics. Astronautics This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and flow parameters on thrust force created by the flow from convergent divergent nozzles to a suddenly expanded circular duct of larger cross-sectional area. The study is focusing on resultant thrust force. The nozzles are designed for Mach numbers 1.1, 1.4, 1.8 and 2.0. The CFD analysis is done by varying the area ratios and nozzle pressure ratios for all Mach numbers. The area ratios considered for the analysis are 1, 2, 4, 6, 8, 10 and 12. The values of nozzle pressure ratios considered in the analysis are 2, 4, 6, 8, 10 and 12. The results for different combinations of Mach number, area ratios and nozzle pressure ratios are compared with the help of tables. By observing all the results it can be concluded that the resultant thrust force created by flow through nozzle is strongly influenced by Mach number, area ratio and Nozzle pressure ratio. IEEE 2017-12-21 Conference or Workshop Item REM application/pdf en http://irep.iium.edu.my/60790/1/08226302.pdf Pathan, Khizer Ahmed and Khan, Sher Afghan and Dabeer, P. S. (2017) CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle. In: 2017 2nd International Conference for Convergence in Technology (I2CT), 7-9 April 2017, Pune, Maharashtra, India. http://ieeexplore.ieee.org/document/8226302/ 10.1109/I2CT.2017.8226302
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
topic T Technology (General)
T175 Industrial research. Research and development
TL Motor vehicles. Aeronautics. Astronautics
spellingShingle T Technology (General)
T175 Industrial research. Research and development
TL Motor vehicles. Aeronautics. Astronautics
Pathan, Khizer Ahmed
Khan, Sher Afghan
Dabeer, P. S.
CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
description This paper presents the Computational Fluid Dynamic (CFD) analysis to study the effect geometry and flow parameters on thrust force created by the flow from convergent divergent nozzles to a suddenly expanded circular duct of larger cross-sectional area. The study is focusing on resultant thrust force. The nozzles are designed for Mach numbers 1.1, 1.4, 1.8 and 2.0. The CFD analysis is done by varying the area ratios and nozzle pressure ratios for all Mach numbers. The area ratios considered for the analysis are 1, 2, 4, 6, 8, 10 and 12. The values of nozzle pressure ratios considered in the analysis are 2, 4, 6, 8, 10 and 12. The results for different combinations of Mach number, area ratios and nozzle pressure ratios are compared with the help of tables. By observing all the results it can be concluded that the resultant thrust force created by flow through nozzle is strongly influenced by Mach number, area ratio and Nozzle pressure ratio.
format Conference or Workshop Item
author Pathan, Khizer Ahmed
Khan, Sher Afghan
Dabeer, P. S.
author_facet Pathan, Khizer Ahmed
Khan, Sher Afghan
Dabeer, P. S.
author_sort Pathan, Khizer Ahmed
title CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
title_short CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
title_full CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
title_fullStr CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
title_full_unstemmed CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
title_sort cfd analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle
publisher IEEE
publishDate 2017
url http://irep.iium.edu.my/60790/1/08226302.pdf
http://irep.iium.edu.my/60790/
http://ieeexplore.ieee.org/document/8226302/
_version_ 1643615869893345280
score 13.211869

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