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/ http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/1/08226302.pdf

id	iium-60790
recordtype	eprints
spelling	iium-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 PeerReviewed 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
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
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/ http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/ http://irep.iium.edu.my/60790/1/08226302.pdf
first_indexed	2023-09-18T21:26:11Z
last_indexed	2023-09-18T21:26:11Z
_version_	1777412206634205184

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

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