Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir

Aviation and Space travel has become more important, demand need to be met with better technology via in depth research on the matter, thruster is propulsive device used by aircraft and spacecraft for altitude control. Thrust force is generated by combustion of propellant which is the fuel and oxidi...

Full description

Saved in:

Bibliographic Details
Main Author:	Syed Mohd Tahir, Syed Daniel Shukri
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Mechanics applied to machinery Dynamics Mechanical movements Machine construction (General)
Online Access:	https://ir.uitm.edu.my/id/eprint/36619/1/36619.pdf
Tags:	Add Tag No Tags, Be the first to tag this record!

id	my-uitm-ir.36619
record_format	uketd_dc
spelling	my-uitm-ir.366192020-11-12T08:01:23Z Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir 2009 Syed Mohd Tahir, Syed Daniel Shukri Mechanics applied to machinery. Dynamics Mechanical movements Machine construction (General) Aviation and Space travel has become more important, demand need to be met with better technology via in depth research on the matter, thruster is propulsive device used by aircraft and spacecraft for altitude control. Thrust force is generated by combustion of propellant which is the fuel and oxidizer within the thrust chamber, that turn the combustion effect to thrust force that accelerated and ejected at high velocity through a nozzle thereby imparting momentum to the system. There are several distinctive variables that determined the efficiency of the thruster nozzle, one of the most important and effective method to do so is by possessing the most superior nozzle configuration. Research is done to studies the effect of variable changes in nozzle design to thruster nozzle parameter, they are subjected to the same flow condition while applying constrain of flight simulation on a sea level altitude. Six different geometry of nozzle divergence section which varies in angle and length, would be studied based on the criteria set under the studies constraint. These studies could aid us by ensuring better understanding of flow characteristic in nozzle studies with emphasize on nozzle configuration by providing comprehensive research information and visualization interpretation via simulation. Also, it is with great expectation that the nation would be interested in further aviation studies where this research could be the basic guideline of thruster design. 2009 Thesis https://ir.uitm.edu.my/id/eprint/36619/ https://ir.uitm.edu.my/id/eprint/36619/1/36619.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Adbul Hamid, Ahmad Hussein
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Adbul Hamid, Ahmad Hussein
topic	Mechanics applied to machinery Dynamics Mechanical movements Machine construction (General)
spellingShingle	Mechanics applied to machinery Dynamics Mechanical movements Machine construction (General) Syed Mohd Tahir, Syed Daniel Shukri Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir
description	Aviation and Space travel has become more important, demand need to be met with better technology via in depth research on the matter, thruster is propulsive device used by aircraft and spacecraft for altitude control. Thrust force is generated by combustion of propellant which is the fuel and oxidizer within the thrust chamber, that turn the combustion effect to thrust force that accelerated and ejected at high velocity through a nozzle thereby imparting momentum to the system. There are several distinctive variables that determined the efficiency of the thruster nozzle, one of the most important and effective method to do so is by possessing the most superior nozzle configuration. Research is done to studies the effect of variable changes in nozzle design to thruster nozzle parameter, they are subjected to the same flow condition while applying constrain of flight simulation on a sea level altitude. Six different geometry of nozzle divergence section which varies in angle and length, would be studied based on the criteria set under the studies constraint. These studies could aid us by ensuring better understanding of flow characteristic in nozzle studies with emphasize on nozzle configuration by providing comprehensive research information and visualization interpretation via simulation. Also, it is with great expectation that the nation would be interested in further aviation studies where this research could be the basic guideline of thruster design.
format	Thesis
qualification_level	Bachelor degree
author	Syed Mohd Tahir, Syed Daniel Shukri
author_facet	Syed Mohd Tahir, Syed Daniel Shukri
author_sort	Syed Mohd Tahir, Syed Daniel Shukri
title	Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir
title_short	Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir
title_full	Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir
title_fullStr	Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir
title_full_unstemmed	Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir
title_sort	computational analysis of thruster nozzle / syed daniel shukri syed mohd tahir
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/36619/1/36619.pdf
_version_	1783734349718355968

Computational analysis of thruster nozzle / Syed Daniel Shukri Syed Mohd Tahir

Similar Items