Thrust test stand for pulse jet engine / Hamirul Adli Hashim

One of the important performance parameters of a pulse jet engine is the thrustproduced. Hence, for any new design, the measurement of the thrust produced isnecessary. A test stand was successfully designed and fabricated from scratch usingfacilities available in the FKM's workshop. The test st...

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Bibliographic Details
Main Author:	Hashim, Hamirul Adli
Format:	Thesis
Language:	English
Published:	2004
Subjects:	Control engineering systems Automatic machinery (General)
Online Access:	https://ir.uitm.edu.my/id/eprint/84288/1/84288.pdf
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id	my-uitm-ir.84288
record_format	uketd_dc
spelling	my-uitm-ir.842882024-01-24T03:30:20Z Thrust test stand for pulse jet engine / Hamirul Adli Hashim 2004 Hashim, Hamirul Adli Control engineering systems. Automatic machinery (General) Aeronautics. Aeronautical engineering One of the important performance parameters of a pulse jet engine is the thrustproduced. Hence, for any new design, the measurement of the thrust produced isnecessary. A test stand was successfully designed and fabricated from scratch usingfacilities available in the FKM's workshop. The test stand was designed for a pulse jetengine with maximum thrust of 25 N.The design concept was based on balancing the moment due to the thrust of thepulse jet engine with a dead weight which is movable so as to provide a counter-moment. 2004 Thesis https://ir.uitm.edu.my/id/eprint/84288/ https://ir.uitm.edu.my/id/eprint/84288/1/84288.pdf text en public degree Universiti Teknologi MARA (UiTM) Faculty of Mechanical Engineering Mohamad, Nazri
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Mohamad, Nazri
topic	Control engineering systems Automatic machinery (General) Control engineering systems Automatic machinery (General)
spellingShingle	Control engineering systems Automatic machinery (General) Control engineering systems Automatic machinery (General) Hashim, Hamirul Adli Thrust test stand for pulse jet engine / Hamirul Adli Hashim
description	One of the important performance parameters of a pulse jet engine is the thrustproduced. Hence, for any new design, the measurement of the thrust produced isnecessary. A test stand was successfully designed and fabricated from scratch usingfacilities available in the FKM's workshop. The test stand was designed for a pulse jetengine with maximum thrust of 25 N.The design concept was based on balancing the moment due to the thrust of thepulse jet engine with a dead weight which is movable so as to provide a counter-moment.
format	Thesis
qualification_level	Bachelor degree
author	Hashim, Hamirul Adli
author_facet	Hashim, Hamirul Adli
author_sort	Hashim, Hamirul Adli
title	Thrust test stand for pulse jet engine / Hamirul Adli Hashim
title_short	Thrust test stand for pulse jet engine / Hamirul Adli Hashim
title_full	Thrust test stand for pulse jet engine / Hamirul Adli Hashim
title_fullStr	Thrust test stand for pulse jet engine / Hamirul Adli Hashim
title_full_unstemmed	Thrust test stand for pulse jet engine / Hamirul Adli Hashim
title_sort	thrust test stand for pulse jet engine / hamirul adli hashim
granting_institution	Universiti Teknologi MARA (UiTM)
granting_department	Faculty of Mechanical Engineering
publishDate	2004
url	https://ir.uitm.edu.my/id/eprint/84288/1/84288.pdf
_version_	1794191990337830912

Thrust test stand for pulse jet engine / Hamirul Adli Hashim

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