Thrust test stand for pulse jet engine / Hamirul Adli Hashim

Hashim, Hamirul Adli (2004) Thrust test stand for pulse jet engine / Hamirul Adli Hashim. Degree thesis, Universiti Teknologi MARA (UiTM).

Abstract

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.

Metadata

Item Type:	Thesis (Degree)
Creators:	Creators Email / ID Num. Hashim, Hamirul Adli 2000127592
Contributors:	Contribution Name Email / ID Num. Thesis advisor Mohamad, Nazri UNSPECIFIED
Subjects:	T Technology > TJ Mechanical engineering and machinery > Control engineering systems. Automatic machinery (General) T Technology > TL Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineering
Divisions:	Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering
Programme:	Bachelor Engineering (Hons) Mechanical
Keywords:	Jet engine, measurement, parameters
Date:	2004
URI:	https://ir.uitm.edu.my/id/eprint/84288