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.

Item Details
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
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  • Koleksi Akses Terhad | PTAR Utama | Shah Alam
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