Thrust test stand for pulse jet engine / Nor Azwan Sarbani

Sarbani, Nor Azwan (2004) Thrust test stand for pulse jet engine / Nor Azwan Sarbani. Degree thesis, Universiti Teknologi MARA (UiTM).

Abstract

One of the important performance parameters of a pulse jet engine is the thrust produced. Hence, for any new design, the measurement of the thrust produced is necessary. A test stand was successfully designed and fabricated from scratch using facilities available in the FKM's workshop. The test stand was designed for a pulse jet engine with maximum thrust of 25N. The design concept was based on balancing the moment due to the thrust of the pulse jet engine with a dead weight which is movable so as to provide a counter-moment. Calibration was performed by applying a known force (known weight) at the line of retain of the thrust. The movement of one centimeter movable portion of the minor scale is equivalent to an increment of 0.0294 N of the produced thrust.

Metadata

Item Type: Thesis (Degree)
Creators:
Creators
Email / ID Num.
Sarbani, Nor Azwan
2000127585
Contributors:
Contribution
Name
Email / ID Num.
Thesis advisor
Mohamad, Nazri
UNSPECIFIED
Divisions: Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering
Programme: Bachelor of Engineering (Hons) (Mechanical)
Keywords: pulse, jet, engine
Date: 2004
URI: https://ir.uitm.edu.my/id/eprint/73956
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