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) |
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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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