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.

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  • Koleksi Akses Terhad | PTAR Utama | Shah Alam
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