Thrust test stand for pulse jet engine / Nor Azwan Sarbani
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...
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2004
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my-uitm-ir.739562024-05-29T09:36:06Z Thrust test stand for pulse jet engine / Nor Azwan Sarbani 2004 Sarbani, Nor Azwan 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. 2004 Thesis https://ir.uitm.edu.my/id/eprint/73956/ https://ir.uitm.edu.my/id/eprint/73956/1/73956.pdf text en public degree Universiti Teknologi MARA (UiTM) Faculty of Mechanical Engineering Mohamad, Nazri |
| institution |
Universiti Teknologi MARA |
| collection |
UiTM Institutional Repository |
| language |
English |
| advisor |
Mohamad, Nazri |
| description |
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. |
| format |
Thesis |
| qualification_level |
Bachelor degree |
| author |
Sarbani, Nor Azwan |
| spellingShingle |
Sarbani, Nor Azwan Thrust test stand for pulse jet engine / Nor Azwan Sarbani |
| author_facet |
Sarbani, Nor Azwan |
| author_sort |
Sarbani, Nor Azwan |
| title |
Thrust test stand for pulse jet engine / Nor Azwan Sarbani |
| title_short |
Thrust test stand for pulse jet engine / Nor Azwan Sarbani |
| title_full |
Thrust test stand for pulse jet engine / Nor Azwan Sarbani |
| title_fullStr |
Thrust test stand for pulse jet engine / Nor Azwan Sarbani |
| title_full_unstemmed |
Thrust test stand for pulse jet engine / Nor Azwan Sarbani |
| title_sort |
thrust test stand for pulse jet engine / nor azwan sarbani |
| granting_institution |
Universiti Teknologi MARA (UiTM) |
| granting_department |
Faculty of Mechanical Engineering |
| publishDate |
2004 |
| url |
https://ir.uitm.edu.my/id/eprint/73956/1/73956.pdf |
| _version_ |
1804889687962157056 |