Thrust test stand for pulse jet engine / Hamirul Adli Hashim
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 st...
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| 语言: | English |
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2004
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my-uitm-ir.842882024-01-24T03:30:20Z Thrust test stand for pulse jet engine / Hamirul Adli Hashim 2004 Hashim, Hamirul Adli Control engineering systems. Automatic machinery (General) Aeronautics. Aeronautical engineering 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. 2004 Thesis https://ir.uitm.edu.my/id/eprint/84288/ https://ir.uitm.edu.my/id/eprint/84288/1/84288.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 |
| topic |
Control engineering systems Automatic machinery (General) Control engineering systems Automatic machinery (General) |
| spellingShingle |
Control engineering systems Automatic machinery (General) Control engineering systems Automatic machinery (General) Hashim, Hamirul Adli Thrust test stand for pulse jet engine / Hamirul Adli Hashim |
| description |
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. |
| format |
Thesis |
| qualification_level |
Bachelor degree |
| author |
Hashim, Hamirul Adli |
| author_facet |
Hashim, Hamirul Adli |
| author_sort |
Hashim, Hamirul Adli |
| title |
Thrust test stand for pulse jet engine / Hamirul Adli Hashim |
| title_short |
Thrust test stand for pulse jet engine / Hamirul Adli Hashim |
| title_full |
Thrust test stand for pulse jet engine / Hamirul Adli Hashim |
| title_fullStr |
Thrust test stand for pulse jet engine / Hamirul Adli Hashim |
| title_full_unstemmed |
Thrust test stand for pulse jet engine / Hamirul Adli Hashim |
| title_sort |
thrust test stand for pulse jet engine / hamirul adli hashim |
| granting_institution |
Universiti Teknologi MARA (UiTM) |
| granting_department |
Faculty of Mechanical Engineering |
| publishDate |
2004 |
| url |
https://ir.uitm.edu.my/id/eprint/84288/1/84288.pdf |
| _version_ |
1794191990337830912 |