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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2004
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my.uitm.ir.842882024-01-24T03:30:20Z https://ir.uitm.edu.my/id/eprint/84288/ Thrust test stand for pulse jet engine / Hamirul Adli Hashim 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 NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/84288/1/84288.pdf Thrust test stand for pulse jet engine / Hamirul Adli Hashim. (2004) Degree thesis, thesis, Universiti Teknologi MARA (UiTM). |
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English |
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Control engineering systems. Automatic machinery (General) Aeronautics. Aeronautical engineering |
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Control engineering systems. Automatic machinery (General) Aeronautics. Aeronautical engineering 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 |
| 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 |
| publishDate |
2004 |
| url |
https://ir.uitm.edu.my/id/eprint/84288/1/84288.pdf https://ir.uitm.edu.my/id/eprint/84288/ |
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1789429214981652480 |
| score |
13.160551 |