Investigation of swirl injectors and supersonic nozzles for the development of a meso-scale thrust chamber / Ahmad Hussein Abdul Hamid
Issues of propellant atomizing, mixing and viscous loss become increasingly more important as the thrust chamber are reduced in size. Two main components in thrust chamber have been identified as critical since small differences in its design can result in dramatically different performance. They...
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| 格式: | Thesis |
| 语言: | English |
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2008
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| 在线阅读: | https://ir.uitm.edu.my/id/eprint/544/1/TM_AHMAD%20HUSSEIN%20ABD%20HAMID%2008_5%201.pdf |
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