Numerical study of trapped vortex combustors characteristics in small ramjets
Small-scale ramjets are promising air-breathing engines for high-speed propulsion in military, due to their high specific impulse, low aerodynamic drag and good compatibility with operating systems. The challenges of designing a miniature ramjet combustor mainly stem from insufficient space and shor...
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| Format: | Thesis |
| Language: | English |
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2016
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| Online Access: | https://hdl.handle.net/10356/67062 |