Discharge coefficient and jet deflection studies for combustor liner air-entry holes
In the simple tubular combustor system for turbojets and ramjets, figure 1, at the primary zone it is required to achieve a high heat release and stable flame. At the dilution cone to have a good air flow distribution (Ref. I ), and adequate penetration. In both zones these requirements needs to be...
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| Language: | en |
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Cranfield University
2013
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/7834 |