An assessment of high overall pressure ratio intercooled engines for civil aviation
As gas turbine technology matures, further significant improvements in engine efficiency will be difficult to achieve without the implementation of new aero-engine configurations. This thesis delivers an original contribution to knowledge by comparing the design, performance, fuel burn and emission...
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| Language: | en |
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Cranfield University
2016
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/10419 |