Numerical modelling of pressure rise combustion for reducing emissions of future civil aircraft
This work assesses the feasibility of designing and implementing the wave rotor (WR), the pulse detonation engine (PDE) and the internal combustion wave rotor (ICWR) as part of novel Brayton cycles able to reduce emissions of future aircraft. The design and evaluation processes are performed using t...
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| Language: | en |
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Cranfield University
2015
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/9259 |