Improving the efficiency of aviation turboshaft engine with the recuperator in the helicopter system
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0128264
Reference21 articles.
1. Optimization and design of heat recovery system for aviation
2. Recuperated gas turbine aeroengines. Part III: engine concepts for reduced emissions, lower fuel consumption, and noise abatement
3. A hybrid engine concept for multi-fuel blended wing body
4. Bouty E, Paty G, Cheftel B 2011 SAGE 5 clean sky's approach to quieter turboshaft engines International Symposium on Air Breathing Engines ISABE p1303.
5. Overall performance design of paralleled heat release and compression system for hypersonic aeroengine
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