Thermodynamics Cycle Analysis, Pressure Loss, and Heat Transfer Assessment of a Recuperative System for Aero-Engines

Aiming in the direction of designing more efficient aero-engines, various concepts have been developed in recent years, among which is the concept of an intercooled and recuperative aero-engine. Particularly, in the area of recuperation, MTU Aero Engines has been driving research activities in the l...

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Veröffentlicht in:	Journal of engineering for gas turbines and power 2015-04, Vol.137 (4)
Hauptverfasser:	Goulas, A, Donnerhack, S, Flouros, M, Misirlis, D, Vlahostergios, Z, Yakinthos, K
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engines Assessments Combustion chambers Coolers Engines Exhaust nozzles Fuel consumption Gas Turbines: Aircraft Engine Heat transfer Reduction
Online-Zugang:	Volltext
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