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Improved Local Scale Generic Cycle Model for Aerothermodynamic Simulations of Gas Turbine Engines for Propulsion

A local scale Aerothermodynamic Generic Cycle Model (AGCM) is proposed. The AGCM accounts for several improvements not considered in similar models, such as compressor bleed extraction for aircraft Environmental Control System (ECS), parasitic shaft power extraction, and the enthalpy of the fuel ent...

Täydet tiedot

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Bibliografiset tiedot
Päätekijät: Manuel de Jesús Gurrola Arrieta, Ruxandra Mihaela Botez
Aineistotyyppi: Artigo
Kieli:Inglês
Julkaistu: MDPI AG 2022-10-01
Sarja:Designs
Aiheet:
Linkit:https://www.mdpi.com/2411-9660/6/5/91
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