In this thesis I analysed two turbofan engines with unmixed flows using the GasTurb software. Engine performances are obtained for design and off-desing cycle points. Flight performances of both the engines are also compared in an hypotetical test flight. In the last chapter I completed a fan preliminary design based on simulated results obtained in GasTurb, and then I compared it to real geometrical fan data.
Performance of modern unmixed turbofan engines: model simulation, analysis and optimization using GasTurb software
Fanzago, Bruno
2019/2020
Abstract
In this thesis I analysed two turbofan engines with unmixed flows using the GasTurb software. Engine performances are obtained for design and off-desing cycle points. Flight performances of both the engines are also compared in an hypotetical test flight. In the last chapter I completed a fan preliminary design based on simulated results obtained in GasTurb, and then I compared it to real geometrical fan data.File in questo prodotto:
File | Dimensione | Formato | |
---|---|---|---|
Fanzago_Bruno_1180012.pdf
Open Access dal 16/10/2022
Dimensione
6.11 MB
Formato
Adobe PDF
|
6.11 MB | Adobe PDF | Visualizza/Apri |
The text of this website © Università degli studi di Padova. Full Text are published under a non-exclusive license. Metadata are under a CC0 License
Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/28908