An analysis upon turbine based combined cycle (TBCC) engines focused on the first production implementation of the technology in an aircraft: the propulsion system of the Lockheed SR-71 Blackbird. After a brief historical contextualization of the SR-71 project, the features and the main engineering solutions of the propulsion system will be analysed. Lastly, a short view to the modern state of the art of the technology will be provided with particular attention upon the future of supersonic and hypersonic air travel.
The Lockheed SR-71 Blackbird propulsion system
BAGGIO, FEDERICO
2022/2023
Abstract
An analysis upon turbine based combined cycle (TBCC) engines focused on the first production implementation of the technology in an aircraft: the propulsion system of the Lockheed SR-71 Blackbird. After a brief historical contextualization of the SR-71 project, the features and the main engineering solutions of the propulsion system will be analysed. Lastly, a short view to the modern state of the art of the technology will be provided with particular attention upon the future of supersonic and hypersonic air travel.File in questo prodotto:
| File | Dimensione | Formato | |
|---|---|---|---|
|
Tesi-BaggioFederico.pdf
accesso aperto
Dimensione
603.25 kB
Formato
Adobe PDF
|
603.25 kB | 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/20.500.12608/48861