| KEYWORD |
Development of a parametric model for TMS design of more-electric and hybrid electric aircraft
Thesis in external company
keywords TMS, MEA, HYBRID-ELECTRIC
Reference persons MARCO FIORITI
External reference persons Flavio Di Fede (Leonardo Aircraft Division)
Research Groups 22-Progetto e sviluppo di sistemi e tecnologie aerospaziali
Thesis type M.SC.
Description Thesis within a research project with Leonardo Aircraft Division
Main activities:
- state of the art of Thermal Management System applied to different vehicles and applied to electrified aircraft
- definition of main thermal loads and development of mathematical models for TMS design
- integration of the model written in Matlab in the existing ASTRID tool
Required skills Progetto dei velivoli, progetto dei sistemi di bordo, MATLAB
Deadline 25/10/2023
PROPONI LA TUA CANDIDATURA