| KEYWORD |
Development of a conceptual design model for hybrid-electric aircraft
keywords AIRCRAFT CONCEPTUAL DESIGN, AIRCRAFT ELECTRIFICATION, HYBRID ELECTRIC PROPULSION
Reference persons MARCO FIORITI
Research Groups 22-Progetto e sviluppo di sistemi e tecnologie aerospaziali
Thesis type M.SC.
Description The thesis objective is the modification of an existing tool by including more hybrid-electric configurations
- state of the art of preliminary design models for electric hybrid aircraft
- modification of the existing tool by including a module for the automatic generation of the aircraft geometry
- integration of several hybrid-electric configurations
- integration of the model written in Matlab in the existing ASTRID tool
Required skills Progetto dei velivoli, progetto dei sistemi di bordo, MATLAB
Deadline 23/02/2023
PROPONI LA TUA CANDIDATURA