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  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